Commission Directive (EU) 2015/996 of 19 May 2015 establishing common noise assessment methods according to Directive 2002/49/EC of the European Parliament and of the Council (Text with EEA relevance)

1.7.2015 EN Official Journal of the European Union L 168/1 II (Non-legislative acts) DIRECTIVES COMMISSION DIRECTIVE (EU) 2015/996 of 19 May 2015 establishing common noise assessment methods according to Directive 2002/49/EC of the European Parliament and of the Council (Text with EEA relevance) THE EUROPEAN COMMISSION, Having regard to the Treaty on the Functioning of the European Union, Having regard to Directive 2002/49/EC of the European Parliament and of the Council of 25 June 2002 relating to the assessment and management of environmental noise (1), and in particular Article 6, paragraph 2 thereof, Whereas: (1) According to its Article 1, the aim of Directive 2002/49/EC is to define a common approach intended to avoid, prevent or reduce on a prioritised basis the harmful effects, including annoyance, due to exposure to environ­ mental noise. To that end the Member States shall determine the exposure to environmental noise, through noise mapping, by methods of assessment common to the Member States, shall ensure that information on environ­ mental noise and its effects is made available to the public and shall adopt action plans based upon noise- mapping results, with a view to preventing and reducing environmental noise where necessary and particularly where exposure levels can induce harmful effects on human health, and to preserving environmental noise quality where it is good. (2) According to Article 5 of Directive 2002/49/EC, Member States shall apply the noise indicators (L and L ) den night referred to in Annex I to that Directive for the preparation and revision of strategic noise mapping in accordance with Article 7. (3) According to Article 6 of Directive 2002/49/EC, the values of the noise indicators (L and L ) shall be den night determined by means of the assessment methods defined in Annex II to that Directive. (4) According to Article 6 of Directive 2002/49/EC, the Commission shall establish common assessment methods for the determination of the noise indicators L and L through a revision of Annex II. den night (5) According to Article 7 of Directive 2002/49/EC, Member States shall ensure that strategic noise maps are made no later than 30 June 2007 and 30 June 2012 and thereafter reviewed, and revised if necessary, at least every 5 years. (6) Directive 2002/49/EC provides for action plans to be based on strategic noise maps. Strategic noise maps shall be drawn up with the common assessment methods when these methods have been adopted by Member States. However, Member States may use other methods to design measures addressing priorities identified by using the common methods as well as for assessment of other national measures to prevent and reduce environmental noise. (1) OJ L 189, 18.7.2002, p. 12.L 168/2 EN Official Journal of the European Union 1.7.2015 (7) In 2008, the Commission launched the development of the common noise assessment methodological framework through the project ‘Common Noise Assessment Methods in the EU’ (CNOSSOS-EU) led by its Joint Research Centre. The project was carried out in close consultation with the Committee established under Article 18 of Directive 2000/14/EC of the European Parliament and of the Council (1), and other experts from Member States. Its results were published in the JRC Reference Report on CNOSSOS-EU (2). (8) The Annex to this Commission Directive sets out the common assessment methods. Member States are required to use these methods from 31 December 2018 onwards. (9) The assessment methods provided for in the Annex to this Directive are, according to its Article 2, paragraph 1, to be adopted by 31 December 2018 at the latest and until that date Member States may, according to Article 6, paragraph 2 of Directive 2002/49/EC, continue to use the existing assessment methods that they have previously adopted at the national level. (10) In accordance with Article 12 of Directive 2002/49/EC, the Commission shall adapt Annex II to technical and scientific progress. (11) Apart from the adaptation to scientific and technical progress in accordance with Article 12 of Directive 2002/49/EC, the Commission shall endeavour to modify the Annex based on the experience from Member States. (12) The common assessment methods are also to be used for the purpose of other EU legislation where that legislation refers to Annex II to Directive 2002/49/EC. (13) The measures provided for in this Directive are in accordance with the opinion of the Committee established under Article 13 of Directive 2002/49/EC, HAS ADOPTED THIS DIRECTIVE: Article 1 Annex II to Directive 2002/49/EC is replaced by the text set out in the Annex to this Directive. Article 2 1. Member States shall bring into force the laws, regulations and administrative provisions necessary to comply with this Directive by 31 December 2018 at the latest. They shall forthwith communicate to the Commission the text of those provisions. When Member States adopt those provisions, they shall contain a reference to this Directive or be accompanied by such a reference on the occasion of their official publication. Member States shall determine how such reference is to be made. 2. Member States shall communicate to the Commission the text of the main provisions of national law which they adopt in the field covered by this Directive. Article 3 This Directive shall enter into force on the day following that of its publication in the Official Journal of the European Union. (1) Directive 2000/14/EC of the European Parliament and of the Council of 8 May 2000 on the approximation of the laws of the Member States relating to the noise emission in the environment by equipment for use outdoors (OJ L 162, 3.7.2000, p. 1). (2) Common Noise Assessment Methods in Europe (CNOSSOS-EU) — JRC Reference Report, EUR 25379 EN. Luxembourg: Publications Office of the European Union, 2012, — ISBN 978-92-79-25281-51.7.2015 EN Official Journal of the European Union L 168/3 Article 4 This Directive is addressed to the Member States. Done at Brussels, 19 May 2015. For the Commission, On behalf of the President, Karmenu VELLA Member of the CommissionL 168/4 EN Official Journal of the European Union 1.7.2015 ANNEX ASSESSMENT METHODS FOR THE NOISE INDICATORS (Referred to in Article 6 of Directive 2002/49/EC) 1. INTRODUCTION The values of L and L shall be determined at the assessment positions by computation, according to the den night method set out in Chapter 2 and the data described in Chapter 3. Measurements may be performed according to Chapter 4. 2. COMMON NOISE ASSESSMENT METHODS 2.1. General provisions — Road traffic, railway and industrial noise 2.1.1. Indicators, frequency range and band definitions Noise calculations shall be defined in the frequency range from 63 Hz to 8 kHz. Frequency band results shall be provided at the corresponding frequency interval. Calculations are performed in octave bands for road traffic, railway traffic and industrial noise, except for the railway noise source sound power, that uses third octave bands. For road traffic, railway traffic and industrial noise, based on these octave band results, the A-weighted long term average sound pressure level for the day, evening and night period, as defined in Annex I and referred to in Art. 5 of Directive 2002/49/EC, is computed by summation over all frequencies: X L Aeq,T ¼10�lg 10ðLeq,T,iþAiÞ=10 (2.1.1) i¼1 where A denotes the A-weighting correction according to IEC 61672-1 i i = frequency band index and T is the time period corresponding to day, evening or night. Noise parameters: L Instantaneous sound pressure level [dB] p (re. 2 10–5 Pa) L Global long-term sound level L due to all sources and image sources at [dB] Aeq,LT Aeq point R (re. 2 10–5 Pa) L ‘In situ’ sound power level of a point source (moving or steady) [dB] W (re. 10–12 W) L Directional ‘in situ’ sound power level for the i-th frequency band [dB] W,i,dir (re. 10–12 W) L Average ‘in situ’ sound power level per metre of source line [dB/m] W′ (re. 10–12 W)1.7.2015 EN Official Journal of the European Union L 168/5 Other physical parameters: p r.m.s. of the instantaneous sound pressure [Pa] p Reference sound pressure = 2 10–5 Pa [Pa] 0 W Reference sound power = 10–12 W [watt] 0 2.1.2. Quality framework Accuracy of input values All input values affecting the emission level of a source shall be determined with at least the accuracy corresponding to an uncertainty of ± 2dB(A) in the emission level of the source (leaving all other parameters unchanged). Use of default values In the application of the method, the input data shall reflect the actual usage. In general there shall be no reliance on default input values or assumptions. Default input values and assumptions are accepted if the collection of real data is associated with disproportionately high costs. Quality of the software used for the calculations Software used to perform the calculations shall prove compliance with the methods herewith described by means of certification of results against test cases. 2.2. Road traffic noise 2.2.1. Source description Classification of vehicles The road traffic noise source shall be determined by combining the noise emission of each individual vehicle forming the traffic flow. These vehicles are grouped into five separate categories with regard to their character­ istics of noise emission: Category 1: Light motor vehicles Category 2: Medium heavy vehicles Category 3: Heavy vehicles Category 4: Powered two-wheelers Category 5: Open category In the case of powered two-wheelers, two separate subclasses are defined for mopeds and more powerful motorcycles, since they operate in very different driving modes and their numbers usually vary widely. The first four categories shall be used, and the fifth category is optional. It is foreseen for new vehicles that may be developed in the future and may be sufficiently different in their noise emission to require an additional category to be defined. This category could cover, for example, electric or hybrid vehicles or any vehicle developed in the future substantially different from those in categories 1 to 4.L 168/6 EN Official Journal of the European Union 1.7.2015 The details of the different vehicle classes are given in Table [2.2.a]. Table [2.2.a] Vehicle classes Vehicle category in EC Category Name Description Whole Vehicle Type Ap­ proval(1) 1 Light motor vehicles Passenger cars, delivery vans ≤ 3,5 tons, SUVs(2), M1 and N1 MPVs(3) including trailers and caravans 2 Medium heavy vehi­ Medium heavy vehicles, delivery vans > 3,5 tons, M2, M3 and N2, N3 cles buses, motorhomes, etc. with two axles and twin tyre mounting on rear axle 3 Heavy vehicles Heavy duty vehicles, touring cars, buses, with M2 and N2 with trailer, three or more axles M3 and N3 4 Powered two-wheel­ 4a Two-, Three- and Four-wheel Mopeds L1, L2, L6 ers 4b Motorcycles with and without sidecars, Tri­ L3, L4, L5, L7 cycles and Quadricycles 5 Open category To be defined according to future needs N/A (1) Directive 2007/46/EC of the European Parliament and of the Council of 5 September 2007 establishing a framework for the approval of motor vehicles and their trailers, and of systems, components and separate technical units intended for such vehicles (OJ L 263, 9.10.2007, p. 1). (2) Sport Utility Vehicles. (3) Multi-Purpose Vehicles.1.7.2015 EN Official Journal of the European Union L 168/7 Number and position of equivalent sound sources In this method, each vehicle (category 1, 2, 3, 4 and 5) is represented by one single point source radiating uniformly into the 2-π half space above the ground. The first reflection on the road surface is treated implicitly. As depicted in Figure [2.2.a], this point source is placed 0,05 m above the road surface. Figure [2.2.a] Location of equivalent point source on light vehicles (category 1), heavy vehicles (categories 2 and 3) and two-wheelers (category 4) The traffic flow is represented by a source line. In the modelling of a road with multiple lanes, each lane should ideally be represented by a source line placed in the centre of each lane. However, it is also acceptable to model one source line in the middle of a two way road or one source line per carriageway in the outer lane of multi- lane roads. Sound power emission General considerations The sound power of the source is defined in the ‘semi-free field’, thus the sound power includes the effect of the reflection of the ground immediately under the modelled source where there are no disturbing objects in its immediate surroundings except for the reflection on the road surface not immediately under the modelled source. Traffic flow The noise emission of a traffic flow is represented by a source line characterised by its directional sound power per metre per frequency. This corresponds to the sum of the sound emission of the individual vehicles in the traffic flow, taking into account the time spent by the vehicles in the road section considered. The implemen­ tation of the individual vehicle in the flow requires the application of a traffic flow model.L 168/8 EN Official Journal of the European Union 1.7.2015 If a steady traffic flow of Q vehicles of category m per hour is assumed, with an average speed v (in km/h), m m the directional sound power per metre in frequency band i of the source line L is defined by: W′, eq,line,i,m � � Q L ¼L þ10�lg m (2.2.1) W′,eq,line,i,m W,i,m 1 000�v m where L is the directional sound power of a single vehicle. L is expressed in dB (re. 10–12 W/m). These W,i,m W′,m sound power levels are calculated for each octave band i from 125 Hz to 4 kHz. Traffic flow data Q shall be expressed as yearly average per hour, per time period (day-evening-night), per m vehicle class and per source line. For all categories, input traffic flow data derived from traffic counting or from traffic models shall be used. The speed v is a representative speed per vehicle category: in most cases the lower of the maximum legal speed m for the section of road and the maximum legal speed for the vehicle category. If local measurement data is unavailable the maximum legal speed for the vehicle category shall be used. Individual vehicle In the traffic flow, all vehicles of category m are assumed to drive at the same speed, i.e. v , the average speed of m the flow of vehicles of the category. A road vehicle is modelled by a set of mathematical equations representing the two main noise sources: 1. Rolling noise due to the tyre/road interaction; 2. Propulsion noise produced by the driveline (engine, exhaust, etc.) of the vehicle. Aerodynamic noise is incorporated in the rolling noise source. For light, medium and heavy motor vehicles (categories 1, 2 and 3), the total sound power corresponds to the energetic sum of the rolling and the propulsion noise. Thus, the total sound power level of the source lines m = 1, 2 or 3 is defined by: L ðv Þ¼10�lgð10LWR,i,mðvmÞ=10þ10LWP,i,mðvmÞ=10Þ (2.2.2) W,i,m m where L is the sound power level for rolling noise and L is the sound power level for propulsion noise. WR,i,m WP,i,m This is valid on all speed ranges. For speeds less than 20 km/h it shall have the same sound power level as defined by the formula for v = 20 km/h. m For two-wheelers (category 4), only propulsion noise is considered for the source: L (v ) = L (v ) (2.2.3) W,i,m = 4 m = 4 WP,i,m = 4 m = 4 This is valid on all speed ranges. For speeds less than 20 km/h it shall have the same sound power level as defined by the formula for v = 20 km/h. m 2.2.2. Reference conditions The source equations and coefficients are valid for the following reference conditions: — a constant vehicle speed — a flat road — an air temperature τ = 20 °C ref1.7.2015 EN Official Journal of the European Union L 168/9 — a virtual reference road surface, consisting of an average of dense asphalt concrete 0/11 and stone mastic asphalt 0/11, between 2 and 7 years old and in a representative maintenance condition — a dry road surface — no studded tyres. 2.2.3. Rolling noise General equation The rolling noise sound power level in the frequency band i for a vehicle of class m = 1,2 or 3 is defined as: ! v L ¼A þB �lg m þΔL (2.2.4) WR,i,m R,i,m R,i,m v WR,i,m ref The coefficients A and B are given in octave bands for each vehicle category and for a reference speed R,i,m R,i,m v = 70 km/h. ΔL corresponds to the sum of the correction coefficients to be applied to the rolling noise ref WR,i,m emission for specific road or vehicle conditions deviating from the reference conditions: ΔL = ΔL + ΔL + ΔL + ΔL (2.2.5) WR,i,m WR,road,i,m studdedtyres,i,m WR,acc,i,m W,temp ΔL accounts for the effect on rolling noise of a road surface with acoustic properties different from those WR,road,i,m of the virtual reference surface as defined in Chapter 2.2.2. It includes both the effect on propagation and on generation. ΔL is a correction coefficient accounting for the higher rolling noise of light vehicles equipped with studded tyres,i,m studded tyres. ΔL accounts for the effect on rolling noise of a crossing with traffic lights or a roundabout. It integrates WR,acc,i,m the effect on noise of the speed variation. ΔL is a correction term for an average temperature τ different from the reference temperature τ = 20 °C. W,temp ref Correction for studded tyres In situations where a significant number of light vehicles in the traffic flow use studded tyres during several months every year, the induced effect on rolling noise shall be taken into account. For each vehicle of category m = 1 equipped with studded tyres, a speed-dependent increase in rolling noise emission is evaluated by: 8 >>>><a i + b i × lg(50/70) for v < 50 km/h Δ (v) = a + b × lg(v/70) for 50 ≤ v ≤ 90 km/h (2.2.6) stud,i >>>>: i i a + b × lg(90/70) for v > 90 km/h i i where coefficients a and b are given for each octave band. i i The increase in rolling noise emission shall only be attributed according to the proportion of light vehicles with studded tyres and during a limited period T (in months) over the year. If Q is the average ratio of the total s stud,ratio volume of light vehicles per hour equipped with studded tyres during the period T (in months), then the yearly s average proportion of vehicles equipped with studded tyres p is expressed by: s T p ¼Q � s (2.2.7) s stud,ratio 12L 168/10 EN Official Journal of the European Union 1.7.2015 The resulting correction to be applied to the rolling sound power emission due to the use of studded tyres for vehicles of category m = 1 in frequency band i shall be: � � Δstud,i,m¼1 ΔL studdedtyres,i,m¼1 ¼10�lg ð1 − p sÞþp s 10 10 (2.2.8) For vehicles of all other categories no correction shall be applied: ΔL = 0 (2.2.9) studdedtyres,i,m ≠ 1 Effect of air temperature on rolling noise correction The air temperature affects rolling noise emission; the rolling sound power level decreases when the air temperature increases. This effect is introduced in the road surface correction. Road surface corrections are usually evaluated at an air temperature of τ = 20 °C. In the case of a different yearly average air temperature °C, ref the road surface noise shall be corrected by: ΔL (τ) = K × (τ – τ) (2.2.10) W,temp,m m ref The correction term is positive (i.e. noise increases) for temperatures lower than 20 °C and negative (i.e. noise decreases) for higher temperatures. The coefficient K depends on the road surface and the tyre characteristics and in general exhibits some frequency dependence. A generic coefficient K = 0,08 dB/°C for light vehicles m = 1 (category 1) and K = K = 0,04 dB/°C for heavy vehicles (categories 2 and 3) shall be applied for all road m = 2 m = 3 surfaces. The correction coefficient shall be applied equally on all octave bands from 63 to 8 000 Hz. 2.2.4. Propulsion noise General equation The propulsion noise emission includes all contributions from engine, exhaust, gears, air intake, etc. The propulsion noise sound power level in the frequency band i for a vehicle of class m is defined as: ðv − v Þ L ¼A þB � m ref þΔL (2.2.11) WP,i,m P,i,m P,i,m v WP,i,m ref The coefficients A and B are given in octave bands for each vehicle category and for a reference speed P,i,m P,i,m v = 70 km/h. ref ΔL corresponds to the sum of the correction coefficients to be applied to the propulsion noise emission for WP,i,m specific driving conditions or regional conditions deviating from the reference conditions: ΔL = ΔL + ΔL + ΔL (2.2.12) WP,i,m WP,road,i,m WP,grad,i,m WP,acc,i,m ΔL accounts for the effect of the road surface on the propulsion noise via absorption. The calculation WP,road,i,m shall be performed according to Chapter 2.2.6. ΔL and ΔL account for the effect of road gradients and of vehicle acceleration and deceleration at WP,acc,i,m WP,grad,i,m intersections. They shall be calculated according to Chapters 2.2.4 and 2.2.5 respectively. Effect of road gradients The road gradient has two effects on the noise emission of the vehicle: first, it affects the vehicle speed and thus the rolling and propulsion noise emission of the vehicle; second, it affects both the engine load and the engine speed via the choice of gear and thus the propulsion noise emission of the vehicle. Only the effect on the propulsion noise is considered in this section, where a steady speed is assumed.1.7.2015 EN Official Journal of the European Union L 168/11 The effect of the road gradient on the propulsion noise is taken into account by a correction term ΔL WP,grad,m which is a function of the slope s (in %), the vehicle speed v (in km/h) and the vehicle class m. In the case of a m bi-directional traffic flow, it is necessary to split the flow into two components and correct half for uphill and half for downhill. The correction term is attributed to all octave bands equally: For m = 1 8 >>>>>>>>< Minð12 % 1 ; % − sÞ − 6 % for s < – 6 % ΔL (v ) = 0 for – 6 % ≤ s ≤ 2 % (2.2.13) WP,grad,i,m = 1 m >>>>>>>>: Minð12 %;sÞ − 2 % � v m for s > 2 % 1,5 % 100 For m = 2 8 >>>>>>>>< Minð12 0 % ,7; − % sÞ − 4 % �v m 1 − 0 02 0 for s < – 4 % ΔL (v ) = 0 for – 4 % ≤ s ≤ 0 % (2.2.14) WP,grad,i,m = 2 m >>>>>>>>: Min ð12 %;sÞ � v m for s > 0 % 1 % 100 For m = 3 8 >>>>>>>>< Minð12 0 % ,5; − % sÞ − 4 % �v m 1 − 0 01 0 for s < – 4 % ΔL (v ) = 0 for – 4 % ≤ s ≤ 0 % (2.2.15) WP,grad,i,m = 3 m >>>>>>>>: Min ð12 %;sÞ � v m for s > 0 % 0,8 % 100 For m = 4 ΔL = 0 (2.2.16) WP,grad,i,m = 4 The correction ΔL implicitly includes the effect of slope on speed. WP,grad,m 2.2.5. Effect of the acceleration and deceleration of vehicles Before and after crossings with traffic lights and roundabouts a correction shall be applied for the effect of acceleration and deceleration as described below. The correction terms for rolling noise, ΔL , and for propulsion noise, ΔL , are linear functions of the WR,acc,m,k WP,acc,m,k distance x (in m) of the point source to the nearest intersection of the respective source line with another source line. They are attributed to all octave bands equally: jxj ΔL ¼C �Maxð1 − ;0Þ (2.2.17) WR,acc,m,k R,m,k 100 jxj ΔL ¼C �Maxð1 − ;0Þ (2.2.18) WP,acc,m,k P,m,k 100L 168/12 EN Official Journal of the European Union 1.7.2015 The coefficients C and C depend on the kind of junction k (k = 1 for a crossing with traffic lights; k = 2 R,m,k P,m,k for a roundabout) and are given for each vehicle category. The correction includes the effect of change in speed when approaching or moving away from a crossing or a roundabout. Note that at a distance |x| ≥ 100 m, ΔL = ΔL = 0. WR,acc,m,k WP,acc,m,k 2.2.6. Effect of the type of road surface General principles For road surfaces with acoustic properties different from those of the reference surface, a spectral correction term for both rolling noise and propulsion noise shall be applied. The road surface correction term for the rolling noise emission is given by: ! v ΔL ¼α þβ �lg m (2.2.19) WR,road,i,m i,m m v ref where α is the spectral correction in dB at reference speed v for category m (1, 2 or 3) and spectral band i. i,m ref β is the speed effect on the rolling noise reduction for category m (1, 2 or 3) and is identical for all frequency m bands. The road surface correction term for the propulsion noise emission is given by: ΔL = min{α ;0} (2.2.20) WP,road,i,m i,m Absorbing surfaces decrease the propulsion noise, while non-absorbing surfaces do not increase it. Age effect on road surface noise properties The noise characteristics of road surfaces vary with age and the level of maintenance, with a tendency to become louder over time. In this method the road surface parameters are derived to be representative for the acoustic performance of the road surface type averaged over its representative lifetime and assuming proper maintenance. 2.3. Railway noise 2.3.1. Source description Classification of vehicles Definition of vehicle and train For the purposes of this noise calculation method, a vehicle is defined as any single railway sub-unit of a train (typically a locomotive, a self-propelled coach, a hauled coach or a freight wagon) that can be moved independ­ ently and can be detached from the rest of the train. Some specific circumstances may occur for sub-units of a train that are a part of a non-detachable set, e.g. share one bogie between them. For the purpose of this calculation method, all these sub-units are grouped into a single vehicle. For the purpose of this calculation method, a train consists of a series of coupled vehicles.1.7.2015 EN Official Journal of the European Union L 168/13 Table [2.3.a] defines a common language to describe the vehicle types included in the source database. It presents the relevant descriptors to be used to classify the vehicles in full. These descriptors correspond to properties of the vehicle, which affect the acoustic directional sound power per metre length of the equivalent source line modelled. The number of vehicles for each type shall be determined on each of the track sections for each of the time periods to be used in the noise calculation. It shall be expressed as an average number of vehicles per hour, which is obtained by dividing the total number of vehicles travelling in a given time period by the duration in hours of this time period (e.g. 24 vehicles in 4 hours means 6 vehicles per hour). All vehicle types travelling on each track section shall be used. Table [2.3.a] Classification and descriptors for railway vehicles Digit 1 2 3 4 Number of axles per Descriptor Vehicle type Brake type Wheel measure vehicle A letter that describes Explanation of A letter that describes The actual number of A letter that describes the noise reduction the descriptor the type axles the brake type measure type Possible h 1 c n descriptors high speed vehicle cast-iron block no measure (> 200 km/h) m 2 k d self-propelled passen­ composite or sinter dampers ger coaches metal block p 3 n s hauled passenger non-tread braked, screens coaches like disc, drum, mag­ netic c 4 o city tram or light other metro self-propelled and non-self-pro­ pelled coach d etc. diesel loco e electric loco a any generic freight vehicle o other (i.e. mainten­ ance vehicles etc.)L 168/14 EN Official Journal of the European Union 1.7.2015 Classification of tracks and support structure The existing tracks may differ because there are several elements contributing to and characterising their acoustic properties. The track types used in this method are listed in Table [2.3.b] below. Some of the elements have a large influence on acoustic properties, while others have only secondary effects. In general, the most relevant elements influencing the railway noise emission are: railhead roughness, rail pad stiffness, track base, rail joints and radius of curvature of the track. Alternatively, the overall track properties can be defined and, in this case, the railhead roughness and the track decay rate according to ISO 3095 are the two acoustically essential parameters, plus the radius of curvature of the track. A track section is defined as a part of a single track, on a railway line or station or depot, on which the track's physical properties and basic components do not change. Table [2.3.b] defines a common language to describe the track types included in the source database. Table [2.3.b] Digit 1 2 3 4 5 6 Railhead Additional Descriptor Track base Rail pad type Rail joints Curvature Roughness measures Represents an A letter Presence of Indicate the Explanation of Type of track Indicator for indication of describing joints and radius of the descriptor base roughness the ‘acoustic’ acoustic device spacing curvature in m stiffness Codes al­ B E S N N N lowed Ballast Well main­ Soft None None Straight track tained and (150-250 very smooth MN/m) S M M D S L Slab track Normally Medium Rail damper Single joint Low maintained or switch (250 to 800 (1 000- MN/m) 500 m) L N H B D M Ballasted Not well Stiff Low barrier Two joints or Medium bridge maintained switches per (800-1 000 (Less than 100 m MN/m) 500 m and more than 300 m) N B A M H Non-ballasted Not main­ Absorber More than High bridge tained and plate on slab two joints or (Less than bad condi­ track switches per 300 m) tion 100 m T E Embedded Embedded track rail O O Other Other1.7.2015 EN Official Journal of the European Union L 168/15 Number and position of the equivalent sound sources Figure [2.3.a] Equivalent noise sources position The different equivalent noise line sources are placed at different heights and at the centre of the track. All heights are referred to the plane tangent to the two upper surfaces of the two rails. The equivalent sources include different physical sources (index p). These physical sources are divided into different categories depending on the generation mechanism, and are: (1) rolling noise (including not only rail and track base vibration and wheel vibration but also, where present, superstructure noise of the freight vehicles); (2) traction noise; (3) aerodynamic noise; (4) impact noise (from crossings, switches and junctions); (5) squeal noise and (6) noise due to additional effects such as bridges and viaducts. (1) The roughness of wheels and railheads, through three transmission paths to the radiating surfaces (rails, wheels and superstructure), constitutes the rolling noise. This is allocated to h = 0,5 m (radiating surfaces A) to represent the track contribution, including the effects of the surface of the tracks, especially slab tracks (in accordance with the propagation part), to represent the wheel contribution and to represent the contribution of the superstructure of the vehicle to noise (in freight trains). (2) The equivalent source heights for traction noise vary between 0,5 m (source A) and 4,0 m (source B), depending on the physical position of the component concerned. Sources such as gear transmissions and electric motors will often be at an axle height of 0,5 m (source A). Louvres and cooling outlets can be at various heights; engine exhausts for diesel-powered vehicles are often at a roof height of 4,0 m (source B). Other traction sources such as fans or diesel engine blocks may be at a height of 0,5 m (source A) or 4,0 m (source B). If the exact source height is in between the model heights, the sound energy is distributed proportionately over the nearest adjacent source heights. For this reason, two source heights are foreseen by the method at 0,5 m (source A), 4,0 m (source B), and the equivalent sound power associated with each is distributed between the two depending on the specific configuration of the sources on the unit type. (3) Aerodynamic noise effects are associated with the source at 0,5 m (representing the shrouds and the screens, source A), and the source at 4,0 m (modelling all over roof apparatus and pantograph, source B). The choice of 4,0 m for pantograph effects is known to be a simple model, and has to be considered carefully if the objective is to choose an appropriate noise barrier height.L 168/16 EN Official Journal of the European Union 1.7.2015 (4) Impact noise is associated with the source at 0,5 m (source A). (5) Squeal noise is associated with the sources at 0,5 m (source A). (6) Bridge noise is associated with the source at 0,5 m (source A). 2.3.2. Sound power emission General equations Individual vehicle The model for railway traffic noise, analogously to road traffic noise, describes the noise sound power emission of a specific combination of vehicle type and track type which fulfils a series of requirements described in the vehicle and track classification, in terms of a set of sound power per each vehicle (L ). W,0 Traffic flow The noise emission of a traffic flow on each track shall be represented by a set of 2 source lines characterised by its directional sound power per metre per frequency band. This corresponds to the sum of the sound emissions due to the individual vehicles passing by in the traffic flow and, in the specific case of stationary vehicles, taking into account the time spent by the vehicles in the railway section under consideration. The directional sound power per metre per frequency band, due to all the vehicles passing by each track section on the track type (j), is defined: — for each frequency band (i), — for each given source height (h) (for sources at 0,5 m h = 1, at 4,0 m h = 2), and is the energy sum of all contributions from all vehicles running on the specific j-th track section. These contributions are: — from all vehicle types (t) — at their different speeds (s) — under the particular running conditions (constant speed) (c) — for each physical source type (rolling, impact, squeal, traction, aerodynamic and additional effects sources such as for example bridge noise) (p). To calculate the directional sound power per metre (input to the propagation part) due to the average mix of traffic on the j-th track section, the following is used: ! XX L ¼10�lg 10Lw′,eq,line,x=10 (2.3.1) W′,eq,T,dir,i x¼1 where T = reference time period for which the average traffic is considered ref1.7.2015 EN Official Journal of the European Union L 168/17 = total number of existing combinations of i, t, s, c, p for each j-th track section X t = index for vehicle types on the j-th track section s = index for train speed: there are as many indexes as the number of different average train speeds on the j-th track section c = index for running conditions: 1 (for constant speed), 2 (idling) p = index for physical source types: 1 (for rolling and impact noise), 2 (curve squeal), 3 (traction noise), 4 (aerodynamic noise), 5 (additional effects) L = x-th directional sound power per metre for a source line of one combination of t, s, c, p on each W′,eq,line,x j-th track section If a steady flow of Q vehicles per hour is assumed, with an average speed v, on average at each moment in time there will be an equivalent number of Q/v vehicles per unit length of the railway section. The noise emission of the vehicle flow in terms of directional sound power per metre L (expressed in dB/m (re. 10–12 W)) is W′,eq,line integrated by: � � Q L ðψ,φÞ¼L ðψ,φÞþ10�lg (for c = 1) (2.3.2) W′,eq,line,i W,0,dir,i 1 000v where — Q is the average number of vehicles per hour on the j-th track section for vehicle type t, average train speed s and running condition c — v is their speed on the j-th track section for vehicle type t and average train speed s — L is the directional sound power level of the specific noise (rolling, impact, squeal, braking, traction, W,0,dir aerodynamic, other effects) of a single vehicle in the directions ψ, φ defined with respect to the vehicle's direction of movement (see Figure [2.3.b]). In the case of a stationary source, as during idling, it is assumed that the vehicle will remain for an overall time T at a location within a track section with length L. Therefore, with T as the reference time period for the idle ref noise assessment (e.g. 12 hours, 4 hours, 8 hours), the directional sound power per unit length on that track section is defined by: ! T L ðψ,φÞ¼L ðψ,φÞþ10�lg idle (for c = 2) (2.3.4) W′,eq,line,i W,0,dir,i T L ref In general, directional sound power is obtained from each specific source as: L (ψ,φ) = L + ΔL + ΔL (2.3.5) W,0,dir,i W,0,i W,dir,vert,i W,dir,hor,i where — ΔL is the vertical directivity correction (dimensionless) function of ψ (Figure [2.3.b]) W,dir,vert,i — ΔL is the horizontal directivity correction (dimensionless) function of φ (Figure [2.3.b]). W,dir,hor,iL 168/18 EN Official Journal of the European Union 1.7.2015 And where L shall, after being derived in 1/3 octave bands, be expressed in octave bands by energetically W,0,dir,i(ψ,φ) adding each pertaining 1/3 octave band together into the corresponding octave band. Figure [2.3.b] Geometrical definition For the purpose of the calculations, the source strength is then specifically expressed in terms of directional sound power per 1 m length of track L to account for the directivity of the sources in their vertical and W′,tot,dir,i horizontal direction, by means of the additional corrections. Several L (ψ,φ) are considered for each vehicle-track-speed-running condition combination: W,0,dir,i — for a 1/3 octave frequency band (i) — for each track section (j) — source height (h) (for sources at 0,5 m h = 1, at 4,0 m h = 2) — directivity (d) of the source A set of L (ψ,φ) are considered for each vehicle-track-speed-running condition combination, each track W,0,dir,i section, the heights corresponding to h = 1 and h = 2 and the directivity. Rolling noise The vehicle contribution and the track contribution to rolling noise are separated into four essential elements: wheel roughness, rail roughness, vehicle transfer function to the wheels and to the superstructure (vessels) and track transfer function. Wheel and rail roughness represent the cause of the excitation of the vibration at the contact point between the rail and the wheel, and the transfer functions are two empirical or modelled functions that represent the entire complex phenomena of the mechanical vibration and sound generation on the surfaces of the wheel, the rail, the sleeper and the track substructure. This separation reflects the physical evidence that roughness present on a rail may excite the vibration of the rail, but it will also excite the vibration of the wheel and vice versa. Not including one of these four parameters would prevent the decoupling of the classification of tracks and trains. Wheel and rail roughness Rolling noise is mainly excited by rail and wheel roughness in the wavelength range from 5-500 mm.1.7.2015 EN Official Journal of the European Union L 168/19 Definition The roughness level L is defined as 10 times the logarithm to the base 10 of the square of the mean square r value r2 of the roughness of the running surface of a rail or a wheel in the direction of motion (longitudinal level) measured in μm over a certain rail length or the entire wheel diameter, divided by the square of the reference value r2: 0 � � 2 r L ¼10�lg dB (2.3.6) r r 0 where r = 1 μm 0 r = r.m.s. of the vertical displacement difference of the contact surface to the mean level The roughness level L is typically obtained as a spectrum of wavelength λ and it shall be converted to a r frequency spectrum f = v/λ, where f is the centre band frequency of a given 1/3 octave band in Hz, λ is the wavelength in m, and v is the train speed in km/h. The roughness spectrum as a function of frequency shifts along the frequency axis for different speeds. In general cases, after conversion to the frequency spectrum by means of the speed, it is necessary to obtain new 1/3 octave band spectra values averaging between two corresponding 1/3 octave bands in the wavelength domain. To estimate the total effective roughness frequency spectrum corresponding to the appropriate train speed, the two corresponding 1/3 octave bands defined in the wavelength domain shall be averaged energetically and proportionally. The rail roughness level (track side roughness) for the i-th wave-number band is defined as L r,TR,i By analogy, the wheel roughness level (vehicle side roughness) for the i-th wave-number band is defined as L . r,VEH,i The total and effective roughness level for wave-number band i (L ) is defined as the energy sum of the R,tot,i roughness levels of the rail and that of the wheel plus the A3(λ) contact filter to take into account the filtering effect of the contact patch between the rail and the wheel, and is in dB: L ¼10�lgð10Lr,TR,i=10þ10Lr,VEH,i=10ÞþA (2.3.7) R,TOT,i 3,i where expressed as a function of the i-th wave-number band corresponding to the wavelength λ. The contact filter depends on the rail and wheel type and the load. The total effective roughness for the j-th track section and each t-th vehicle type at its corresponding v speed shall be used in the method. Vehicle, track and superstructure transfer function Three speed-independent transfer functions, L L and L , are defined: the first for each j-th track H,TR,i H,VEH,i H,VEH,SUP,i section and the second two for each t-th vehicle type. They relate the total effective roughness level with the sound power of the track, the wheels and the superstructure respectively. The superstructure contribution is considered only for freight wagons, therefore only for vehicle type ‘a’. For rolling noise, therefore, the contributions from the track and from the vehicle are fully described by these transfer functions and by the total effective roughness level. When a train is idling, rolling noise shall be excluded.L 168/20 EN Official Journal of the European Union 1.7.2015 For sound power per vehicle the rolling noise is calculated at axle height, and has as an input the total effective roughness level L as a function of the vehicle speed v, the track, vehicle and superstructure transfer R,TOT,i functions L , L and L , and the total number of axles N: H,TR,i H,VEH,i H,VEH,SUP,i a for h = 1: L = L + L + 10 × lg(N) dB (2.3.8) W,0,TR,i R,TOT,i H,TR,i a L = L + L + 10 × lg(N) dB (2.3.9) W,0,VEH,i R,TOT,i H,VEH,i a L = L + L + 10 × lg(N) dB (2.3.10) W,0,VEHSUP,i R,TOT,i H,VEHSUP,i a where N is the number of axles per vehicle for the t-th vehicle type. a Figure [2.3.c] Scheme of the use of the different roughness and transfer function definitions A minimum speed of 50 km/h (30 km/h only for trams and light metro) shall be used to determine the total effective roughness and therefore the sound power of the vehicles (this speed does not affect the vehicle flow calculation) to compensate for the potential error introduced by the simplification of rolling noise definition, braking noise definition and impact noise from crossings and switches definition. Impact noise (crossings, switches and junctions) Impact noise can be caused by crossings, switches and rail joints or points. It can vary in magnitude and can dominate rolling noise. Impact noise shall be considered for jointed tracks. For impact noise due to switches, crossings and joints in track sections with a speed of less than 50 km/h (30 km/h only for trams and light metro), since the minimum speed of 50 km/h (30 km/h only for trams and light metro) is used to include more effects according to the description of the rolling noise chapter, modelling shall be avoided. Impact noise modelling shall also be avoided under running condition c = 2 (idling). Impact noise is included in the rolling noise term by (energy) adding a supplementary fictitious impact roughness level to the total effective roughness level on each specific j-th track section where it is present. In this case a new L shall be used in place of L and it will then become: R,TOT + IMPACT,i R,TOT,i L ¼10�lgð10LR,TOT,i=10þ10LR,IMPACT,i=10Þ dB (2.3.11) R,TOT þIMPACT,i1.7.2015 EN Official Journal of the European Union L 168/21 L is a 1/3 octave band spectrum (as a function of frequency). To obtain this frequency spectrum, a R,IMPACT,i spectrum is given as a function of wavelength λ and shall be converted to the required spectrum as a function of frequency using the relation λ = v/f, where f is the 1/3 octave band centre frequency in Hz and v is the s-th vehicle speed of the t-th vehicle type in km/h. Impact noise will depend on the severity and number of impacts per unit length or joint density, so in the case where multiple impacts are given, the impact roughness level to be used in the equation above shall be calculated as follows: � � n L ¼L þ10�lg l dB (2.3.12) R,IMPACT,i R, IMPACT − SINGLE,i 0,01 where L is the impact roughness level as given for a single impact and n is the joint density. R,IMPACT–SINGLE,i l The default impact roughness level is given for a joint density n = 0,01 m–1, which is one joint per each 100 m l of track. Situations with different numbers of joints shall be approximated by adjusting the joint density n. It l should be noted that when modelling the track layout and segmentation, the rail joint density shall be taken into account, i.e. it may be necessary to take a separate source segment for a stretch of track with more joints. The L of track, wheel/bogie and superstructure contribution are incremented by means of the L for W,0 R,IMPACT,i +/– 50 m before and after the rail joint. In the case of a series of joints, the increase is extended to between – 50 m before the first joint and + 50 m after the last joint. The applicability of these sound power spectra shall normally be verified on-site. For jointed tracks, a default n of 0,01 shall be used. l Squeal Curve squeal is a special source that is only relevant for curves and is therefore localised. As it can be significant, an appropriate description is required. Curve squeal is generally dependent on curvature, friction conditions, train speed and track-wheel geometry and dynamics. The emission level to be used is determined for curves with radius below or equal to 500 m and for sharper curves and branch-outs of points with radii below 300 m. The noise emission should be specific to each type of rolling stock, as certain wheel and bogie types may be significantly less prone to squeal than others. The applicability of these sound power spectra shall normally be verified on-site, especially for trams. Taking a simple approach, squeal noise shall be considered by adding 8 dB for R < 300 m and 5 dB for 300 m < R < 500 m to the rolling noise sound power spectra for all frequencies. Squeal contribution shall be applied on railway track sections where the radius is within the ranges mentioned above for at least a 50 m length of track. Traction noise Although traction noise is generally specific to each characteristic operating condition amongst constant speed, deceleration, acceleration and idling, the only two conditions modelled are constant speed (that is valid as well when the train is decelerating or when it is accelerating) and idling. The source strength modelled only corresponds to maximum load conditions and this results in the quantities L = L . Also, the L W,0,const,i W,0,idling,i W,0,idling,i corresponds to the contribution of all physical sources of a given vehicle attributable to a specific height, as described in 2.3.1. The L is expressed as a static noise source in the idling position, for the duration of the idling condition, W,0,idling,i and to be used modelled as a fixed point source as described in the following chapter for industrial noise. It shall be considered only if trains are idling for more than 0,5 hours.L 168/22 EN Official Journal of the European Union 1.7.2015 These quantities can either be obtained from measurements of all sources at each operating condition, or the partial sources can be characterised individually, determining their parameter dependency and relative strength. This may be done by means of measurements on a stationary vehicle, by varying shaft speeds of the traction equipment, following ISO 3095:2005. As far as relevant, several traction noise sources have to be characterised which might not be all directly depending on the train speed: — noise from the power train, such as diesel engines (including inlet, exhaust and engine block), gear transmission, electrical generators, mainly dependent on engine round per minute speed (rpm), and electrical sources such as converters, which may be mostly load-dependent, — noise from fans and cooling systems, depending on fan rpm; in some cases fans can be directly coupled to the driveline, — intermittent sources such as compressors, valves and others with a characteristic duration of operation and corresponding duty cycle correction for the noise emission. As each of these sources can behave differently at each operating condition, the traction noise shall be specified accordingly. The source strength is obtained from measurements under controlled conditions. In general, locomotives will tend to show more variation in loading as the number of vehicles hauled and thereby the power output can vary significantly, whereas fixed train formations such as electric motored units (EMUs), diesel motored units (DMUs) and high-speed trains have a better defined load. There is no a priori attribution of the source sound power to the source heights, and this choice shall depend on the specific noise and vehicle assessed. It shall be modelled to be at source A (h = 1) and at source B (h = 2). Aerodynamic noise Aerodynamic noise is only relevant at high speeds above 200 km/h and therefore it should first be verified whether it is actually necessary for application purposes. If the rolling noise roughness and transfer functions are known, it can be extrapolated to higher speeds and a comparison can be made with existing high-speed data to check whether higher levels are produced by aerodynamic noise. If train speeds on a network are above 200 km/h but limited to 250 km/h, in some cases it may not be necessary to include aerodynamic noise, depending on the vehicle design. The aerodynamic noise contribution is given as a function of speed: � � v L ¼L ðv Þþα �lg dB For h = 1 (2.3.13) W,0,i W,0,1,i 0 1,i v 0 � � v L ¼L ðv Þþα �lg dB For h = 2 (2.3.14) W,0,i W,0,2,i 0 2,i v 0 where v is a speed at which aerodynamic noise is dominant and is fixed at 300 km/h 0 L is a reference sound power determined from two or more measurement points, for sources at known W,0,1,i source heights, for example the first bogie L is a reference sound power determined from two or more measurement points, for sources at known W,0,2,i source heights, for example the pantograph recess heights α is a coefficient determined from two or more measurement points, for sources at known source heights, for 1,i example the first bogie α is a coefficient determined from two or more measurement points, for sources at known source heights, for 2,i example the pantograph recess heights.1.7.2015 EN Official Journal of the European Union L 168/23 Source directivity The horizontal directivity ΔL in dB is given in the horizontal plane and by default can be assumed to W,dir,hor,i be a dipole for rolling, impact (rail joints etc.), squeal, braking, fans and aerodynamic effects, given for each i-th frequency band by: ΔL = 10 × lg(0,01 + 0,99 · sin2φ) (2.3.15) W,dir,hor,i The vertical directivity ΔL in dB is given in the vertical plane for source A (h = 1), as a function of the W,dir,ver,i centre band frequency f of each i-th frequency band, and for – π/2 < ψ < π/2 by: c,i �� � � � ��� ΔL W,dir,ver,i ¼ � � �4 30 � 2 3�sinð2�ψÞ − sinψ �lg f c,i 2þ 00600 � � � (2.3.16) For source B (h = 2) for the aerodynamic effect: ΔL = 10 × lg(cos2ψ) for ψ < 0 (2.3.17) W,dir,ver,i ΔL = 0 elsewhere W,dir,ver,i Directivity ΔL is not considered for source B (h = 2) for other effects, as omni-directionality is assumed for dir,ver,i these sources in this position. 2.3.3. Additional effects Correction for structural radiation (bridges and viaducts) In the case where the track section is on a bridge, it is necessary to consider the additional noise generated by the vibration of the bridge as a result of the excitation caused by the presence of the train. Because it is not simple to model the bridge emission as an additional source, given the complex shapes of bridges, an increase in the rolling noise is used to account for the bridge noise. The increase shall be modelled exclusively by adding a fixed increase in the noise sound power per each third octave band. The sound power of only the rolling noise is modified when considering the correction and the new L shall be used instead of L : W,0,rolling–and–bridge,i W,0,rolling-only,i L = L + C dB (2.3.18) W,0,rolling–and–bridge,i W,0,rolling–only,i bridge where C is a constant that depends on the bridge type, and L is the rolling noise sound power on bridge W,0,rolling–only,i the given bridge that depends only on the vehicle and track properties. Correction for other railway-related noise sources Various sources like depots, loading/unloading areas, stations, bells, station loudspeakers, etc. can be present and are associated with the railway noise. These sources are to be treated as industrial noise sources (fixed noise sources) and shall be modelled, if relevant, according to the following chapter for industrial noise. 2.4. Industrial noise 2.4.1. Source description Classification of source types (point, line, area) The industrial sources are of very variable dimensions. They can be large industrial plants as well as small concentrated sources like small tools or operating machines used in factories. Therefore, it is necessary to use an appropriate modelling technique for the specific source under assessment. Depending on the dimensions and the way several single sources extend over an area, with each belonging to the same industrial site, these may be modelled as point sources, source lines or area sources. In practice, the calculations of the noise effect are always based on point sources, but several point sources can be used to represent a real complex source, which mainly extends over a line or an area.L 168/24 EN Official Journal of the European Union 1.7.2015 Number and position of equivalent sound sources The real sound sources are modelled by means of equivalent sound sources represented by one or more point sources so that the total sound power of the real source corresponds to the sum of the single sound powers attributed to the different point sources. The general rules to be applied in defining the number of point sources to be used are: — line or surface sources where the largest dimension is less than 1/2 of the distance between the source and the receiver can be modelled as single point sources, — sources where the largest dimension is more than 1/2 of the distance between the source and the receiver should be modelled as a series of incoherent point sources in a line or as a series of incoherent point sources over an area, such that for each of these sources the condition of 1/2 is fulfilled. The distribution over an area can include vertical distribution of point sources, — for sources where the largest dimensions in height are over 2 m or near the ground, special care should be administered to the height of the source. Doubling the number of sources, redistributing them only in the z-component, may not lead to a significantly better result for this source, — in the case of any source, doubling the number of sources over the source area (in all dimensions) may not lead to a significantly better result. The position of the equivalent sound sources cannot be fixed, given the large number of configurations that an industrial site can have. Best practices will normally apply. Sound power emission General The following information constitutes the complete set of input data for sound propagation calculations with the methods to be used for noise mapping: — Emitted sound power level spectrum in octave bands — Working hours (day, evening, night, on a yearly averaged basis) — Location (coordinates x, y) and elevation (z) of the noise source — Type of source (point, line, area) — Dimensions and orientation — Operating conditions of the source — Directivity of the source. The point, line and area source sound power are required to be defined as: — For a point source, sound power L and directivity as a function of the three orthogonal coordinates (x, y, z); W — Two types of source lines can be defined: — source lines representing conveyor belts, pipe lines, etc., sound power per metre length L and directivity as W′ a function of the two orthogonal coordinates to the axis of the source line,1.7.2015 EN Official Journal of the European Union L 168/25 — source lines representing moving vehicles, each associated with sound power L and directivity as a function W of the two orthogonal coordinates to the axis of the source line and sound power per metre L derived by W′ means of the speed and number of vehicles travelling along this line during day, evening and night; The correction for the working hours, to be added to the source sound power to define the corrected sound power that is to be used for calculations over each time period, C in dB is calculated as follows: W � � l �n C ¼ − 10lg (2.4.1) W 1 000�V �T 0 Where: V Speed of the vehicle [km/h]; n Number of vehicles passages per period [-]; l Total length of the source [m]. — For an area source, sound power per square metre L , and no directivity (may be horizontal or vertical). W/m2 The working hours are an essential input for the calculation of noise levels. The working hours shall be given for the day, evening and night period and, if the propagation is using different meteorological classes defined during each of the day, night and evening periods, then a finer distribution of the working hours shall be given in sub-periods matching the distribution of meteorological classes. This information shall be based on a yearly average. The correction for the working hours, to be added to the source sound power to define the corrected sound power that shall be used for calculations over each time period, C in dB is calculated as follows: W ! T C ¼10�lg (2.4.2) W T ref where T is the active source time per period based on a yearly averaged situation, in hours; T is the reference period of time in hours (e.g. day is 12 hours, evening is 4 hours, night is 8 hours). ref For the more dominant sources, the yearly average working hours correction shall be estimated at least within 0,5 dB tolerance in order to achieve an acceptable accuracy (this is equivalent to an uncertainty of less than 10 % in the definition of the active period of the source). Source directivity The source directivity is strongly related to the position of the equivalent sound source next to nearby surfaces. Because the propagation method considers the reflection of the nearby surface as well its sound absorption, it is necessary to consider carefully the location of the nearby surfaces. In general, these two cases will always be distinguished: — a source sound power and directivity is determined and given relative to a certain real source when this is in free field (excluding the terrain effect). This is in agreement with the definitions concerning the propagation, if it is assumed that there is no nearby surface less than 0,01 m from the source and surfaces at 0,01 m or more are included in the calculation of the propagation,L 168/26 EN Official Journal of the European Union 1.7.2015 — a source sound power and directivity is determined and given relative to a certain real source when this is placed in a specific location and therefore the source sound power and directivity is in fact an ‘equivalent’ one, since it includes the modelling of the effect of the nearby surfaces. This is defined in ‘semi-free field’ according to the definitions concerning the propagation. In this case, the nearby surfaces modelled shall be excluded from the calculation of propagation. The directivity shall be expressed in the calculation as a factor ΔL (x, y, z) to be added to the sound power W,dir,xyz to obtain the right directional sound power of a reference sound source seen by the sound propagation in the direction given. The factor can be given as a function of the direction vector defined by (x,y,z) with qffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi x2þy2þz2 ¼1. This directivity can also be expressed by means of other coordinate systems such as angular coordinate systems. 2.5. Calculation of noise propagation for road, railway, industrial sources. 2.5.1. Scope and applicability of the method This document specifies a method for calculating the attenuation of noise during its outdoor propagation. Knowing the characteristics of the source, this method predicts the equivalent continuous sound pressure level at a receiver point corresponding to two particular types of atmospheric conditions: — downward-refraction propagation conditions (positive vertical gradient of effective sound celerity) from the source to the receiver, — homogeneous atmospheric conditions (null vertical gradient of effective sound celerity) over the entire area of propagation. The method of calculation described in this document applies to industrial infrastructures and land transport infrastructures. It therefore applies in particular to road and railway infrastructures. Aircraft transport is included in the scope of the method only for the noise produced during ground operations and excludes take- off and landing. Industrial infrastructures that emit impulsive or strong tonal noises as described in ISO 1996-2:2007 do not fall within the scope of this method. The method of calculation does not provide results in upward-refraction propagation conditions (negative vertical gradient of effective sound speed) but these conditions are approximated by homogeneous conditions when computing L . den To calculate the attenuation due to atmospheric absorption in the case of transport infrastructure, the temperature and humidity conditions are calculated according to ISO 9613-1:1996. The method provides results per octave band, from 63 Hz to 8 000 Hz. The calculations are made for each of the centre frequencies. Partial covers and obstacles sloping, when modelled, more than 15° in relation to the vertical are out of the scope of this calculation method. A single screen is calculated as a single diffraction calculation, two or more screens in a single path are treated as a subsequent set of single diffractions by applying the procedure described further. 2.5.2. Definitions used All distances, heights, dimensions and altitudes used in this document are expressed in metres (m). The notation MN stands for the distance in 3 dimensions (3D) between the points M and N, measured according to a straight line joining these points. The notation M^ N stands for the curved path length between the points M and N, in favourable conditions.1.7.2015 EN Official Journal of the European Union L 168/27 It is customary for real heights to be measured vertically in a direction perpendicular to the horizontal plane. Heights of points above the local ground are denoted h, absolute heights of points and absolute height of the ground are to be noted by the letter H. To take into account the actual relief of the land along a propagation path, the notion of ‘equivalent height’ is introduced, to be noted by the letter z. This substitutes real heights in the ground effect equations. The sound levels, noted by the capital letter L, are expressed in decibels (dB) per frequency band when index A is omitted. The sound levels in decibels dB(A) are given the index A. The sum of the sound levels due to mutually incoherent sources is noted by the sign � in accordance with the following definition: (2.5.1) 2.5.3. Geometrical considerations Source segmentation Real sources are described by a set of point sources or, in the case of railway traffic or road traffic, by incoherent source lines. The propagation method assumes that line or area sources have previously been split up to be represented by a series of equivalent point sources. This may have occurred as pre-processing of the source data, or may occur within the pathfinder component of the calculation software. The means by which this has occurred is outside the scope of the current methodology. Propagation paths The method operates on a geometrical model consisting of a set of connected ground and obstacles surfaces. A vertical propagation path is deployed on one or more vertical planes with respect to the horizontal plane. For trajectories including reflections onto vertical surfaces not orthogonal to the incident plane, another vertical plane is subsequently considered including the reflected part of the propagation path. In these cases, where more vertical planes are used to describe the entire trajectory from the source to the receiver, the vertical planes are then flattened, like an unfolding Chinese screen. Significant heights above the ground The equivalent heights are obtained from the mean ground plane between the source and the receiver. This replaces the actual ground with a fictitious plane representing the mean profile of the land. Figure 2.5.a Equivalent heights in relation to the ground 1: Actual relief 2: Mean planeL 168/28 EN Official Journal of the European Union 1.7.2015 The equivalent height of a point is its orthogonal height in relation to the mean ground plane. The equivalent source height z and the equivalent receiver height z can therefore be defined. The distance between the source s r and receiver in projection over the mean ground plane is noted by d. p If the equivalent height of a point becomes negative, i.e. if the point is located below the mean ground plane, a null height is retained, and the equivalent point is then identical with its possible image. Calculation of the mean plane In the plane of the path, the topography (including terrain, mounds, embankments and other man- made obstacles, buildings, …) may be described by an ordered set of discrete points (x, H); k є {1,…,n}. This set k k of points defines a polyline, or equivalently, a sequence of straight segments H = ax + b, x є [x, x ]; k є k k k k k + 1 {1,…n}, where: 8 <a = (H – H)/(x – x) k k + 1 k k + 1 k (2.5.2) : b = (H · x – H · x)/(x – x) k k k + 1 k + 1 k k + 1 k The mean plane is represented by the straight line Z = ax + b; x є [x , x], which is adjusted to the polyline by 1 n means of a least-square approximation. The equation of the mean line can be worked out analytically. Using: 8 >>>>>>><A¼2 3Xn − 1 a kðx3 kþ1 − x3 kÞþXn − 1 b kðx2 kþ1 − x2 kÞ k¼1 k¼1 (2.5.3) >>>>>>>:B¼Xn − 1 a kðx2 kþ1 − x2 kÞþ2Xn − 1 b kðx kþ1 − x kÞ k¼1 k¼1 The coefficients of the straight line are given by: 8 >>>>><a¼3ð2A ð − x B −ð x xn Þþ 3 x 1ÞÞ n 1 (2.5.4) >>>>>:b¼2ðx3 n − x3 1Þ B − 3ðx nþx 1Þ A ðx − x Þ4 ðx − x Þ3 n 1 n 1 Where segments with x = x shall be ignored when evaluating eq. 2.5.3. k + 1 k Reflections by building façades and other vertical obstacles Contributions from reflections are taken into account by the introduction of image sources as described further. 2.5.4. Sound propagation model For a receiver R the calculations are made according to the following steps: (1) on each propagation path: — calculation of the attenuation in favourable conditions, — calculation of the attenuation in homogeneous conditions, — calculation of the long-term sound level for each path;1.7.2015 EN Official Journal of the European Union L 168/29 (2) accumulation of the long-term sound levels for all paths affecting a specific receiver, therefore allowing the total sound level to be calculated at the receiver point. It should be noted that only the attenuations due to the ground effect (A ) and diffraction (A ) are affected ground dif by meteorological conditions. 2.5.5. Calculation process For a point source S of directional sound power L and for a given frequency band, the equivalent w,0,dir continuous sound pressure level at a receiver point R in given atmospheric conditions is obtained according to the equations following below. Sound level in favourable conditions (L ) for a path (S,R) F L = L – A (2.5.5) F W,0,dir F The term A represents the total attenuation along the propagation path in favourable conditions, and is broken F down as follows: L = A + A + A (2.5.6) F div atm boundary,F where A is the attenuation due to geometrical divergence; div A is the attenuation due to atmospheric absorption; atm A is the attenuation due to the boundary of the propagation medium in favourable conditions. It may boundary,F contain the following terms: A which is the attenuation due to the ground in favourable conditions; ground,F A which is the attenuation due to diffraction in favourable conditions. dif,F For a given path and frequency band, the following two scenarios are possible: — either A is calculated with no diffraction (A = 0 dB) and A = A ; ground,F dif,F boundary,F ground,F — or A is calculated. The ground effect is taken into account in the A equation itself (A = 0 dB). This dif,F dif,F ground,F therefore gives A = A . boundary,F dif,F Sound level in homogeneous conditions (L ) for a path (S,R) H The procedure is strictly identical to the case of favourable conditions presented in the previous section. L = L – A (2.5.7) H W,0,dir H The term A represents the total attenuation along the propagation path in homogeneous conditions and is H broken down as follows: A = A + A + A (2.5.8) H div atm boundary,HL 168/30 EN Official Journal of the European Union 1.7.2015 where A is the attenuation due to geometrical divergence; div Α is the attenuation due to atmospheric absorption; atm A is the attenuation due to the boundary of the propagation medium in homogeneous conditions. It may boundary,H contain the following terms: Α which is the attenuation due to the ground in homogeneous conditions; ground,H A which is the attenuation due to diffraction in homogeneous conditions. dif,H For a given path and frequency band, the following two scenarios are possible: — either Α (A = 0 dB) is calculated with no diffraction and A = Α ; ground,H dif,H boundary,H ground,H — or A (Α = 0 dB) is calculated. The ground effect is taken into account in the A equation itself. dif,H ground,H dif,H This therefore gives A = A boundary,H dif,H Statistical approach inside urban areas for a path (S,R) Inside urban areas, a statistical approach to the calculation of the sound propagation behind the first line of buildings is also allowed, provided that such a method is duly documented, including relevant information on the quality of the method. This method may replace the calculation of the A and A by an approxi­ boundary,H boundary,F mation of the total attenuation for the direct path and all reflections. The calculation will be based on the average building density and the average height of all buildings in the area. Long-term sound level for a path (S,R) The ‘long-term’ sound level along a path starting from a given point source is obtained from the logarithmic sum of the weighted sound energy in homogeneous conditions and the sound energy in favourable conditions. These sound levels are weighted by the mean occurrence p of favourable conditions in the direction of the path (S,R): � � LF LH L LT ¼10�lg p�1010þð1 − pÞ�1010 (2.5.9) NB: The occurrence values for p are expressed in percentages. So for example, if the occurrence value is 82 %, equation (2.5.9) would have p = 0,82. Long-term sound level at point R for all paths The total long-term sound level at the receiver for a frequency band is obtained by energy summing contri­ butions from all N paths, all types included: ! X Ln,LT L tot,LT ¼10�lg 10 10 (2.5.10) n where n is the index of the paths between S and R.1.7.2015 EN Official Journal of the European Union L 168/31 Taking reflections into account by means of image sources is described further. The percentage of occurrences of favourable conditions in the case of a path reflected on a vertical obstacle is taken to be identical to the occurrence of the direct path. If S′ is the image source of S, then the occurrence p′ of the path (S′,R) is taken to be equal to the occurrence p of the path (S,R). i Long-term sound level at point R in decibels A (dBA) The total sound level in decibels A (dBA) is obtained by summing levels in each frequency band: X L Aeq,LT ¼10�lg 10ðLtot,LT,iþAWCf,iÞ=10 (2.5.11) i where i is the index of the frequency band. AWC is the A-weighting correction according to the international standard IEC 61672-1:2003. This level L constitutes the final result, i.e. the long-term A-weighted sound pressure level at the receiver Aeq,LT point on a specific reference time interval (e.g. day or evening, or night or a shorter time during day, evening or night). 2.5.6. Calculation of noise propagation for road, railway, industrial sources. Geometrical divergence The attenuation due to geometrical divergence, A , corresponds to a reduction in the sound level due to the div propagation distance. For a point sound source in free field, the attenuation in dB is given by: A = 20 × lg(d) + 11 (2.5.12) div where d is the direct 3D slant distance between the source and the receiver. Atmospheric absorption The attenuation due to atmospheric absorption A during propagation over a distance d is given in dB by the atm equation: A = α · d/1 000 (2.5.13) atm atm where d is the direct 3D slant distance between the source and the receiver in m; α is the atmospheric attenuation coefficient in dB/km at the nominal centre frequency for each frequency atm band, in accordance with ISO 9613-1. The values of the α coefficient are given for a temperature of 15 °C, a relative humidity of 70 % and an atm atmospheric pressure of 101 325 Pa. They are calculated with the exact centre frequencies of the frequency band. These values comply with ISO 9613-1. Meteorological average over the long term shall be used if meteor­ ological data is available.L 168/32 EN Official Journal of the European Union 1.7.2015 Ground effect The attenuation due to the ground effect is mainly the result of the interference between the reflected sound and the sound that is propagated directly from the source to the receiver. It is physically linked to the acoustic absorption of the ground above which the sound wave is propagated. However, it is also significantly dependent on atmospheric conditions during propagation, as ray bending modifies the height of the path above the ground and makes the ground effects and land located near the source more or less significant. In case the propagation between the source and the receiver is affected by any obstacle in the propagation plane, the ground effect is calculated separately on the source and receiver side. In this case, z and z refer to s r the equivalent source and/or receiver position as indicated further where the calculation of the diffraction A is dif presented. Acoustic characterisation of ground The acoustic absorption properties of the ground are mainly linked to its porosity. Compact ground is generally reflective and porous ground is absorbent. For operational calculation requirements, the acoustic absorption of a ground is represented by a dimensionless coefficient G, between 0 and 1. G is independent of the frequency. Table 2.5.a gives the G values for the ground outdoors. In general, the average of the coefficient G over a path takes values between 0 and 1. Table 2.5.a G values for different types of ground Description Type (kPa · s/m2) G value Very soft (snow or moss-like) A 12,5 1 Soft forest floor (short, dense heather-like B 31,5 1 or thick moss) Uncompacted, loose ground (turf, grass, C 80 1 loose soil) Normal uncompacted ground (forest floors, D 200 1 pasture field) Compacted field and gravel (compacted E 500 0,7 lawns, park area) Compacted dense ground (gravel road, car F 2 000 0,3 park) Hard surfaces (most normal asphalt, con­ G 20 000 0 crete) Very hard and dense surfaces (dense as­ H 200 000 0 phalt, concrete, water) G is defined as the fraction of absorbent ground present over the entire path covered. path1.7.2015 EN Official Journal of the European Union L 168/33 When the source and receiver are close-by so that d ≤ 30(z + z), the distinction between the type of ground p s r located near the source and the type of ground located near the receiver is negligible. To take this comment into account, the ground factor G is therefore ultimately corrected as follows: path 8 � � >>< G d p þG 1 − d p if d ≤ 30(z + z) G′ path = >>: path30ðz sþz rÞ s 30ðz sþz rÞ p s r (2.5.14) G otherwise path where G is the ground factor of the source area. G = 0 for road platforms (1), slab tracks. G = 1 for rail tracks s s s on ballast. There is no general answer in the case of industrial sources and plants. G may be linked to the flow resistivity. Figure 2.5.b Determination of the ground coefficient G over a propagation path path The following two subsections on calculations in homogeneous and favourable conditions introduce the generic G and G notations for the absorption of the ground. Table 2.5.b gives the correspondence between these w m notations and the G and G′ variables. path path Table 2.5.b Correspondence between G and G and (G , G′ ) w m path path Homogeneous conditions Favourable conditions A Δ Δ A Δ Δ ground ground(S,O) ground(O,R) ground ground(S,O) ground(O,R) G G′ G w path path G G′ G G′ G m path path path path (1) The absorption of porous road pavements is taken into account in the emission model.L 168/34 EN Official Journal of the European Union 1.7.2015 Calculations in homogeneous conditions The attenuation due to the ground effect in homogeneous conditions is calculated according to the following equations: if G ≠ 0 path " rffiffiffiffiffiffiffi ! rffiffiffiffiffiffiffi !# ! A ¼max − 10�lg 4k2 z2 − 2C fz þC f z2 − 2C fz þC f ,A (2.5.15) ground,H d2 s k s k r k r k ground,H,min p where fm is the nominal centre frequency of the frequency band considered, in Hz, c is the speed of the sound in the air, taken as equal to 340 m/s, and C is defined by: f pffiffiffiffiffi 1þ3wd e − wdp C ¼d p (2.5.16) f p 1þwd p where the values of w are given by the equation below: (2.5.17) G may be equal to either G or G′ depending on whether the ground effect is calculated with or without w path path diffraction, and according to the nature of the ground under the source (real source or diffracted). This is specified in the following subsections and summarised in Table 2.5.b. (2.5.18) is the lower bound of A . ground,H For a path (S,R) in homogeneous conditions without diffraction: i G = G′ w path G = G′ m path With diffraction, refer to the section on diffraction for the definitions of G and G . w m if G = 0: A = – 3 dB path ground,H The term – 3(1 – G ) takes into account the fact that when the source and the receiver are far apart, the first m reflection source side is no longer on the platform but on natural land.1.7.2015 EN Official Journal of the European Union L 168/35 Calculation in favourable conditions The ground effect in favourable conditions is calculated with the equation of A , provided that the following ground,H modifications are made: If G ≠ 0 path (a) In the equation of A , the heights z and z are replaced by z + δ z + δ z and z + δ z + δ z respectively ground,H s r s s T r r T where 8 � � >>>>>><δz s ¼a 0 z þz s z 2d 22 p s r (2.5.19) >>>>>>:δz ¼a � z r � 2d2 p r 0 z þz 2 s r a =2 × 10–4 m–1 is the reverse of the radius of curvature o d δz ¼6�10 − 3 p T z þz s r (b) The lower bound of A depends on the geometry of the path: ground,F (2.5.20) If G = 0 path A = A ground,F ground,F,min The height corrections δ z and δ z convey the effect of the sound ray bending. δ z accounts for the effect of s r T the turbulence. G may also be equal to either G or G′ depending on whether the ground effect is calculated with or m path path without diffraction, and according to the nature of the ground under the source (real source or diffracted). This is specified in the following subsections. For a path (S,R) in favourable conditions without diffraction: i G = G in equation (2.5.17); w path G = G′ . m path With diffraction, refer to the next section for the definitions of G and G . w m Diffraction As a general rule, the diffraction shall be studied at the top of each obstacle located on the propagation path. If the path passes ‘high enough’ over the diffraction edge, A = 0 can be set and a direct view calculated, in dif particular by evaluating A . groundL 168/36 EN Official Journal of the European Union 1.7.2015 In practice, for each frequency band centre frequency, the path difference δ is compared with the quantity – λ/20. If an obstacle does not produce diffraction, this for instance being determined according to Rayleigh's criterion, there is no need to calculate A for the frequency band considered. In other words, A = 0 in this dif dif case. Otherwise, A is calculated as described in the remainder of this part. This rule applies in both dif homogeneous and favourable conditions, for both single and multiple diffraction. When, for a given frequency band, a calculation is made according to the procedure described in this section, A is set as equal to 0 dB when calculating the total attenuation. The ground effect is taken into account ground directly in the general diffraction calculation equation. The equations proposed here are used to process the diffraction on thin screens, thick screens, buildings, earth berms (natural or artificial), and by the edges of embankments, cuttings and viaducts. When several diffracting obstacles are encountered on a propagation path, they are treated as a multiple diffraction by applying the procedure described in the following section on calculation of the path difference. The procedures presented here are used to calculate the attenuations in both homogeneous conditions and favourable conditions. Ray bending is taken into account in the calculation of the path difference and to calculate the ground effects before and after diffraction. General principles Figure 2.5.c illustrates the general method of calculation of the attenuation due to diffraction. This method is based on breaking down the propagation path into two parts: the ‘source side’ path, located between the source and the diffraction point, and the ‘receiver side’ path, located between the diffraction point and the receiver. The following are calculated: — a ground effect, source side, Δ ground(S,O) — a ground effect, receiver side, Δ ground(O,R) — and three diffractions: — between the source S and the receiver R: Δ dif(S,R) — between the image source S′ and R: Δ dif(S′,R) — between S and the image receiver R′: Δ . dif(S,R′) Figure 2.5.c Geometry of a calculation of the attenuation due to diffraction 1: Source side 2: Receiver side1.7.2015 EN Official Journal of the European Union L 168/37 where S is the source; R is the receiver; S′ is the image source in relation to the mean ground plane source side; R′ is the image receiver in relation to the mean ground plane receiver side; O is the diffraction point; z is the equivalent height of the source S in relation to the mean plane source side; s z is the equivalent height of the diffraction point O in relation to the mean ground plane source side; o,s z is the equivalent height of the receiver R in relation to the mean plane receiver side; r z is the equivalent height of the diffraction point O in relation to the mean ground plane receiver side. o,r The irregularity of the ground between the source and the diffraction point, and between the diffraction point and the receiver, is taken into account by means of equivalent heights calculated in relation to the mean ground plane, source side first and receiver side second (two mean ground planes), according to the method described in the subsection on significant heights above the ground. Pure diffraction For pure diffraction, with no ground effects, the attenuation is given by: 8 � � >>>< 10C �lg 3þ40 C″δ if 40 C″δ� − 2 h λ λ Δ = (2.5.21) dif >>>: 0 otherwise where C = 1 (2.5.22) h λ is the wavelength at the nominal centre frequency of the frequency band considered; δ is the path difference between the diffracted path and the direct path (see next subsection on calculation of the path difference); C″ is a coefficient used to take into account multiple diffractions: C″ = 1 for a single diffraction. For a multiple diffraction, if e is the total distance along the path, O1 to O2 + O2 to O3 + O3 to O4 from the ‘rubber band method’, (see Figures 2.5.d and 2.5.f) and if e exceeds 0,3 m (otherwise C″ = 1), this coefficient is defined by: (2.5.23)L 168/38 EN Official Journal of the European Union 1.7.2015 The values of Δ shall be bound: dif — if Δ < 0: Δ = 0 dB dif dif — if Δ > 25: Δ = 25 dB for a diffraction on a horizontal edge and only on the term Δ which figures in the dif dif dif calculation of A . This upper bound shall not be applied in the Δ terms that intervene in the calculation of dif dif Δ , or for a diffraction on a vertical edge (lateral diffraction) in the case of industrial noise mapping. ground Calculation of the path difference The path difference δ is calculated in a vertical plane containing the source and the receiver. This is an approxi­ mation in relation to the Fermat principle. The approximation remains applicable here (source lines). The path difference δ is calculated as in the following Figures, based on the situations encountered. Homogeneous conditions Figure 2.5.d Calculation of the path difference in homogeneous conditions. O, O , and O are the diffraction points 1 2 Note: For each configuration, the expression of δ is given. Favourable conditions Figure 2.5.e Calculation of the path difference in favourable conditions (single diffraction)1.7.2015 EN Official Journal of the European Union L 168/39 In favourable conditions, it is considered that the three curved sound rays SO, OR, and SR have an identical radius of curvature Γ defined by: Γ = max(1 000,8d) (2.5.24) The length of a sound ray curve MN is noted M^N in favourable conditions. This length is equal to: (2.5.25) In principle, three scenarios should be considered in the calculation of the path difference in favourable conditions δ (see Figure 2.5.e). In practice, two equations are sufficient: F — if the straight sound ray SR is masked by the obstacle (1st and 2nd case in Figure 2.5.e): (2.5.26) — if the straight sound ray SR is not masked by the obstacle (3rd case in Figure 2.5.e): (2.5.27) where A is the intersection of the straight sound ray SR and the extension of the diffracting obstacle. For the multiple diffractions in favourable conditions: — determine the convex hull defined by the various potential diffraction edges; — eliminate the diffraction edges which are not on the boundary of the convex hull; — calculate δ based on the lengths of the curved sound ray, by breaking down the diffracted path into as F many curved segments as necessary (see Figure 2.5.f) (2.5.28) Figure 2.5.f Example of calculation of the path difference in favourable conditions, in the case of multiple diffractionsL 168/40 EN Official Journal of the European Union 1.7.2015 In the scenario presented in Figure 2.5.f, the path difference is: (2.5.29) Calculation of the attenuation A dif The attenuation due to diffraction, taking the ground effects on the source side and receiver side into account, is calculated according to the following general equations: A ¼Δ þΔ þΔ (2.5.30) dif dif ðS,RÞ ground ðS,OÞ ground ðOn ,RÞ where — Δ is the attenuation due to the diffraction between the source S and the receiver R dif (S,R) — Δ is the attenuation due to the ground effect on the source side, weighted by the diffraction on the ground(S,O) source side; where it is understood that O = O in case of multiple diffractions as in Figure 2.5.f 1 — Δ is the attenuation due to the ground effect on the receiver side, weighted by the diffraction on the ground(O,R) receiver side (see the following subsection on calculation of the term Δ ). ground(O,R) Calculation of the term Δ ground(S,O) (2.5.31) where — A is the attenuation due to the ground effect between the source S and the diffraction point O. This ground(S,O) term is calculated as indicated in the previous subsection on calculations in homogeneous conditions and in the previous subsection on calculation in favourable conditions, with the following hypotheses: z = z , r o,s — G is calculated between S and O, path — In homogeneous conditions: G = G′ in equation (2.5.17), G = G′ in equation (2.5.18), w path m path — In favourable conditions: G = G in equation (2.5.17), G = G′ in equation (2.5.20), w path m path — Δ is the attenuation due to the diffraction between the image source S′ and R, calculated as in the dif(S′,R) previous subsection on pure diffraction, — Δ is the attenuation due to the diffraction between S and R, calculated as in Subsection VI.4.4.b. dif(S,R) Calculation of the term Δ ground(O,R) (2.5.32) where — A is the attenuation due to the ground effect between the diffraction point O and the receiver R. This ground (O,R) term is calculated as indicated in the previous subsection on calculation in homogeneous conditions and in the previous subsection on calculation in favourable conditions, with the following hypotheses: z = z s o,r — G is calculated between O and R. path1.7.2015 EN Official Journal of the European Union L 168/41 The G′ correction does not need to be taken into account here as the source considered is the diffraction path point. Therefore, G shall indeed be used in the calculation of ground effects, including for the lower bound path term of the equation which becomes – 3(1 – G ). path — In homogeneous conditions, G = G in equation (2.5.17) and G = G in equation (2.5.18); w path m path — In favourable conditions, G = G in equation (2.5.17) and G = G in equation (2.5.20); w path m path — Δ is the attenuation due to the diffraction between S and the image receiver R′, calculated as in the dif(S,R′) previous section on pure diffraction; — Δ is the attenuation due to the diffraction between S and R, calculated as in the previous subsection on dif(S,R) pure diffraction. Vertical edge scenarios Equation (2.5.21) may be used to calculate the diffractions on vertical edges (lateral diffractions) in case of industrial noise. If this is the case, A = Δ is taken and the term A is kept. In addition, A and A dif dif(S,R) ground atm ground shall be calculated from the total length of the propagation path. A is still calculated from the direct div distance d. Equations (2.5.8) and (2.5.6) respectively become: A ¼A þApathþApath þΔ (2.5.33) H div atm ground,H dif,H ðS,RÞ A ¼A þApathþApath þΔ (2.5.34) F div atm ground,F dif,H ðS,RÞ Δ is indeed used in homogeneous conditions in equation (2.5.34). dif Reflections on vertical obstacles Attenuation through absorption The reflections on vertical obstacles are dealt with by means of image sources. Reflections on building façades and noise barriers are thus treated in this way. An obstacle is considered to be vertical if its slope in relation to the vertical is less than 15°. When dealing with reflections on objects which slope in relation to the vertical is more or equal to 15° the object is not considered. The obstacles where at least one dimension is less than 0,5 m shall be ignored in the reflection calculation, except for special configurations (1). Note that reflections on the ground are not dealt with here. They are taken into account in the calculations of attenuation due to the boundary (ground, diffraction). If L is the power level of the source S and α the absorption coefficient of the surface of the obstacle as WS r defined by the EN 1793-1:2013, then the power level of the image source S′ is equal to: L = L + 10 · lg(1 – α) = L + A (2.5.35) WS′ WS r WS refl where 0 ≤ α < 1 r (1) A network of small obstacles in a plane and at regular intervals constitutes one example of a special configuration.L 168/42 EN Official Journal of the European Union 1.7.2015 The propagation attenuations described above are then applied to this path (image source, receiver), as for a direct path. Figure 2.5.g Specular reflection on an obstacle dealt with by the image source method (S: source, S′: image source, R: receiver) Attenuation through retrodiffraction In the geometrical research of sound paths, during reflection on a vertical obstacle (barrier wall, building), the position of the impact of the ray in relation to the upper edge of this obstacle determines the more or less significant proportion of energy effectively reflected. This loss of acoustic energy when the ray undergoes a reflection is called attenuation through retrodiffraction. In the case of potential multiple reflections between two vertical walls, at least the first reflection shall be considered. In the case of a trench (see for example Figure 2.5.h), the attenuation through retrodiffraction shall be applied to each reflection on the retaining walls. Figure 2.5.h Sound ray reflected to the order of 4 in a track in a trench: actual cross-section (top), unfolded cross- section (bottom) In this representation, the sound ray reaches the receiver ‘by successively passing through’ the retaining walls of the trench, which can therefore be compared to openings.1.7.2015 EN Official Journal of the European Union L 168/43 When calculating propagation through an opening, the sound field at the receiver is the sum of the direct field and the field diffracted by the edges of the opening. This diffracted field ensures the continuity of the transition between the clear area and the shadow area. When the ray approaches the edge of the opening, the direct field is attenuated. The calculation is identical to that of the attenuation by a barrier in the clear area. The path difference δ′ associated with each retrodiffraction is the opposite of the path difference between S and R relatively at each upper edge O, and this in a view according to a deployed cross-section (see Figure 2.5.i). δ′ = – (SO + OR – SR) (2.5.36) Figure 2.5.i The path difference for the second reflection The ‘minus’ sign of equation (2.5.36) means that the receiver is considered here in the clear area. Attenuation through retrodiffraction Δ is obtained by equation (2.5.37), which is similar to equation retrodif (2.5.21) with reworked notations. 8 � � >><10C �lg 3þ40 δ′ if 40 δ′� − 2 h λ λ Δ = (2.5.37) retrodif >>: 0 otherwise This attenuation is applied to the direct ray each time it ‘passes through’ (reflects on) a wall or building. The power level of the image source S′ therefore becomes: L = L + 10 × lg(1 – α) – Δ (2.5.38) W′ W r retrodif In complex propagation configurations, diffractions may exist between reflections, or between the receiver and the reflections. In this case, the retrodiffraction by the walls is estimated by considering the path between source and first diffraction point R′ (therefore considered as the receiver in equation (2.5.36)). This principle is illustrated in Figure 2.5.j. Figure 2.5.j The path difference in the presence of a diffraction: actual cross-section (top), unfolded cross-section (bottom) In case of multiple reflections the reflections due to every single reflections are added.L 168/44 EN Official Journal of the European Union 1.7.2015 2.6. General provisions — Aircraft noise 2.6.1. Definitions and symbols Some important terms are described here by the general meanings attributed to them in this document. The list is not exhaustive; only expressions and acronyms used frequently are included. Others are described where they first occur. The mathematical symbols (listed after the terms) are the main ones used in equations in the main text. Other symbols used locally in both the text and the appendices are defined where they are used. The reader is reminded periodically of the interchangeability of the words sound and noise in this document. Although the word noise has subjective connotations — it is usually defined by acousticians as ‘unwanted sound’ — in the field of aircraft noise control it is commonly taken to mean just sound — airborne energy transmitted by acoustic wave motion. The symbol !denotes cross references to other terms included in the list. Terms AIP Aeronautical Information Publication Aircraft configuration The positions of slats, flaps and landing gear Aircraft movement An arrival, departure or other aircraft action that affects noise exposure around an aerodrome Aircraft noise and per­ Data describing the acoustic and performance characteristics of different aeroplanes formance data types that are required by the modelling process. They include ! NPD relationships and information that allows engine thrust/power to be calculated as a function of ! flight configuration. The data are usually supplied by the aircraft manufacturer although when that is not possible it is sometimes obtained from other sources. When no data are available, it is usual to represent the aircraft concerned by adapt­ ing data for a suitably similar aircraft — this is referred to as substitution Altitude Height above mean sea level ANP database The Aircraft Noise and Performance database included in Appendix I A-weighted sound level, Basic sound/noise level scale used for measuring environmental noise including that L from aircraft and on which most noise contour metrics are based A Backbone ground track A representative or nominal ground track which defines the centre of a swathe of tracks Baseline noise event level The noise event level read from an NPD database Brake release !Start of roll Corrected net thrust At a given power setting (e.g. EPR or N ) net thrust falls with air density and thus 1 with increasing aircraft altitude; corrected net thrust is the value at sea level Cumulative sound/noise A decibel measure of the noise received over a specified period of time, at a point level near an airport, from aeroplane traffic using normal operating conditions and flight paths. It is calculated by accumulating in some way the event sound/noise levels occurring at that point Decibel sum or average Sometimes referred to elsewhere as ‘energy’ or ‘logarithmic’ (as opposed to arith­ metic) values. Used when it is appropriaXte to sum or average the underlying energy- like quantities; e.g. decibel sum¼10�lg 10Li=101.7.2015 EN Official Journal of the European Union L 168/45 Energy fraction, F Ratio of sound energy received from segment to energy received from infinite flight path Engine power setting Value of the ! noise related power parameter used to determine noise emission from the NPD database Equivalent (continuous) A measure of long-term sound. The level of a hypothetical steady sound, which sound level, L over a specified period of time, contains the same total energy as the actual variable eq sound Event sound/noise level A decibel measure of the finite quantity of sound (or noise) received from a passing aeroplane !sound exposure level Flight configuration = !Aircraft configuration + !Flight parameters Flight parameters Aircraft power setting, speed, bank angle and weight Flight path The path of an aeroplane through the air, defined in three dimensions, usually with reference to an origin at the start of take-off roll or at the landing threshold Flight path segment Part of an aircraft flight path represented for noise modelling purposes by a straight line of finite length Flight procedure The sequence of operational steps followed by the aircraft crew or flight manage­ ment system: expressed as changes of flight configuration as a function of distance along the ground track Flight profile Variation of aeroplane height along the ground track (sometimes includes changes of !flight configuration too) — described by a set of !profile points Ground plane (Or Nominal Ground Plane) Horizontal ground surface through the aerodrome refer­ ence point on which the contours are normally calculated Ground speed Aircraft speed relative to a fixed point on the ground Ground track Vertical projection of the flight path onto the ground plane Height Vertical distance between aircraft and !ground plane Integrated sound level Otherwise termed !single event sound exposure level ISA International Standard Atmosphere — defined by ICAO. Defines variation of air temperature, pressure, and density with height above mean sea level. Used to nor­ malise the results of aircraft design calculations and analysis of test data Lateral attenuation Excess attenuation of sound with distance attributable, directly or indirectly, to the presence of the ground surface. Significant at low angles of elevation (of the aircraft above the ground plane) Maximum noise/sound The maximum sound level reached during an event level Mean Sea Level, MSL The standard earth surface elevation to which the !ISA is referred Net thrust The propulsive force exerted by an engine on the airframeL 168/46 EN Official Journal of the European Union 1.7.2015 Noise Noise is defined as unwanted sound. But metrics such as A-weighted sound level (L ) A and effective perceived noise level (EPNL) effectively convert sound levels into noise levels. Despite a consequent lack of rigour, the terms sound and noise are sometimes used interchangeably in this document, as elsewhere — especially in conjunction with the word level Noise contour A line of constant value of a cumulative aircraft noise level or index around an air­ port Noise impact The adverse effect(s) of noise on its recipients; importantly it is implied that noise metrics are indicators of noise impact Noise index A measure of long term, or cumulative sound which correlates with (i.e. is consid­ ered to be a predictor of) its effects on people. May take some account of factors in addition to the magnitude of sound (especially time of day). An example is day-eve­ ning-night level L DEN Noise level A decibel measure of sound on a scale which indicates its loudness or noisiness. For environmental noise from aircraft, two scales are generally used: A-weighted sound level and Perceived Noise Level. These scales apply different weights to sound of dif­ ferent frequencies — to mimic human perception Noise metric An expression used to describe any measure of quantity of noise at a receiver pos­ ition whether it be a single event or an accumulation of noise over extended time. There are two commonly used measures of single event noise: the maximum level reached during the event, or its sound exposure level, a measure of its total sound en­ ergy determined by time integration Noise-power-distance Noise event levels tabulated as a function of distance below an aeroplane in steady (NPD) relationships/data level flight at a reference speed in a reference atmosphere, for each of a number of ! engine power settings. The data account for the effects of sound attenuation due to spherical wave spreading (inverse-square law) and atmospheric absorption. The dis­ tance is defined perpendicular to the aeroplane flight path and the aircraft wing-axis (i.e. vertically below the aircraft in non-banked flight) Noise-related power para­ Parameter that describes or indicates the propulsive effort generated by an aircraft meter engine to which acoustic power emission can logically be related; usually taken to be ! corrected net thrust. Loosely termed ‘power’ or ‘power setting’ throughout the text Noise significance The contribution from a flight path segment is ‘noise significant’ if it affects the event noise level to an appreciable extent. Disregarding segments that are not noise- significant yields massive savings in computer processing Observer !Receiver Procedural steps Prescription for flying a profile — steps include changes of speed and/or altitude Profile point Height of flight path segment end point — in vertical plane above the ground track Receiver A recipient of noise that arrives from a source; principally at a point on or near the ground surface Reference atmosphere A tabulation of sound absorption rates used to standardise NPD data (see Appen­ dix D) Reference day A set of atmospheric conditions on which ANP data are standardised Reference duration A nominal time interval used to standardise single event sound exposure level mea­ surements; equal to 1 second in the case of !SEL1.7.2015 EN Official Journal of the European Union L 168/47 Reference speed Aeroplane groundspeed to which NPD !SEL data are normalised SEL !Sound Exposure Level Single event sound expo­ The sound level an event would have if all its sound energy were compressed uni­ sure level formly into a standard time interval known as the !reference duration Soft ground A ground surface that is acoustically ‘soft’, typically grassy, that surrounds most aerodromes. Acoustically hard, i.e. highly reflective, ground surfaces includes con­ crete and water. The noise contour methodology described herein applies to soft ground conditions Sound Energy transmitted through air by (longitudinal) wave motion which is sensed by the ear Sound attenuation The decrease in sound intensity with distance along a propagation path. For aircraft noise its causes include spherical wave spreading, atmospheric absorption and ! lateral attenuation Sound exposure A measure of total sound energy immission over a period of time Sound Exposure Level, (Acronym SEL) A metric standardised in ISO 1996-1 or ISO 3891 = A-weighted sin­ L gle event sound exposure level referenced to 1 second AE Sound intensity The strength of sound immission at a point — related to acoustical energy (and indi­ cated by measured sound levels) Sound level A measure of sound energy expressed in decibel units. Received sound is measured with or without ‘frequency weighting’; levels measured with a weighting are often termed !noise levels Stage/trip length Distance to first destination of departing aircraft; taken to be an indicator of aircraft weight Start of Roll, SOR The point on the runway from which a departing aircraft commences its take-off. Also termed ‘brake release’ True airspeed Actual speed of aircraft relative to air (= groundspeed in still air) Weighted equivalent An modified version of L in which different weights are assigned to noise occurring eq sound level, L during different period of the day (usually day, evening and night) eq,W Symbols d Shortest distance from an observation point to a flight path segment d Perpendicular distance from an observation point to the flight path (slant distance or slant p range) d Scaled distance λ F Actual net thrust per engine n F/δ Corrected net thrust per engine n h Aircraft altitude (above MSL) L Event noise level (scale undefined) L(t) Sound level at time t (scale undefined)L 168/48 EN Official Journal of the European Union 1.7.2015 L , L (t) A-weighted sound pressure level (at time t) — measured on the slow sound level meter scale A A L (SEL) Sound Exposure Level AE L Maximum value of L (t) during an event Amax A L Single event sound exposure level E L Single event sound exposure level determined from NPD database E∞ L Effective Perceived Noise Level EPN L Equivalent (continuous) sound level eq L Maximum value of L(t) during an event max L Maximum level generated by a segment max,seg ‘ Perpendicular distance from an observation point to the ground track lg Logarithm to base 10 N Number of segments or sub-segments NAT Number of events with L exceeding a specified threshold max P Power parameter in NPD variable L(P,d) P Power parameter relevant to a particular segment seg q Distance from start of segment to closest point of approach R Radius of turn S Standard deviation s Distance along ground track s Runway length RWY t Time t Effective duration of single sound event e t Reference time for integrated sound level 0 V Groundspeed V Equivalent segment groundspeed seg V Reference groundspeed for which NPD data are defined ref x,y,z Local coordinates x′,y′,z′ Aircraft coordinates X ,Y ,Z Position of aerodrome reference point in geographical coordinates ARP ARP ARP z Height of aircraft above ground plane/aerodrome reference point α Parameter used for calculation of the finite segment correction D F β Elevation angle of aircraft relative to ground plane ε Aircraft bank angle γ Climb/descent angle1.7.2015 EN Official Journal of the European Union L 168/49 φ Depression angle (lateral directivity parameter) λ Total segment length ψ Angle between direction of aircraft movement and direction to observer ξ Aircraft heading, measured clockwise from magnetic north Λ(β,‘) Air-to-ground lateral attenuation Λ(β) Long range air-to-ground lateral attenuation Γ(‘) Lateral attenuation distance factor Δ Change in value of a quantity, or a correction (as indicated in the text) Δ Finite segment correction F Δ Engine installation correction I Δ Weighting for ith time of day period, dB i Δ Reverse thrust rev Δ Start of roll correction SOR Δ Duration (speed) correction V Subscripts 1, 2 Subscripts denoting start and end values of an interval or segment E Exposure i Aircraft type/category summation index j Ground track/subtrack summation index k Segment summation index max Maximum ref Reference value seg Segment specific value SOR Related to start of roll TO Takeoff 2.6.2. Quality framework Accuracy of input values All input values affecting the emission level of a source, including the position of the source, shall be determined with at least the accuracy corresponding to an uncertainty of ± 2dB(A) in the emission level of the source (leaving all other parameters unchanged). Use of default values In the application of the method, the input data shall reflect the actual usage. In general there shall be no reliance on default input values or assumptions. Specifically, flight paths derived from radar data to derive the flight paths shall be used whenever they exist and is of sufficient quality. Default input values and assumptions are accepted, for example, to be used for modelled routes instead of radar derived flight paths, if the collection of real data is associated with disproportionately high costs.L 168/50 EN Official Journal of the European Union 1.7.2015 Quality of the software used for the calculations Software used to perform the calculations shall prove compliance with the methods herewith described by means of certification of results against test cases. 2.7. Aircraft noise 2.7.1. Aim and scope of document Contour maps are used to indicate the extent and magnitude of aircraft noise impact around airports, that impact being indicated by values of a specified noise metric or index. A contour is a line along which the index value is constant. The index value aggregates in some way all the individual aircraft noise events that occur during some specified period of time, normally measured in days or months. The noise at points on the ground from aircraft flying into and out of a nearby aerodrome depends on many factors. Principal among these are the types of aeroplane and their powerplant; the power, flap and airspeed management procedures used on the aeroplanes themselves; the distances from the points concerned to the various flight paths; and local topography and weather. Airport operations generally include different types of aeroplanes, various flight procedures and a range of operational weights. Contours are generated by calculating surfaces of local noise index values mathematically. This document explains in detail how to calculate, at one observer point, the individual aircraft noise event levels, each for a specific aircraft flight or type of flight, that are subsequently averaged in some way, or accumulated, to yield index values at that point. The required surface of index values is generated merely by repeating the calculations as necessary for different aircraft movements — taking care to maximise efficiency by excluding events that are not ‘noise-significant’ (i.e. which do not contribute significantly to the total). Where noise generating activities associated with airport operations do not contribute materially to the overall population exposure to aircraft noise and associated noise contours, they may be excluded. These activities include: helicopters, taxiing, engine testing and use of auxiliary power-units. This does not necessarily mean that their impact is insignificant and where these circumstances occur assessment of the sources can be undertaken as set out in paragraphs 2.7.21 and 2.7.22. 2.7.2. Outline of the document The noise contour generation process is illustrated in Figure 2.7.a. Contours are produced for various purposes and these tend to control the requirements for sources and pre-processing of input data. Contours that depict historical noise impact might be generated from actual records of aircraft operations — of movements, weights, radar-measured flight paths, etc. Contours used for future planning purposes of necessity rely more on forecasts — of traffic and flight tracks and the performance and noise characteristics of future aircraft. Figure 2.7.a The noise contour generation process1.7.2015 EN Official Journal of the European Union L 168/51 Whatever the source of flight data, each different aircraft movement, arrival or departure, is defined in terms of its flight path geometry and the noise emission from the aircraft as it follows that path (movements that are essentially the same in noise and flight path terms are included by simple multiplication). The noise emission depends on the characteristics of the aircraft — mainly on the power generated by its engines. The recommended methodology involves dividing the flight path into segments. Sections 2.7.3 to 2.7.6 outline the elements of the methodology and explain the principle of segmentation on which it is based; that the observed event noise level is an aggregation of contributions from all ‘noise-significant’ segments of the flight path, each of which can be calculated independently of the others. Sections 2.7.3 to 2.7.6 also outline the input data requirements for producing a set of noise contours. Detailed specifications for the operational data needed are set out in Appendix A. How the flight path segments are calculated from pre-processed input data is described in Sections 2.7.7 to 2.7.13. This involves applications of aircraft flight performance analysis, equations for which are detailed in Appendix B. Flight paths are subject to significant variability — aircraft following any route are dispersed across a swathe due to the effects of differences in atmospheric conditions, aircraft weights and operating procedures, air traffic control constraints, etc. This is taken into account by describing each flight path statis­ tically — as a central or ‘backbone’ path which is accompanied by a set of dispersed paths. This too is explained in Sections 2.7.7 to 2.7.13 with reference to additional information in Appendix C. Sections 2.7.14 to 2.7.19 set out the steps to be followed in calculating the noise level of one single event — the noise generated at a point on the ground by one aircraft movement. Appendix D deals with the re-calculation of NPD-data for non-reference conditions. Appendix E explains the acoustic dipole source used in the model to define sound radiation from flight path segments of finite length. Applications of the modelling relationships described in Chapters 3 and 4 require, apart from the relevant flight paths, appropriate noise and performance data for the aircraft in question. Determining the event level for a single aircraft movement at a single observer point is the core calculation. It has to be repeated for all aircraft movements at each of a prescribed array of points covering the expected extent of the required noise contours. At each point the event levels are aggregated or averaged in some way to arrive at a ‘cumulative level’ or noise index value. This part of the process is described in Sections 2.7.20 and 2.7.23 to 2.7.25. Sections 2.7.26 to 2.7.28 summarise the options and requirement for fitting noise contours to arrays of noise index values. They provide guidance on contour generation and post-processing. 2.7.3. The concept of segmentation For any specific aircraft, the database contains baseline Noise-Power-Distance (NPD) relationships. These define, for steady straight flight at a reference speed in specified reference atmospheric conditions and in a specified flight configuration, the received sound event levels, both maximum and time integrated, directly beneath the aircraft (1) as a function of distance. For noise modelling purposes, the all-important propulsive power is represented by a noise-related power parameter; the parameter generally used is corrected net thrust. Baseline event levels determined from the database are adjusted to account for, firstly, differences between actual (i.e. modelled) and reference atmospheric conditions and (in the case of sound exposure levels) aircraft speed and, secondly, for receiver points that are not directly beneath the aircraft, differences between downwards and laterally radiated noise. This latter difference is due to lateral directivity (engine installation effects) and lateral attenuation. But the event levels so adjusted still apply only to the total noise from the aircraft in steady level flight. (1) Actually beneath the aircraft perpendicular to the wing axis and direction of flight; taken to be vertically below the aircraft when in non- turning (i.e. non-banked) flight.L 168/52 EN Official Journal of the European Union 1.7.2015 Segmentation is the process by which the recommended noise contour model adapts the infinite path NPD and lateral data to calculate the noise reaching a receiver from a non-uniform flight path, i.e. one along which the aircraft flight configuration varies. For the purposes of calculating the event sound level of an aircraft movement, the flight path is represented by a set of contiguous straight-line segments, each of which can be regarded as a finite part of an infinite path for which an NPD and the lateral adjustments are known. The maximum level of the event is simply the greatest of the individual segment values. The time integrated level of the whole noise event is calculated by summing the noise received from a sufficient number of segments, i.e. those which make a significant contribution to the total event noise. The method for estimating how much noise one finite segment contributes to the integrated event level is a purely empirical one. The energy fraction F — the segment noise expressed as a proportion of the total infinite path noise — is described by a relatively simple expression which allows for the longitudinal directivity of aircraft noise and the receiver's ‘view’ of the segment. One reason why a simple empirical method is generally adequate is that, as a rule, most of the noise comes from the nearest, usually, adjacent segment — for which the closest point of approach (CPA) to the receiver lies within the segment (not at one of its ends). This means that estimates of the noise from non-adjacent segments can be increasingly approximate as they get further away from the receiver without compromising the accuracy significantly. 2.7.4. Flight paths: Tracks and profiles In the modelling context, a flight path (or trajectory) is a full description of the motion of the aircraft in space and time (1). Together with the propulsive thrust (or other noise related power parameter) this is the information required to calculate the noise generated. The ground track is the vertical projection of the flight path on level ground. This is combined with the vertical flight profile to construct the 3-D flight path. Segmentation modelling requires that the flight path of every different aircraft movement is described by a series of contiguous straight segments. The manner in which the segmentation is performed is dictated by a need to balance accuracy and efficiency — it is necessary to approximate the real curved flight path sufficiently closely while minimising the computational burden and data requirements. Each segment has to be defined by the geometrical coordinates of its end points and the associated speed and engine power parameters of the aircraft (on which sound emission depends). Flight paths and engine power may be determined in various ways, the main ones involving (a) synthesis from a series of procedural steps and (b) analysis of measured flight profile data. Synthesis of the flight path (a) requires knowledge of (or assumptions for) ground tracks and their lateral dispersions, aircraft weight, speed, flap and thrust-management procedures, airport elevation, and wind and air temperature. Equations for calculating the flight profile from the required propulsion and aerodynamic parameters are given in Appendix B. Each equation contains coefficients (and/or constants) which are based on empirical data for each specific aircraft type. The aerodynamic-performance equations in Appendix B permit the consideration of any reasonable combination of aircraft operational weight and flight procedure, including operations at different takeoff gross weights. Analysis of measured data (b), e.g. from flight data recorders, radar or other aircraft tracking equipment, involves ‘reverse engineering’, effectively a reversal of the synthesis process (a). Instead of estimating the aircraft and powerplant states at the ends of the flight segments by integrating the effects of the thrust and aerodynamic forces acting on the airframe, the forces are estimated by differentiating the changes of height and speed of the airframe. Procedures for processing the flight path information are described in Section 2.7.12. In an ultimate noise modelling application, each individual flight could, theoretically, be represented independ­ ently; this would guarantee accurate accounting for the spatial dispersion of flight paths — which can be very significant. But to keep data preparation and computer time within reasonable bounds it is normal practice to represent flight path swathes by a small number of laterally displaced ‘subtracks’. (Vertical dispersion is usually represented satisfactorily by accounting for the effects of varying aircraft weights on the vertical profiles.) (1) Time is accounted for via the aircraft speed.1.7.2015 EN Official Journal of the European Union L 168/53 2.7.5. Aircraft noise and performance The ANP database provided in Appendix I covers most existing aircraft types. For aircraft types or variants for which data are not currently listed, they can best be represented by data for other, normally similar, aircraft that are listed. The ANP database includes default ‘procedural steps’ to enable the construction of flight profiles for at least one common noise abatement departure procedure. More recent database entries cover two different noise abatement departure procedures. 2.7.6. Airport and aircraft operations Case-specific data from which to calculate the noise contours for a particular airport scenario includes the following. General airport data — The aerodrome reference point (simply to locate the aerodrome in appropriate geographic coordinates). The reference point is set as the origin of the local Cartesian coordinate system used by the calculation procedure. — The aerodrome reference altitude (= altitude of aerodrome reference point). This is the altitude of the nominal ground plane on which, in the absence of topography corrections, the noise contours are defined. — Average meteorological parameters at or close to the aerodrome reference point (temperature, relative humidity, average windspeed and wind direction). Runway data For each runway: — Runway designation — Runway reference point (centre of runway expressed in local coordinates) — Runway length, direction and mean gradient — Location of start-of-roll and landing threshold (1). Ground track data Aircraft ground tracks shall be described by a series of coordinates in the (horizontal) ground-plane. The source of ground track data depends on whether relevant radar data are available or not. If they are, a reliable backbone track and suitable associated (dispersed) sub-tracks shall be established by statistical analysis of the data. If not, backbone tracks are usually constructed from appropriate procedural information, e.g. using standard instrument departure procedures from Aeronautical Information Publications. This conventional description includes the following information: — Designation of the runway the track originates from — Description of the track origin (start of roll, landing threshold) — Length of segments (for turns, radius and change of direction). (1) Displaced thresholds can be taken into account by defining additional runways.L 168/54 EN Official Journal of the European Union 1.7.2015 This information is the minimum necessary to define the core (backbone) track. But average noise levels calculated on the assumption that aircraft follow the nominal routes exactly can be liable to localised errors of several decibels. Thus lateral dispersion shall be represented, and the following additional information is necessary: — Width of the swathe (or other dispersion statistic) at each segment end — Number of subtracks — Distribution of movements perpendicular to the backbone track. Air traffic data Air traffic data are — the time period covered by the data and — the number of movements (arrivals or departures) of each aircraft type on each flight track, subdivided by (1) time of day as appropriate for specified noise descriptors, (2) for departures, operating weights or stage lengths, and (3), if necessary, operating procedures. Most noise descriptors require that events (i.e. aircraft movements) are defined as average daily values during specified periods of the day (e.g. day, evening and night) — see Sections 2.7.23 to 2.7.25. Topographical data The terrain around most airports is relatively flat. However this is not always the case and there may sometimes be a need to account for variations in terrain elevation relative to the airport reference elevation. The effect of terrain elevation can be especially important in the vicinity of approach tracks, where the aircraft is operating at relatively low altitudes. Terrain elevation data are usually provided as a set of (x,y,z) coordinates for a rectangular grid of certain mesh- size. But the parameters of the elevation grid are likely to be different from those of the grid used for the noise computation. If so linear interpolation may be used to estimate the appropriate z-coordinates in the latter. Comprehensive analysis of the effects of markedly non-level ground on sound propagation is complex and beyond the scope of this method. Moderate unevenness can be accounted for by assuming ‘pseudo-level’ ground; i.e. simply raising or lowering the level ground plane to the local ground elevation (relative to the reference ground plane) at each receiver point (see Section 2.7.4). Reference conditions The international aircraft noise and performance (ANP) data are normalised to standard reference conditions that are widely used for airport noise studies (see Appendix D). Reference conditions for NPD data (1) Atmospheric pressure: 101,325 kPa (1 013,25 mb) (2) Atmospheric absorption: Attenuation rates listed in Table D-1 of Appendix D1.7.2015 EN Official Journal of the European Union L 168/55 (3) Precipitation: None (4) Wind Speed: Less than 8 m/s (15 knots) (5) Groundspeed: 160 knots (6) Local terrain: Flat, soft ground free of large structures or other reflecting objects within several kilometres of aircraft ground tracks. Standardised aircraft sound measurements are made 1,2 m above the ground surface. However no special account of this is necessary as, for modelling purposes, it may be assumed that event levels are relatively insensitive to receiver height (1). Comparisons of estimated and measured airport noise levels indicate that the NPD data can be assumed applicable when the near surface average conditions lie within the following envelope: — Air temperature less than 30 °C — Product of air temperature (°C), and relative humidity, (percent) greater than 500 — Wind speed less than 8 metres per second (15 knots). This envelope is believed to encompass conditions encountered at most of the world's major airports. Appendix D provides a method for converting NPD data to average local conditions which fall outside it, but, in extreme cases, it is suggested that the relevant aeroplane manufacturers be consulted. Reference conditions for aeroplane aerodynamic and engine data (1) Runway Elevation: Mean sea level (2) Air temperature: 15 °C (3) Takeoff gross weight: As defined as a function of stage length in the ANP database (4) Landing gross weight: 90 percent of maximum landing gross weight (5) Engines supplying thrust: All Although ANP aerodynamic and engine data are based on these conditions, they can be used as tabulated for non-reference runway elevations and average air temperatures in ECAC states without significantly affecting the accuracy of the calculated contours of cumulative average sound level. (see Appendix B.) The ANP database tabulates aerodynamic data for the takeoff and landing gross weights noted in items 3 and 4 above. Although, for cumulative noise calculations, the aerodynamic data themselves need not be adjusted for other gross weights, calculation of the takeoff and climbout flight profiles, using the procedures described in Appendix B, shall be based on the appropriate operational takeoff gross weights. (1) Calculated levels at 4 m or higher are sometimes requested. Comparison of measurements at 1,2 m and 10 m and theoretical calculation of ground effects show that variations of the A-weighted sound exposure level are relatively insensitive to receiver height. The variations are in general smaller than one decibel, except if the maximum angle of sound incidence is below 10° and if the A-weighted spectrum at the receiver has its maximum in the range of 200 to 500 Hz. Such low frequency dominated spectra may occur e.g. at long distances for low-bypass ratio engines and for propeller engines with discrete low frequency tones.L 168/56 EN Official Journal of the European Union 1.7.2015 2.7.7. Description of the flight path The noise model requires that each different aircraft movement is described by its three-dimensional flight path and the varying engine power and speed along it. As a rule, one modelled movement represents a subset of the total airport traffic, e.g. a number of (assumed) identical movements, with the same aircraft type, weight and operating procedure, on a single ground track. That track may itself be one of several dispersed ‘sub-tracks’ used to model what is really a swathe of tracks following one designated route. The ground track swathes, the vertical profiles and the aircraft operational parameters are all determined from the input scenario data — in conjunction with aircraft data from the ANP database. The noise-power-distance data (in the ANP database) define noise from aircraft traversing idealised horizontal flight paths of infinite length at constant speed and power. To adapt this data to terminal area flight paths that are characterised by frequent changes of power and velocity, every path is broken into finite straight-line segments; the noise contributions from each of these are subsequently summed at the observer position. 2.7.8. Relationships between flight path and flight configuration The three-dimensional flight path of an aircraft movement determines the geometrical aspects of sound radiation and propagation between aircraft and observer. At a particular aircraft weight and in particular atmospheric conditions, the flight path is governed entirely by the sequence of power, flap and altitude changes that are applied by the pilot (or automatic flight management system) in order to follow routes and maintain heights and speeds specified by ATC — in accordance with the aircraft operator's standard operating procedures. These instructions and actions divide the flight path into distinct phases which form natural segments. In the horizontal plane they involve straight legs, specified as a distance to the next turn, and turns, defined by radius and change of heading. In the vertical plane, segments are defined by the time and/or distance taken to achieve required changes of forward speed and/or height at specified power and flap settings. The corresponding vertical coordinates are often referred to as profile points. For noise modelling, flight path information is generated either by synthesis from a set of procedural steps (i.e. those followed by the pilot) or by analysis of radar data — physical measurements of actual flight paths flown. Whatever method is used, both horizontal and vertical shapes of the flight path, are reduced to segmented forms. Its horizontal shape (i.e. its 2-dimensional projection on the ground) is the ground track defined by the inbound or outbound routeing. Its vertical shape, given by the profile points, and the associated flight parameters speed, bank angle and power setting, together define the flight profile which depends on the flight procedure that is normally prescribed by the aircraft manufacturer and/or the operator. The flight path is constructed by merging the 2-D flight profile with the 2-D ground track to form a sequence of 3-D flight path segments. It should be remembered that, for a given set of procedural steps, the profile depends on the ground track; e.g. at the same thrust and speed the aircraft climb rate is less in turns than in straight flight. Although this guidance explains how to take this dependency into account, it has to be acknowledged that doing so would normally involve a very large computing overhead and users may prefer to assume that, for noise modelling purposes, the flight profile and ground track can be treated as independent entities; i.e. that the climb profile is unaffected by any turns. However, it is important to determine changes of bank angle that turns require as this has an important bearing on the directionality of sound emission. The noise received from a flight path segment depends on the geometry of the segment in relation to the observer and the aircraft flight configuration. But these are interrelated — a change in one causes a change in the other and it is necessary to ensure that, at all points on the path, the configuration of the aircraft is consistent with its motion along the path.1.7.2015 EN Official Journal of the European Union L 168/57 In a flight path synthesis, i.e. when constructing a flight path from a set of ‘procedural steps’ that describe the pilot's selections of engine power, flap angle, and acceleration/vertical speed, it is the motion that has to be calculated. In a flight path analysis, the reverse is the case: the engine power settings have to be estimated from the observed motion of the aeroplane — as determined from radar data, or sometimes, in special studies, from aircraft flight recorder data (although in the latter case engine power is usually part of the data). In either case, the coordinates and flight parameters at all segment end points have to be fed into the noise calculation. Appendix B presents the equations that relate the forces acting on an aircraft and its motion and explains how they are solved to define the properties of the segments that make up the flight paths. The different kinds of segments (and the sections of Appendix B that cover them) are take-off ground roll (B5), climb at constant speed (B6), power cutback (B7), accelerating climb and flap retraction (B8), accelerating climb after flap retraction (B9), descent and deceleration (B10) and final landing approach (B11). Inevitably, practical modelling involves varying degrees of simplification — the requirement for this depends on the nature of the application, the significance of the results and the resources available. A general simplifying assumption, even in the most elaborate applications, is that when accounting for flight track dispersion, the flight profiles and configurations on all the sub-tracks are the same as those on the backbone track. As at least 6 subtracks are to be used (see Section 2.7.11) this reduces computations massively for an extremely small penalty in fidelity. 2.7.9. Sources of flight path data Radar data Although aircraft flight data recorders can yield very high quality data, this is difficult to obtain for noise modelling purposes and radar data shall be regarded as the most readily accessible source of information on actual flight paths flown at airports (1). As it is usually available from airport noise and flight path monitoring systems, it is now used increasingly for noise modelling purposes. Secondary surveillance radar presents the flight path of an aircraft as a sequence of positional coordinates at intervals equal to the period of rotation of the radar scanner, typically about 4 seconds. The position of the aircraft over the ground is determined in polar coordinates — range and azimuth — from the reflected radar return (although the monitoring system normally transforms these to Cartesian coordinates); its height (2) is measured by the aeroplane's own altimeter and transmitted to the ATC computer by a radar-triggered transponder. But inherent positional errors due to radio interference and limited data resolution are significant (although of no consequence for the intended air traffic control purposes). Thus, if the flight path of a specific aircraft movement is required, it is necessary to smooth the data using an appropriate curve-fitting technique. However, for noise modelling purposes the usual requirement is for a statistical description of a swathe of flight paths; e.g. for all movements on a route or for just those of a specific aircraft type. Here the measurement errors associated with the relevant statistics can be reduced to insignificance by the averaging processes. Procedural steps In many cases is not possible to model flight paths on the basis of radar data — because the necessary resources are not available or because the scenario is a future one for which there are no relevant radar data. In the absence of radar data, or when its use is inappropriate, it is necessary to estimate the flight paths on the basis of operational guidance material, for example instructions given to flight crews via AIPs and aircraft operating manuals — referred to here as procedural steps. Advice on interpreting this material shall be sought from air traffic control authorities and the aircraft operators where necessary. (1) Aircraft flight data recorders provide comprehensive operational data. However this is not readily accessible and is costly to provide; thus its use for noise modelling purposes is normally restricted to special projects and model development studies. (2) Usually measured as altitude above MSL (i.e. relative to 1 013 mb) and corrected to airport elevation by the airport monitoring system.L 168/58 EN Official Journal of the European Union 1.7.2015 2.7.10. Coordinate systems The local coordinate system The local coordinate system (x,y,z) is a Cartesian one and has its origin (0,0,0) at the aerodrome reference point (X ,Y ,Z ), where Z is the airport reference altitude and z = 0 defines the nominal ground plane on ARP ARP ARP ARP which contours are usually calculated. The aircraft heading ξ in the xy-plane is measured clockwise from magnetic north (see Figure 2.7.b). All observer locations, the basic calculation grid and the noise contour points are expressed in local coordinates (1). Figure 2.7.b Local coordinate system (x,y,z) and ground-track fixed coordinate s The ground-track fixed coordinate system This coordinate is specific for each ground track and represents distance s measured along the track in the flight direction. For departure tracks s is measured from the start of roll, for approach tracks from the landing threshold. Thus s becomes negative in areas — behind the start of roll for departures and — before crossing the runway landing threshold for approaches. (1) Usually the axes of the local coordinate are parallel to the axis of the map that contours are drawn on. However it is sometimes useful to choose the x-axis parallel to a runway in order to get symmetrical contours without using a fine computational grid (see Sections 2.7.26 to 2.7.28).1.7.2015 EN Official Journal of the European Union L 168/59 Flight operational parameters such as height, speed and power setting are expressed as functions of s. The aircraft coordinate system The aircraft-fixed Cartesian coordinate system (x′,y′,z′) has its origin at the actual aircraft location. The axis- system is defined by the climb-angle γ, the flight direction ξ and the bank-angle ε (see Figure 2.7.c). Figure 2.7.c Aircraft fixed coordinate system (x′,y′,z′) Accounting for topography In cases where topography has to be taken into account (see Section 2.7.6), the aircraft height coordinate z has to be replaced by z′= z – z (where z is the z-coordinate of the observer location O) when estimating the o o propagation distance d. The geometry between aircraft and observer is shown in Figure 2.7.d. For the definitions of d and ‘see Sections 2.7.14 to 2.7.19 (1). Figure 2.7.d Ground elevation along (left) and lateral (right) to ground track (The nominal ground plane z = 0 passes through the aerodrome reference point. O is the observer location.) (1) For non-level ground it is possible for the observer to be above the aircraft in which case, for calculating sound propagation z′ (and the corresponding elevation angle β — see Chapter 4) is put equal to zero.L 168/60 EN Official Journal of the European Union 1.7.2015 2.7.11. Ground Tracks Backbone tracks The backbone track defines the centre of the swathe of tracks followed by aircraft using a particular routeing. For the purposes of aircraft noise modelling it is defined either (i) by prescriptive operational data such as the instructions given to pilots in AIPs, or (ii) by statistical analysis of radar data as explained in Section 2.7.9 — when this is available and appropriate to the needs of the modelling study. Constructing the track from operational instructions is normally quite straightforward as these prescribe a sequence of legs which are either straight — defined by length and heading, or circular arcs defined by turn rate and change of heading; see Figure 2.7.e for an illustration. Figure 2.7.e Ground track geometry in terms of turns and straight segments Fitting a backbone track to radar data is more complex, firstly because actual turns are made at a varying rate and secondly because its line is obscured by the scatter of the data. As explained, formalised procedures have not yet been developed and it is common practice to match segments, straight and curved, to the average positions calculated from cross-sections of radar tracks at intervals along the route. Computer algorithms to perform this task are likely to be developed in future but, for the present, it is for the modeller to decide how to use available data to best advantage. A major factor is that the aircraft speed and turn radius dictate the angle of bank and, as will be seen in Section 2.7.19, non-symmetries of sound radiation around the flight path govern noise on the ground, as well as the position of the flight path itself. Theoretically, seamless transition from straight flight to fixed radius turn would require an instantaneous application of bank angle ε, which is physically impossible. In reality it takes a finite time for the bank angle to reach the value required to maintain a specified speed and turn radius r, during which the turn radius tightens from infinity to r. For modelling purposes the radius transition can be disregarded and the bank angle assumed to increase steadily from zero (or other initial value) to ε at the start of the turn and to be the next value of ε at the end of the turn (1). Track dispersion Where possible, definitions of lateral dispersion and representative sub-tracks shall be based on relevant past experience from the study airport; normally via an analysis of radar data samples. The first step is to group the data by route. Departure tracks are characterised by substantial lateral dispersion which, for accurate modelling, has to be taken into account. Arrival routes normally coalesce into a very narrow swathe about the final approach path and it is usually sufficient to represent all arrivals by a single track. But if the approach swathes are wide within the region of the noise contours they might need to be represented by sub-tracks in the same way as departure routes. (1) How best to implement this is left to the user as this will depend on the way in which turn radii are defined. When the starting point is a sequence of straight or circular legs, a relatively simple option is to insert bank angle transition segments at the start of the turn and at its end in which the aircraft rolls at a constant rate (e.g. expressed in °/m or °/s).1.7.2015 EN Official Journal of the European Union L 168/61 It is common practice to treat the data for a single route as a sample from a single population; i.e. to be represented by one backbone track and one set of dispersed subtracks. However, if inspection indicates that the data for different categories of aircraft or operations differ significantly (e.g. should large and small aircraft have substantially different turn radii), further subdivision of the data into different swathes may be desirable. For each swathe, the lateral track dispersions are determined as a function of distance from the origin; movements then being apportioned between a backbone track and a suitable number of dispersed sub-tracks on the basis of the distribution statistics. As it is normally unwise to disregard the effects of track dispersion, in the absence of measured swathe data a nominal lateral spread across and perpendicular to the backbone track shall be defined by a conventional distribution function. Calculated values of noise indices are not particularly sensitive to the precise shape of the lateral distribution: the Normal (Gaussian) Distribution provides an adequate description of many radar- measured swathes. Typically a 7-point discrete approximation is used (i.e. representing the lateral dispersion by 6 subtracks equally spaced around the backbone track). The spacing of the subtracks depends on the standard deviation of the lateral dispersion function. For normally distributed tracks with a standard deviation S, 98,8 % of the tracks are located within a corridor with boundaries located at ± 2,5 · S. Table 2.7.a gives the spacing of the six subtracks and the percentage of the total movements assigned to each. Appendix C gives values for other numbers of subtracks. Table 2.7.a Percentages of movements for a normal distribution function with standard deviation S for 7 subtracks (backbone track is subtrack 1) Subtrack number Location of subtrack Percentage of movements on subtrack 7 – 2,14 · S 3 % 5 – 1,43 · S 11 % 3 – 0,71 · S 22 % 1 0 28 % 2 0,71 · S 22 % 4 1,43 · S 11 % 6 2,14 · S 3 % The standard deviation S is a function of the coordinate s along the backbone-track. It can be specified — together with the description of the backbone-track — in the flight track data sheet shown in Appendix A3. In the absence of any indicators of the standard deviation — e.g. from radar data describing comparable flight tracks — the following values are recommended: For tracks involving turns of less than 45 degrees: S(s) = 0,055 · s – 150 for 2 700 m ≤ s ≤30 000 m (2.7.1) S(s) = 1 500 for s > 30 000 mL 168/62 EN Official Journal of the European Union 1.7.2015 For tracks involving turns of more than 45 degrees: S(s) = 0,128 · s – 420 for 3 300 m ≤ s ≤ 15 000 m (2.7.2) S(s) = 1 500 m for s > 15 000 m For practical reasons, S(s) is assumed to be zero between the start of roll and s = 2 700 m or s = 3 300 m depending on the amount of turn. Routes involving more than one turn shall be treated as per equation (2.7.2). For arrivals, lateral dispersion can be neglected within 6 000 m of touchdown. 2.7.12. Flight profiles The flight profile is a description of the aircraft motion in the vertical plane above the ground track, in terms of its position, speed, bank angle and engine power setting. One of the most important tasks facing the model user is that of defining aircraft flight profiles that adequately meet the requirements of the modelling application — efficiently, without consuming excessive time and resources. Naturally, to achieve high accuracy, the profiles have to reflect closely the aircraft operations they are intended to represent. This requires reliable information on the atmospheric conditions, aircraft types and variants, operating weights and the operating procedures — the variations of thrust and flap settings and the trade-offs between changes of height and speed — all appropriately averaged over the time period(s) of interest. Often such detailed information are not available but this is not necessarily an obstacle; even if they are, the modeller has to exercise judgement to balance the accuracy and detail of the input information with the needs for, and uses of, the contour outputs. The synthesis of flight profiles from ‘procedural steps’ obtained from the ANP database or from aircraft operators is described in Section 2.7.13 and Appendix B. That process, usually the only recourse open to the modeller when no radar data are available, yields both the flight path geometry and the associated speed and thrust variations. It would normally be assumed that all (alike) aircraft in a swathe, whether assigned to the backbone or the dispersed subtracks, follow the backbone track profile. Beyond the ANP database, which provides default information on procedural steps, the aircraft operators are the best source of reliable information, i.e. the procedures they use and the typical weights flown. For individual flights, the ‘gold standard’ source is the aircraft flight data recorder (FDR) from which all relevant information can be obtained. But even if such data are available, the pre-processing task is formidable. Thus, and in keeping with the necessary modelling economies, the normal practical solution is to make educated assumptions about mean weights and operating procedures. Caution must be exercised before adopting default procedural steps provided in the ANP database (customarily assumed when actual procedures are not known). These are standardised procedures that are widely followed but which may or may not be used by operators in particular cases. A major factor is the definition of take-off (and sometimes climb) engine thrust that can depend to an extent on prevailing circumstances. In particular, it is common practice to reduce thrust levels during departure (from maximum available) in order to extend engine life. Appendix B gives guidance on representing typical practice; this will generally produce more realistic contours than a full thrust assumption. However, if, for example, runways are short and/or average air temperatures are high, full thrust is likely to be a more realistic assumption. When modelling actual scenarios, improved accuracy can be achieved by using radar data to supplement or replace this nominal information. Flight profiles can be determined from radar data in a similar way to the lateral backbone tracks — but only after segregating the traffic by aircraft type and variant and sometimes by weight or stage length (but not by dispersion) — to yield for each sub-group a mean profile of height and speed against ground distance travelled. Again, when merging with the ground tracks subsequently, this single profile is normally assigned to the backbone and subtracks alike. Knowing the aircraft weight, the variation of speed and propulsive thrust can be calculated via step-by-step solution of the equations of motion. Before doing so it is helpful to pre-process the data to minimise the effects1.7.2015 EN Official Journal of the European Union L 168/63 of radar errors which can make acceleration estimates unreliable. The first step in each case is to redefine the profile by fitting straight line segments to represent the relevant stages of flight; with each segment being appropriately classified; i.e. as a ground roll, constant speed climb or descent, thrust cutback, or acceleration/ deceleration with or without flap change. The aircraft weight and atmospheric state are also required inputs. Section 2.7.11 makes it clear that special provision has to be made to account for the lateral dispersion of flight tracks about the nominal or backbone routeings. Radar data samples are characterised by similar dispersions of flight paths in the vertical plane. However it is not usual practice to model vertical dispersion as an independent variable; it arises mainly due to differences in aircraft weights and operating procedures that are taken into account when pre-processing traffic input data. 2.7.13. Construction of flight path segments Each flight path has to be defined by a set of segment coordinates (nodes) and flight parameters. The starting point is to determine the coordinates of the ground track segments. The flight profile is then calculated, remembering that for a given set of procedural steps, the profile depends on the ground track; e.g. at the same thrust and speed the aircraft climb rate is less in turns than in straight flight. Finally the 3-D flight path segments are constructed by merging the 2-D flight profile with the 2-D ground track (1). Ground track A ground track, whether a backbone track or a dispersed sub-track, is defined by a series of (x,y) coordinates in the ground plane (e.g. from radar information) or by a sequence of vectoring commands describing straight segments and circular arcs (turns of defined radius r and change of heading Δξ). For segmentation modelling, an arc is represented by a sequence of straight segments fitted to sub-arcs. Although they do not appear explicitly in the ground-track segments, the banking of aircraft during turns influences their definition. Appendix B4 explains how to calculate bank angles during a steady turn but of course these are not actually applied or removed instantaneously. How to handle the transitions between straight and turning flight, or between one turn and an immediately sequential one, is not prescribed. As a rule, the details, which are left to the user (see Section 2.7.11), are likely to have a negligible effect on the final contours; the requirement is mainly to avoid sharp discontinuities at the ends of the turn and this can be achieved simply, for example, by inserting short transition segments over which the bank angle changes linearly with distance. Only in the special case that a particular turn is likely to have a dominating effect on the final contours would it be necessary to model the dynamics of the transition more realistically, to relate bank angle to particular aircraft types and to adopt appropriate roll rates. Here it is sufficient to state that the end sub-arcs Δξ in any turn are dictated by bank angle change requirements. The remainder of the arc with change of trans heading Δξ – 2 · Δξ degrees is divided into n sub-arcs according to the equation: trans sub n = int(1 + (Δξ – 2 · Δξ )/30) (2.7.3) sub trans where int(x) is a function that returns the integer part of x. Then the change of heading Δξ of each sub-arc is sub computed as Δξ = (Δξ – 2 · Δξ )/n (2.7.4) sub trans sub where n needs to be large enough to ensure that Δξ ≤ 30 degrees. The segmentation of an arc (excluding the sub sub terminating transition sub-segments) is illustrated in Figure 2.7.f (2). (1) For this purpose the total length of the ground track should always exceed that of the flight profile. This can be achieved, if necessary, by adding straight segments of suitable length to the last segment of the ground track. (2) Defined in this simple way, the total length of the segmented path is slightly less than that of the circular path. However the consequent contour error is negligible if the angular increments are below 30°.L 168/64 EN Official Journal of the European Union 1.7.2015 Figure 2.7.f Construction of flight path segments dividing turn into segments of length Ds (upper view in horizontal plane, lower view in vertical plane) Flight profile The parameters describing each flight profile segment at the start (suffix 1) and end (suffix 2) of the segment are: s , s distance along the ground track, 1 2 z , z aeroplane height, 1 2 V , V groundspeed, 1 2 P , P noise-related power parameter (matching that for which the NPD-curves are defined), and 1 2 ε , ε bank angle. 1 2 To build a flight profile from a set of procedural steps (flight path synthesis), segments are constructed in sequence to achieve required conditions at the end points. The end-point parameters for each segment become the start-point parameters for the next segment. In any segment calculation the parameters are known at the start; required conditions at the end are specified by the procedural step. The steps themselves are defined either by the ANP defaults or by the user (e.g. from aircraft flight manuals). The end conditions are usually height and speed; the profile building task is to determine the track distance covered in reaching those conditions. The undefined parameters are determined via flight performance calculations described in Appendix B.1.7.2015 EN Official Journal of the European Union L 168/65 If the ground track is straight, the profile points and associated flight parameters can be determined independ­ ently of the ground track (bank angle is always zero). However ground tracks are rarely straight; they usually incorporate turns and, to achieve best results, these have to be accounted for when determining the 2-dimensional flight profile, where necessary splitting profile segments at ground track nodes to inject changes of bank angle. As a rule the length of the next segment is unknown at the outset and it is calculated provisionally assuming no change of bank angle. If the provisional segment is then found to span one or more ground track nodes, the first being at s, i.e. s < s < s , the segment is truncated at s, calculating the parameters 1 2 there by interpolation (see below). These become the end-point parameters of the current segment and the start- point parameters of a new segment — which still has the same target end conditions. If there is no intervening ground track node the provisional segment is confirmed. If the effects of turns on the flight profile are to be disregarded, the straight flight, single segment solution is adopted although the bank angle information is retained for subsequent use. Whether or not turn effects are fully modelled, each 3-dimensional flight path is generated by merging its ­ 2-dimensional flight profile with its 2-dimensional ground track. The result is a sequence of coordinate sets (x,y, z), each being either a node of the segmented ground track, a node of the flight profile or both, the profile points being accompanied by the corresponding values of height z, ground speed V, bank angle ε and engine power P. For a track point (x,y) which lies between the end points of a flight profile segment, the flight parameters are interpolated as follows: z = z + f · (z – z ) (2.7.5) 1 2 1 qffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi V¼ V2þf �ðV2 − V2Þ (2.7.6) 1 2 1 ε = ε + f · (ε – ε ) (2.7.7) 1 2 1 qffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi P¼ P2þf �ðP2 − P2Þ (2.7.8) 1 2 1 Where f = (s – s )/(s – s ) (2.7.9) 1 2 1 Note that whilst z and ε are assumed to vary linearly with distance, V and P are assumed to vary linearly with time (i.e. constant acceleration (1)). When matching flight profile segments to radar data (flight path analysis) all end-point distances, heights, speeds and bank angles are determined directly from the data; only the power settings have to be calculated using the performance equations. As the ground track and flight profile coordinates can also be matched appropriately, this is usually quite straightforward. Segmentation of the takeoff ground roll When taking off, as an aircraft accelerates between the point of brake release (alternatively termed Start-of-Roll SOR) and the point of lift-off, speed changes dramatically over a distance of 1 500 to 2 500 m, from zero to between around 80 and 100 m/s. (1) Even if engine power settings remain constant along a segment, propulsive force and acceleration can change due to variation of air density with height. However, for the purposes of noise modelling these changes are normally negligible.L 168/66 EN Official Journal of the European Union 1.7.2015 The takeoff roll is thus divided into segments with variable lengths over each of which the aircraft speed changes by specific increment ΔV of no more than 10 m/s (about 20 kt). Although it actually varies during the takeoff roll, an assumption of constant acceleration is adequate for this purpose. In this case, for the takeoff phase, V is initial speed, V is the takeoff speed, n is the number of takeoff segment and s is the equivalent 1 2 TO TO takeoff distance. For equivalent takeoff distance s (see Appendix B), start speed V and takeoff speed V the TO 1 2 number n of segments for the ground roll is TO n = int(1 + (V – V )/10) (2.7.10) TO 2 1 and hence the change of velocity along a segment is ΔV = (V – V )/n (2.7.11) 2 1 TO and the time Δt on each segment is (constant acceleration assumed) 2�s Δt¼ TO (2.7.12) ðV þV Þ�n 2 1 TO The length s of segment k (1 ≤ k ≤ n ) of the takeoff roll is then: TO,k TO ð2k − 1Þ�s s ¼ðk − 0,5Þ�ΔV �Δt¼ TO (2.7.13) TO,k n2 TO Example: For a takeoff distance s = 1 600 m, V = 0 m/s and V = 75 m/s, this yields n = 8 segments with lengths TO 1 2 TO ranging from 25 to 375 meters (see Figure 2.7.g): Figure 2.7.g Segmentation of a takeoff roll (example for 8 segments) Similarly to the speed changes, the aircraft thrust changes over each segment by a constant increment ΔP, calculated as ΔP = (P – P )/n (2.7.14) TO init TO where P and P respectively designate the aircraft thrust at the point of lift-off and the aircraft thrust at the TO init start of takeoff roll.1.7.2015 EN Official Journal of the European Union L 168/67 The use of this constant thrust increment (instead of using the quadratic form (equation (2.7.8)) aims at being consistent with the linear relationship between thrust and speed in the case of jet-engine aircraft (eq. B-1). Segmentation of the initial climb segment During the initial climb segment the geometry is changing rapidly particularly with respect to observer locations to the side of the flight track, where beta angle will change rapidly as the aircraft climbs through this initial segment. Comparisons with very small segment calculations show that a single climb segment results in a poor approximation of noise to the side of the flight track for integrated metrics. Calculation accuracy is improved by sub-segmenting the first lift-off segment. The length of each segment and number is strongly influenced by lateral attenuation. Noting the expression of total lateral attenuation for aircraft with fuselage-mounted engines, it can be shown that for a limiting change in lateral attenuation of 1,5 dB per sub-segment, that the initial climb segment shall be sub-segmented based on the following set of height values: z = {18,9, 41,5, 68,3, 102,1, 147,5, 214,9, 334,9, 609,6, 1 0289,6} metres, or z = {62, 136, 224, 335, 484, 705, 1 099, 2 000, 4 231} feet The above heights are implemented by identifying which height in the set above is closest to the original segment endpoint. The actual sub-segment heights would then be calculated using: z′ = z [z/z ] (i = 1…N) (2.7.15) i i N where z is the original segment end height, z is the ith member of the set of height values and z is the closest i N upper bound to height z. This process results in the lateral attenuation change across each sub-segment remaining constant, producing more accurate contours, but without the expense of using very short segments. Example: If the original segment endpoint height is at z = 304,8 m, then from the set of height values, 214,9 < 304,8 < 334,9 and the closest upper bound is to z = 304,8 m is z = 334,9 m. The sub-segment 7 endpoint heights are then computed by: z′ = 304,8 [z/334,9] (i = 1..N) i i Thus z ′ would be 17,2 m and z ′ would be 37,8 m, etc. 1 2 The speed and engine power values on the inserted points are interpolated using respectively equations (2.7.11) and (2.7.13) Segmentation of airborne segments After the segmented flight path has been derived according to the procedure described in Section 2.7.13 and the sub-segmenting described is applied, further segmentation adjustments may be necessary. These include — the removal of flight path points which are too close together andL 168/68 EN Official Journal of the European Union 1.7.2015 — the insertion of additional points when speed changes along segments are too long. When adjacent points are within 10 metres of each other, and when the associated speeds and thrusts are the same, one of the points shall be eliminated. For airborne segments where there is a significant speed change along a segment, this shall be subdivided as for the ground roll, i.e. n ¼intð1þjV − V j=10Þ (2.7.16) seg 2 1 where V and V are the segment start and end speeds respectively. The corresponding sub-segment parameters 1 2 are calculated in a similar manner as for the takeoff ground roll, using equations (2.7.11) to (2.7.13). The landing ground roll Although the landing ground roll is essentially a reversal of the takeoff ground roll, special account has to be taken of — reverse thrust which is sometimes applied to decelerate the aircraft and — aeroplanes leaving the runway after deceleration (aircraft that leave the runway no longer contribute to air noise as noise from taxiing is disregarded). In contrast to the takeoff roll distance, which is derived from aircraft performance parameters, the stop distance s (i.e. the distance from touchdown to the point where the aircraft leaves the runway) is not purely aircraft stop specific. Although a minimum stop distance can be estimated from aircraft mass and performance (and available reverse thrust), the actual stop distance depends also on the location of the taxiways, on the traffic situation, and on airport-specific regulations on the use of reverse thrust. The use of reverse thrust is not a standard procedure — it is only applied if the needed deceleration cannot be achieved by the use of the wheel brakes. (Reverse thrust can be exceptionally disturbing as a rapid change of engine power from idle to reverse settings produces a sudden burst of noise.) However, most runways are used for departures as well as for landings so that reverse thrust has a very small effect on the noise contours since the total sound energy in the vicinity of the runway is dominated by the noise produced from takeoff operations. Reverse thrust contributions to contours may only be significant when runway use is limited to landing operations. Physically, reverse thrust noise is a very complex process but because of its relatively minor significance to air noise contours it can be modelled simplistically — the rapid change in engine power being taken into account by suitable segmentation. It is clear that modelling the landing ground roll is less straightforward than for takeoff roll noise. The following simplified modelling assumptions are recommended for general use, when no detailed information is available (see Figure 2.7.h).1.7.2015 EN Official Journal of the European Union L 168/69 Figure 2.7.h Modelling of landing ground roll The aeroplane touches down 300 meters beyond the landing threshold (which has the coordinate s = 0 along the approach ground track). The aircraft is then decelerated over a stop-distance s — aircraft specific values of stop which are given in the ANP database — from final approach speed V to 15 m/s. Because of the rapid changes final in speed during this segment it shall be sub-segmented in the same manner as for the takeoff ground roll (or airborne segments with rapid speed changes), using equations (2.7.10) to (2.7.13). The engine power changes from final approach power at touchdown to a reverse thrust power setting P over a rev distance 0,1 · s , then decreases to 10 % of the maximum available power over the remaining 90 percent of stop the stop distance. Up to the end of the runway (at s = – s ) aircraft speed remains constant. RWY NPD curves for reverse thrust are not at present included in the ANP database, and it is therefore necessary to rely on the conventional curves for modelling this effect. Typically the reverse thrust power P is around 20 % rev of the full power setting and this is recommended when no operational information is available. However, at a given power setting, reverse thrust tends to generate significantly more noise than forward thrust and an increment ΔL shall be applied to the NPD-derived event level, increasing from zero to a value ΔL (5 dB is rev recommended provisionally (1)) along 0,1 · s and then falling linearly to zero along the remainder of the stop stop distance. 2.7.14. Noise calculation for a single event The core of the modelling process, described here in full, is the calculation of the event noise level from the flight path information described in Sections 2.7.7 to 2.7.13. (1) This was recommended in the previous edition of ECAC Doc 29 but is still considered provisional pending the acquisition of further corroborative experimental data.L 168/70 EN Official Journal of the European Union 1.7.2015 2.7.15. Single event metrics The sound generated by an aircraft movement at the observer location is expressed as a ‘single event sound (or noise) level’, a quantity which is an indicator of its impact on people. The received sound is measured in noise terms using a basic decibel scale L(t) which applies a frequency weighting (or filter) to mimic a characteristic of human hearing. The scale of most importance in aircraft noise contour modelling is A-weighted sound level, L . A The metric most commonly used to encapsulate entire events is ‘single event sound (or noise) exposure levels’, L, which account for all (or most of) the sound energy in the events. Making provisions for the time integration E that this involves gives rise to the main complexities of segmentation (or simulation) modelling. Simpler to model is an alternative metric L which is the maximum instantaneous level occurring during the event; max however it is L which is the basic building block of most modern aircraft noise indices and practical models E can in future be expected to embody both L and L. Either metric can be measured on different scales of max E noise; in this document only A-weighted sound level is considered. Symbolically, the scale is usually indicated by extending the metric suffix, i.e. L , L . AE Amax The single event sound (or noise) exposure level is expressed exactly as 0 1 Zt2 B1 C L ¼10�lg@ 10L ðtÞ=10dtA (2.7.17) E t 0 t1 where t denotes a reference time. The integration interval [t ,t ] is chosen to ensure that (nearly) all significant 0 1 2 sound in the event is encompassed. Very often, the limits t and t are chosen to span the period for which the 1 2 level L(t) is within 10 dB of L . This period is known as the ‘10-dB down’ time. Sound (noise) exposure levels max tabulated in the ANP database are 10-dB down values (1). For aircraft noise contour modelling, the main application of equation (2.7.17) is the standard metric Sound Exposure Level L (acronym SEL): AE 0 1 Zt2 B1 C L ¼10�lg@ 10LAðtÞ=10dtAwith t = 1 second (2.7.18) AE t 0 0 t1 The exposure level equations above can be used to determine event levels when the entire time history of L(t) is known. Within the recommended noise modelling methodology such time histories are not defined; event exposure levels are calculated by summing segment values, partial event levels each of which defines the contribution from a single, finite segment of the flight path. 2.7.16. Determination of event levels from NPD-data The principal source of aircraft noise data is the international Aircraft Noise and Performance (ANP) database. This tabulates L and L as functions of propagation distance d — for specific aircraft types, variants, flight max E configurations (approach, departure, flap settings), and power settings P. They relate to steady flight at specific reference speeds V along a notionally infinite, straight flight path (2). ref (1) 10dB-down L may be up to 0,5 dB lower than L evaluated over a longer duration. However, except at short slant distances where event E E levels are high, extraneous ambient noise often makes longer measurement intervals impractical and 10-dB down values are the norm. As studies of the effects of noise (used to ‘calibrate’ the noise contours) also tend to rely on 10-dB down values, the ANP tabulations are considered to be entirely appropriate. (2) Although the notion of an infinitely long flight path is important to the definition of event sound exposure level L, it has less relevance E in the case of event maximum level L which is governed by the noise emitted by the aircraft when at a particular position at or near its max closest point of approach to the observer. For modelling purposes the NPD distance parameter is taken to be the minimum distance between the observer and segment.1.7.2015 EN Official Journal of the European Union L 168/71 How values of the independent variables P and d are specified is described later. In a single look-up, with input values P and d, the output values required are the baseline levels L (P,d) and/or L (P,d) (applicable to an infinite max E∞ flight path). Unless values happen to be tabulated for P and/or d exactly, it will generally be necessary to estimate the required event noise level(s) by interpolation. A linear interpolation is used between tabulated power-settings, whereas a logarithmic interpolation is used between tabulated distances (see Figure 2.7.i). Figure 2.7.i Interpolation in noise-power-distance curves If P and P are engine power values for which noise level versus distance data are tabulated, the noise level i i + 1 L(P) at a given distance for intermediate power P, between P and P , is given by: i i + 1 LðP Þ − LðPÞ LðPÞ¼LðPÞþ iþ1 i �ðP − PÞ (2.7.19) i P − P i iþ1 i If, at any power setting, d and d are distances for which noise data are tabulated, the noise level L(d) for an i i + 1 intermediate distance d, between d and d is given by i i + 1 Lðd Þ − LðdÞ LðdÞ¼LðdÞþ iþ1 i �ðlgd − lgdÞ (2.7.20) i lgd − lgd i iþ1 i By using equations (2.7.19) and (2.7.20), a noise level L(P,d) can be obtained for any power setting P and any distance d that is within the envelope of the NPD data base. For distances d that lie outside the NPD envelope, equation (2.7.20) is used to extrapolate from the last two values, i.e. inwards from L(d ) and L(d ) or outwards from L(d ) and L(d) where I is the total number of NPD 1 2 I – 1 I points on the curve. Thus Lðd Þ − Lðd Þ Inwards: LðdÞ¼Lðd Þþ 1 2 �ðlgd − lgdÞ (2.7.21) 2 lgd − lgd 2 2 1 Lðd Þ − LðdÞ Outwards: LðdÞ¼Lðd Þ − I − 1 I �ðlgd − lgd Þ (2.7.22) I − 1 lgd − lgd I − 1 I I − 1 As, at short distances d, noise levels increase very rapidly with decreasing propagation distance, it is recommended that a lower limit of 30 m be imposed on d, i.e. d = max(d, 30 m).L 168/72 EN Official Journal of the European Union 1.7.2015 Impedance adjustment of standard NPD data The NPD data provided in the ANP database are normalised to specific atmospheric conditions (temperature of 25 °C and pressure of 101,325 kPa). Before applying the interpolation/extrapolation method previously described, an acoustic impedance adjustment shall be applied to these standard NPD data. Acoustic impedance is related to the propagation of sound waves in an acoustic medium, and is defined as the product of the density of air and the speed of sound. For a given sound intensity (power per unit area) perceived at a specific distance from the source, the associated sound pressure (used to define SEL and L metrics) Amax depends on the acoustic impedance of the air at the measurement location. It is a function of temperature, atmospheric pressure (and indirectly altitude). There is therefore a need to adjust the standard NPD data of the ANP database to account for the actual temperature and pressure conditions at the receiver point, which are generally different from the normalised conditions of the ANP data. The impedance adjustment to be applied to the standard NPD levels is expressed as follows: � � ρ �c Δ ¼10�lg (2.7.23) Impedance 409,81 where: Δ Impedance adjustment for the actual atmospheric conditions at the receiver point (dB) Impedance ρ · c Acoustic impedance (newton · seconds/m3) of the air at the receiver point (409,81 being the air impedance associated to the reference atmospheric conditions of the NPD data in the ANP database). Impedance ρ · c is calculated as follows: (2.7.24) δ p/p, the ratio of the ambient air pressure at the observer altitude to the standard air pressure at mean sea o level: p = 101,325 kPa (or 1013,25 mb) o θ (T + 273,15)/(T + 273,15) the ratio of the air temperature at the observer altitude to the standard air 0 temperature at mean sea level: T = 15,0 °C 0 The acoustic impedance adjustment is usually less than a few tenths of one dB. In particular, it should be noted that under the standard atmospheric conditions (p = 101,325 kPa and T = 15,0 °C), the impedance adjustment o 0 is less than 0,1 dB (0,074 dB). However, when there is a significant variation in temperature and atmospheric pressure relative to the reference atmospheric conditions of the NPD data, the adjustment can be more substantial. 2.7.17. General expressions Segment event level Lseg The segment values are determined by applying adjustments to the baseline (infinite path) values read from the NPD data. The maximum noise level from one flight path segment L can be expressed in general as max,seg (2.7.25)1.7.2015 EN Official Journal of the European Union L 168/73 and the contribution from one flight path segment to L as E (2.7.26) The ‘correction terms’ in equations (2.7.25) and (2.7.26) — which are described in detail in Section 2.7.19 — account for the following effects: Δ Duration correction: the NPD data relate to a reference flight speed. This adjusts exposure levels to non- V reference speeds. (It is not applied to L .) max,seg Δ (φ) Installation effect: describes a variation in lateral directivity due to shielding, refraction and reflection I caused by the airframe, engines and surrounding flow fields. Λ(β,‘) Lateral attenuation: significant for sound propagating at low angles to the ground, this accounts for the interaction between direct and reflected sound waves (ground effect) and for the effects of atmospheric non-uniformities (primarily caused by the ground) that refract sound waves as they travel towards the observer to the side of the flight path. Δ Finite segment correction (noise fraction): accounts for the finite length of the segment which obviously F contributes less noise exposure than an infinite one. It is only applied to exposure metrics. If the segment is part of the take-off or landing ground roll and the observer is located behind the segment under consideration, special steps are taken to represent the pronounced directionality of jet engine noise that is observed behind an aircraft about to takeoff. These special steps result in particular in the use of a particular form of the noise for the exposure level: (2.7.27) (2.7.28) Δ′ Particular form of the Segment correction F Δ Directivity correction: accounts for the pronounced directionality of jet engine noise behind the ground roll SOR segment The specific treatment of ground roll segments is described in Section 2.7.19. Sections below describe the calculation of segment noise levels. Event noise level L of an aircraft movement Maximum level L is simply the greatest of the segment values L (see equations (2.7.25) and (2.7.27)) max max,seg L = max(L ) (2.7.29) max max,seg where each segment value is determined from the aircraft NPD data for power P and distance d. These parameters and the modifier terms Δ (φ) and Λ(β,‘) are explained below. I Exposure level L is calculated as the decibel sum of the contributions L from each noise-significant segment E E,seg of its flight path; i.e. �X � L ¼10�lg 10LE,seg=10 (2.7.30) EL 168/74 EN Official Journal of the European Union 1.7.2015 The summation proceeds step by step through the flight path segments. The remainder of this chapter is concerned with the determination of the segment noise levels L and L . max,seg E,seg 2.7.18. Flight path segment parameters The power P, and distance d, for which the baseline levels L (P,d) and L (P,d) are interpolated from the NPD max,seg E∞ tables, are determined from geometric and operational parameters that define the segment. How this is done is explained below with the aid of illustrations of the plane containing the segment and the observer. Geometric parameters Figures 2.7.j to 2.7.l show the source-receiver geometries when the observer O is (a) behind, (b) alongside and (c) ahead of the segment S S where the flight direction is from S to S . In these diagrams 1 2 1 2 O is the observer location S , S are the start and end of the segment 1 2 S is the point of perpendicular closest approach to the observer on the segment or its extension p d d are the distances between start, end of segment and observer 1, 2 d is the shortest distance between observer and segment s d is the perpendicular distance between observer and extended segment (minimum slant range) p λ is the length of flight path segment q is the distance from S to S (negative if the observer position is behind the segment) 1 p Figure 2.7.j Flight path segment geometry for observer behind segment1.7.2015 EN Official Journal of the European Union L 168/75 Figure 2.7.k Flight path segment geometry for observer alongside segment Figure 2.7.l Flight path segment geometry for observer ahead of segment The flight path segment is represented by a bold, solid line. The dotted line represents the flight path extension which stretches to infinity in both directions. For airborne segments, when the event metric is an exposure level L, the NPD distance parameter d is the distance d between S and the observer, called the minimum slant range E p p (i.e. the perpendicular distance from the observer to the segment or its extension, in other words to the (hypothetical) infinite flight path of which the segment is considered to be part). However, for exposure level metrics where observer locations are behind the ground segments during the takeoff roll and locations ahead of ground segments during the landing roll, the NPD distance parameter d becomes the distance d, the shortest distance from the observer to the segment (i.e. the same as for maximum s level metrics). For maximum level metrics, the NPD distance parameter d is d, the shortest distance from the observer to the s segment.L 168/76 EN Official Journal of the European Union 1.7.2015 Segment power P The tabulated NPD data describe the noise of an aircraft in steady straight flight on an infinite flight path, i.e. at constant engine power P. The recommended methodology breaks actual flight paths, along which speed and direction vary, into a number of finite segments, each of which is then taken to be part of a uniform, infinite flight path for which the NPD data are valid. But the methodology provides for changes of power along the length of a segment; it is taken to change linearly with distance from P at its start to P at its end. It is therefore 1 2 necessary to define an equivalent steady segment value P. This is taken to be the value at the point on the segment that is closest to the observer. If the observer is alongside the segment (Figure 2.7.k) it is obtained by interpolation as given by equation (2.7.8) between the end values, i.e. rffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi q P¼ P2þ �ðP2 − P2Þ (2.7.31) 1 λ 2 1 If the observer is behind or ahead of the segment, it is that at the nearest end point, P or P . 1 2 2.7.19. Segment Event level correction terms The NPD data define noise event levels as a function of distance perpendicularly beneath an idealised straight level path of infinite length along which the aircraft flies with steady power at a fixed reference speed (1). The event level interpolated from the NPD table for a specific power setting and slant distance is thus described as a baseline level. It applies to an infinite flight path and has to be corrected to account for the effects of (1) non- reference speed, (2) engine installation effects (lateral directivity), (3) lateral attenuation, (4) finite segment length and (5) longitudinal directivity behind start of roll on takeoff — see equations (2.7.25) and (2.7.26). The duration correction DV (Exposure levels LE only) This correction (2) accounts for a change in exposure levels if the actual segment groundspeed is different to the aircraft reference speed V to which the basic NPD-data relate. Like engine power, speed varies along the ref segment (groundspeed varies from V to V ) and it is necessary to define an equivalent segment speed V 1 2 seg remembering that the segment is inclined to the ground; i.e. V = V/cosγ (2.7.32) seg where here V is an equivalent segment groundspeed (for information, see equation B-22 which expresses V in terms of calibrated airspeed, V and c � � z − z γ¼tan − 1 2 1 (2.7.33) s − s 2 1 For airborne segments, V is taken to be the groundspeed at the closest point of approach S — interpolated between the segment end-point values assuming it varies linearly with time; i.e. if the observer is alongside the segment: rffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi q V¼ V2þ �ðV2 − V2Þ (2.7.34) 1 λ 2 1 (1) NPD specifications require that the data be based on measurements of steady straight flight, not necessarily level; to create the necessary flight conditions, the test aircraft flight path can be inclined to the horizontal. However, as will be seen, inclined paths lead to computa­ tional difficulties and, when using the data for modelling, it is convenient to visualise the source paths as being both straight and level. (2) This is known as the duration correction because it makes allowance for the effects of aircraft speed on the duration of the sound event — implementing the simple assumption that, other things being equal, duration, and thus received event sound energy, is inversely proportional to source velocity.1.7.2015 EN Official Journal of the European Union L 168/77 If the observer is behind or ahead of the segment, it is that at the nearest end point, V or V . 1 2 For runway segments (parts of the take-off or landing ground rolls for which γ = 0) V is taken to be simply seg the average of the segment start and end speeds; i.e. V = (V + V )/2 (2.7.35) seg 1 2 In either case the additive duration correction is then Δ = 10 · lg(V /V ) (2.7.36) V ref seg Sound propagation geometry Figure 2.7.l shows the basic geometry in the plane normal to the aircraft flight path. The ground line is the intersection of the normal plane and the level ground plane. (If the flight path is level the ground line is an end view of the ground plane.) The aircraft is banked at angle ε measured counter-clockwise about its roll axis (i.e. starboard wing up). It is therefore positive for left turns and negative for right turns. Figure 2.7.m Aircraft-observer angles in plane normal to flight path — The elevation angle β (between 0 and 90°) between the direct sound propagation path and the level ground line (1) determines, together with the flight path inclination and the lateral displacement ‘ of the observer from the ground track, the lateral attenuation. — The depression angle φ between the wing plane and the propagation path, determines the engine installation effects. With respect to the convention for the bank angle φ = β ± ε with the sign positive for observers to starboard (right) and negative for observers to port (left). (1) In the case of non-flat terrain there can be different definitions of elevation angle. Here it is defined by the aircraft height above the observation point and the slant distance — hence neglecting local terrain gradients as well as obstacles on the sound propagation path (see Sections 2.7.6 and 2.7.10). In the event that, due to ground elevation, the receiver point is above the aircraft, elevation angle β is set equal to zero.L 168/78 EN Official Journal of the European Union 1.7.2015 Engine installation correction ΔI An aircraft in flight is a complex sound source. Not only are the engine (and airframe) sources complex in origin, but the airframe configuration, particularly the location of the engines, influences the noise radiation patterns through the processes of reflection, refraction and scattering by the solid surfaces and aerodynamic flow fields. This results in a non-uniform directionality of sound radiated laterally about the roll axis of the aircraft, referred to here as lateral directivity. There are significant differences in lateral directivity between aircraft with fuselage-mounted and underwing- mounted engines and these are allowed for in the following expression: � � ΔðφÞ¼10�lg ða�cos2φþsin2φÞb=ðc�sin22φþcos22φÞ dB (2.7.37) I where Δ (φ) is the correction, in dB, at depression angle φ (see Figure 2.7.m) and I a = 0,00384, b = 0,0621, c = 0,8786 for wing-mounted engines and a = 0,1225, b = 0,3290, c = 1 for fuselage-mounted engines. For propeller aircraft directivity variations are negligible and for these it may be assumed that Δ(φ) = 0 (2.7.38) I Figure 2.7.n shows the variation of Δ(φ) about the aircraft roll axis for the three engine installations. These I empirical relationships have been derived by the SAE from experimental measurements made mainly beneath the wing. Until above-wing data have been analysed it is recommended that, for negative φ, Δ(φ) = Δ(0) for all I I installations. Figure 2.7.n Lateral directivity of installation effects1.7.2015 EN Official Journal of the European Union L 168/79 It is assumed that Δ (φ) is two-dimensional; i.e. it does not depend on any other parameter — and in particular I that it does not vary with the longitudinal distance of the observer from the aircraft. This means that the elevation angle β for Δ (φ) is defined as β = tan–1(z/‘). This is for modelling convenience until there is a better I understanding of the mechanisms; in reality, installation effects are bound to be substantially three-dimensional. Despite that, a two-dimensional model is justified by the fact that event levels tend to be dominated by noise radiated sideways from the nearest segment. Lateral attenuation Λ(β,‘) (infinite flight path) Tabulated NPD event levels relate to steady level flight and are generally based on measurements made 1,2 m over soft level ground beneath the aircraft; the distance parameter is effectively height above the surface. Any effect of the surface on event noise levels beneath the aircraft, that might cause the tabulated levels to differ from free-field values (1), is assumed to be inherent in the data (i.e. in the shape of the level vs. distance relationships). To the side of the flight path, the distance parameter is the minimum slant distance — the length of the normal from the receiver to the flight path. At any lateral position the noise level will generally be less than at the same distance immediately below the aircraft. Apart from lateral directivity or ‘installation effects’ described above is due to an excess lateral attenuation which causes the sound level to fall more rapidly with distance than indicated by the NPD curves. A previous, widely used method for modelling lateral propagation of aircraft noise was developed by the Society of Automotive Engineers (SAE) in AIR-1751 and the algorithms described below are based on improvements SAE now recommends AIR-5662. Lateral attenuation is a reflection effect, due to interference between directly radiated sound and that which reflects from the surface. It depends on the nature of the surface and can cause significant reductions in observed sound levels at low elevation angles. It is also very strongly affected by sound refraction, steady and unsteady, caused by wind and temperature gradients and turbulence which are themselves attributable to the presence of the surface (2). The mechanism of surface reflection is well understood and, for uniform atmospheric and surface conditions, it can be described theore­ tically with some precision. However, atmospheric and surface non-uniformities — which are not amenable to simple theoretical analysis — have a profound effect on the reflection effect, tending to ‘spread’ it to higher elevation angles; thus the theory is of limited applicability. SAE work to develop a better understanding of surface effects is continuing and this is expected to lead to better models. Until these are developed, the following methodology, described in AIR-5662, is recommended for calculating lateral attenuation. It is confined to the case of sound propagation over soft level ground which is appropriate for the great majority of civil airports. Adjustments to account for the effects of a hard ground surface (or, acoustically equivalent, water) are still under development. The methodology is built on the substantial body of experimental data on sound propagation from aircraft with fuselage-mounted engines in straight (non-turning), steady, level flight reported originally in AIR-1751. Making the assumption that, for level flight, air-to-ground attenuation depends on (i) elevation angle β measured in the vertical plane and (ii) lateral displacement from the aircraft ground track ‘, the data were analysed to obtain an empirical function for the total lateral adjustment Λ(β,‘) (= lateral event level minus the level at the same T distance beneath the aircraft). As the term Λ(β,‘) accounted for lateral directivity as well as lateral attenuation, the latter can be extracted by T subtraction. Describing lateral directivity by equation (2.7.37), with the fuselage-mount coefficients and with φ replaced by β (appropriate to non-turning flight), the lateral attenuation becomes: (2.7.39) where β and ‘ are measured as depicted in Figure 2.7.m in a plane normal to the infinite flight path which, for level flight, is also vertical. (1) A ‘free-field’ level is that which would be observed if the ground surface were not there. (2) The wind and temperature gradients and turbulence depend in part upon the roughness and heat transfer characteristics of the surface.L 168/80 EN Official Journal of the European Union 1.7.2015 Although Λ(β,‘) could be calculated directly using equation (2.7.39) with Λ(β,‘) taken from AIR-1751, a more T efficient relationship is recommended. This is the following empirical approximation adapted from AIR-5662: (2.7.40) where Γ(‘) is a distance factor given by for 0 ≤ ‘≤ 914 m (2.7.41) for ‘> 914 m (2.7.42) and Λ(β) is long-range air-to-ground lateral attenuation given by Λ(β) = 1,137 – 0,0229β + 9,72 · exp(– 0,142β) for 0° ≤ β ≤ 50° (2.7.43) Λ(β) = 0 for 50° ≤ β ≤ 90° (2.7.44) The expression for lateral attenuation Λ(β,‘), equation (2.7.40), which is assumed to hold good for all aircraft, propeller aircraft as well as fuselage-mount and wing-mount jets, is shown graphically in Figure 2.7.o. Under certain circumstances (with terrain), it is possible for β to be less than zero. In such cases it is recommended that Λ(β) = 10,57. Figure 2.7.o Variation of lateral attenuation Λ(β,‘) with elevation angle and distance Finite segment lateral attenuation Equations (2.7.41) to (2.7.44) describe the lateral attenuation Λ(β,‘) of sound arriving at the observer from an aeroplane in steady flight along an infinite, level flight path. When applying them to finite path segments that are not level, the attenuation has to be calculated for an equivalent level path — as the closest point on a simple extension of the inclined segment (that passes through the ground surface at some point) generally does not yield an appropriate elevation angle β.1.7.2015 EN Official Journal of the European Union L 168/81 The determination of lateral attenuation for finite segments differs markedly for L and L metrics. Segment max E maximum levels L are determined from NPD data as a function of propagation distance d from the nearest max point on the segment; no corrections are required to account for the dimensions of the segment. Likewise, lateral attenuation of L is assumed to depend only on the elevation angle of, and ground distance to, the same max point. Thus only the coordinates of that point are required. But for L, the process is more complicated. E The baseline event level L(P,d) that is determined from the NPD data, even though for finite segment E parameters, applies nevertheless to an infinite flight path. The event exposure level from a segment, L , is of E,seg course less than the baseline level — by the amount of the finite segment correction defined later in Section 2.7.19. That correction, a function of the geometry of triangles OS S in Figures 2.7.j to 2.7.l, defines 1 2 what proportion of the total infinite path noise energy received at O comes from the segment; the same correction applies, whether or not there is any lateral attenuation. But any lateral attenuation shall be calculated for the infinite flight path, i.e. as a function of its displacement and elevation, not those of the finite segment. Adding the corrections Δ and Δ, and subtracting lateral attenuation Λ(β,‘) from the NPD baseline level gives the V I adjusted event noise level for equivalent steady level flight on an adjacent, infinite straight path. But the actual flight path segments being modelled, those that affect the noise contours, are rarely level; aircraft are usually climbing or descending.L 168/82 EN Official Journal of the European Union 1.7.2015 Figure 2.7.p illustrates a departure segment S S — the aircraft is climbing at an angle γ — but the consider­ 1 2 ations remain very similar for an arrival. The remainder of the ‘real’ flight path is not shown; suffice it to state that S S represents just a part of the whole path (which in general will be curved). In this case, the observer O 1 2 is alongside, and to the left of, the segment. The aircraft is banked (anti-clockwise about the flight path) at an angle ε to the lateral horizontal axis. The depression angle φ from the wing plane, of which the installation effect Δ is a function (equation (2.7.39)), lies in the plane normal to the flight path in which ε is defined. Thus I φ = β – ε where β = tan–1(h/‘) and ‘ is the perpendicular distance OR from the observer to the ground track; i.e. the lateral displacement of the observer (1). The aeroplane's closest point of approach to the observer, S, is defined by the perpendicular OS, of length (slant distance) d. The triangle OS S accords with Figure 2.7.k, the p 1 2 geometry for calculating the segment correction Δ. F Figure 2.7.p Observer alongside segment To calculate the lateral attenuation using equation (2.7.40) (where β is measured in a vertical plane), an equivalent level flight path is defined in the vertical plane through S S and with the same perpendicular slant distance d 1 2 p from the observer. This is visualised by rotating the triangle ORS, and its attached flight path about OR (see Figure 2.7.p) through angle γ thus forming the triangle ORS′. The elevation angle of this equivalent level path (now in a vertical plane) is β = tan–1(h/‘) (‘ remains unchanged). In this case, observer alongside, the lateral attenuation Λ(β,‘) is the same for L and L metrics. E max (1) For an observer located on the right side to the segment φ would become β + ε (see Section 2.7.19).1.7.2015 EN Official Journal of the European Union L 168/83 Figure 2.7.q illustrates the situation when the observer point O lies behind the finite segment, not alongside. Here the segment is observed as a more distant part of an infinite path; a perpendicular can only be drawn to point S on its extension. The triangle OS S accords with Figure 2.7.j which defines the segment correction Δ. But p 1 2 F in this case the parameters for lateral directivity and attenuation are less obvious. Figure 2.7.q Observer behind segment Remembering that, as conceived for modelling purposes, lateral directivity (installation effect) is two- dimensional, the defining depression angle φ is still measured laterally from the aircraft wing plane. (The baseline event level is still that generated by the aircraft traversing the infinite flight path represented by the extended segment.) Thus the depression angle is determined at the closest point of approach, i.e. φ = β - ε p where β is angle S OC. p p For maximum level metrics, the NPD distance parameter is taken as the shortest distance to the segment, i.e. d = d . For exposure level metrics, it is the shortest distance d from O to S on the extended flight path; 1 p p i.e. the level interpolated from the NPD table is L (P , d). E∞ 1 p The geometrical parameters for lateral attenuation also differ for maximum and exposure level calculations. For maximum level metrics the adjustment L(β,‘) is given by equation (2.7.40) with β = β = sin–1(z /d ) and 1 1 1 where β and d are defined by the triangle OC S in the vertical plane through O and 1 1 1 1 S . 1 When calculating the lateral attenuation for airborne segments only and exposure level metrics, ‘ remains the shortest lateral displacement from the segment extension (OC). But to define an appropriate value of β it is again necessary to visualise an (infinite) equivalent level flight path of which the segment can be considered part. This is drawn through S ′, height h above the surface, where h is equal to the length of RS the perpendicular 1 1 from the ground track to the segment. This is equivalent to rotating the actual extended flight path through angle γ about point R (see Figure 2.7.q). Insofar as R is on the perpendicular to S , the point on the segment 1 that is closest to O, the construction of the equivalent level path is the same as when O is alongside the segment.L 168/84 EN Official Journal of the European Union 1.7.2015 The closest point of approach of the equivalent level path to the observer O is at S′, slant distance d, so that the triangle OCS′ so formed in the vertical plane then defines the elevation angle β = cos–1(‘/d). Although this trans­ formation might seem rather convoluted, it should be noted that the basic source geometry (defined by d , d 1 2 and φ) remains untouched, the sound travelling from the segment towards the observer is simply what it would be if the entire flight along the infinitely extended inclined segment (of which for modelling purposes the segment forms part) were at constant speed V and power P . The lateral attenuation of sound from the segment 1 received by the observer, on the other hand, is related not to β, the elevation angle of the extended path, but to p β, that of the equivalent level path. The case of an observer ahead of the segment is not described separately; it is evident that this is essentially the same as the case of the observer behind. However, for exposure level metrics where observer locations are behind ground segments during the takeoff roll and locations ahead of ground segments during the landing roll, the value of β becomes the same as that for maximum level metrics, i.e. β = β = sin–1(z /d ) and 1 1 1 The finite segment correction Δ (Exposure levels L only) F E The adjusted baseline noise exposure level relates to an aircraft in continuous, straight, steady level flight (albeit with a bank angle ε that is inconsistent with straight flight). Applying the (negative) finite segment correction Δ = 10 · lg(F), where F is the energy fraction, further adjusts the level to what it would be if the aircraft traversed F the finite segment only (or were completely silent for the remainder of the infinite flight path). The energy fraction term accounts for the pronounced longitudinal directivity of aircraft noise and the angle subtended by the segment at the observer position. Although the processes that cause the directionality are very complex, studies have shown that the resulting contours are quite insensitive to the precise directional character­ istics assumed. The expression for Δ below is based on a fourth-power 90-degree dipole model of sound F radiation. It is assumed to be unaffected by lateral directivity and attenuation. How this correction is derived is described in detail in Appendix E. The energy fraction F is a function of the ‘view’ triangle OS S defined in Figures 2.7.j to 2.7.l such that: 1 2 � � �� 1 α α Δ ¼10�lg 2 þarctanα − 1 − arctanα (2.7.45) F π 1þα2 2 1þα2 1 2 1 with α 1 ¼ − dq λ; α 2 ¼ − q d− λ λ ; d λ ¼d 0�10½LE∞ðP,dpÞ − LmaxðP,dpÞ�=10; d 0 ¼2 π�V ref �t 0. where d is known as the ‘scaled distance’ (see Appendix E). Note that L (P, d) is the maximum level, from λ max p NPD data, for perpendicular distance d, NOT the segment L . p max It is advised to apply a lower limit of – 150 dB to Δ. F In the particular case of observer locations behind every takeoff ground-roll segment and every landing ground- roll segment, a reduced form of the noise fraction expressed in equation (2.7.45) is used, which corresponds to the specific case of q = 0. This is computed using � � � � Δ ¼10 log ð1=πÞ α =ð1þα2Þþtan − 1α 10ΔSOR=10 (2.7.46) F′ 10 2 2 2 where α = λ/d and Δ is the start-of-roll directivity function defined by equations (2.7.51) and (2.7.52). 2 λ SOR1.7.2015 EN Official Journal of the European Union L 168/85 The rationale for using this particular form of noise fraction is further explained in the section below, as part of the start-of-roll directivity application method. Specific Treatments of Ground-roll Segments, including the start-of-roll directivity function Δ SOR In the case of ground roll segments, both for takeoff and landing, specific treatments are applied, which are described below. The start-of-roll directivity function Δ SOR The noise of jet aircraft — especially those equipped with lower by-pass ratio engines — exhibits a lobed radiation pattern in the rearward arc, which is characteristic of jet exhaust noise. This pattern is the more pronounced the higher the jet velocity and the lower the aircraft speed. This is of special significance for observer locations behind the start of roll, where both conditions are fulfilled. This effect is taken into account by a directivity function Δ . SOR The function Δ has been derived from several noise measurement campaigns using microphones adequately SOR positioned behind and on the side of the SOR of departing jet aircraft. Figure 2.7.r shows the relevant geometry. The azimuth angle ψ between the aircraft longitudinal axis and the vector to the observer is defined by � � q ψ¼arccos . (2.7.47) d SOR The relative distance q is negative (see Figure 2.7.j) so that ψ ranges from 0° in the direction of the aircraft forward heading to 180° in the reverse direction. Figure 2.7.r Aircraft-observer geometry at ground for estimation of directivity correction The function Δ represents the variation of the overall noise emanating from the takeoff ground roll measured SOR behind the start of roll, relatively to the overall noise from takeoff ground roll measured on the side of the SOR, at the same distance: L (d ,ψ) = L (d ,90°) + Δ (d ,ψ) (2.7.48) TGR SOR TGR SOR SOR SORL 168/86 EN Official Journal of the European Union 1.7.2015 where L (d ,90°) is the overall takeoff ground roll noise level generated by all takeoff ground roll segments at TGR SOR the point distance d to the side of the SOR. At distances d less than a normalising distance d , the SOR SOR SOR SOR,0 directivity function is given by Δ0 ¼51,47 − 1,553�ψþ0,015147�ψ2 − 0,000047173�ψ3 if 90° ≤ ψ < 148,4° (2.7.49) SOR Δ0 ¼339,18 − 2,5802�ψ − 0,0045545�ψ2þ0,000044193�ψ3 if 148,4° ≤ ψ ≤ 180° (2.7.50) SOR If the distance d exceeds the normalising distance d , the directivity correction is multiplied by a correction SOR SOR,0 factor to account for the fact that the directivity becomes less pronounced for greater distances from the aircraft; i.e. Δ ¼Δ0 if d ≤ d (2.7.51) SOR SOR SOR SOR,0 d Δ ¼Δ0 � SOR,0 if d > d (2.7.52) SOR SOR d SOR SOR,0 SOR The normalising distance d equals 762 m (2 500 ft). SOR,0 Treatment of receivers located behind each takeoff and landing ground-roll segment The Δ function described above mostly captures the pronounced directivity effect of the initial portion of the SOR takeoff roll at locations behind the SOR (because it is the closest to the receivers, with the highest jet velocity to aircraft speed ratio). However, the use of the hence established Δ is ‘generalised’ to positions behind each SOR individual ground roll segment — both takeoff and landing —, so not only behind the Start-of-Roll point (in the case of takeoff). The parameters d and ψ are calculated relative to the start of each individual ground roll segment. S The event level L for a location behind a given takeoff or landing ground-roll segment is calculated to comply seg with the formalism of the Δ function: it is essentially calculated for the reference point located on the side of SOR the start point of the segment, at the same distance d as the actual point, and is further adjusted with Δ to S SOR obtain the event level at the actual point. This means that the different correction terms in the equations below shall use the geometric parameters corresponding to this reference point located on the side of the start point: L = L (P,d = d) + Δ(φ) – Λ(β,l = d) + Δ (2.7.53) max,seg max s I s SOR L = L (P,d = d) + Δ + Δ(φ) – Λ(β,l = d) + Δ′ + Δ (2.7.54) E,seg E,∞ s V I s F SOR where Δ′ is the reduced form of the noise fraction expressed in equation (2.7.46) for the case of q = 0 (as the F reference point is located on the side of the start point) and remembering that d shall be calculated using d λ S (and not d): p d ¼d �10½LE∞ðP,dsÞ − LmaxðP,dsÞ�=10 (2.7.55) λ 0 2.7.20. Event noise level L of a general-aviation aircraft movement The method described in Section 2.7.19 is applicable to propeller-engined general-aviation aircraft when they are treated as propeller aircraft with regard to engine installation effects.1.7.2015 EN Official Journal of the European Union L 168/87 The ANP database includes entries for several general aviation aircraft. Whilst these are often the most common general-aviation aircraft operating, there may be occasions when it is appropriate to use additional data. Where the specific general aviation aircraft are either not known or not in the ANP database, it is recommended to use the more generic aircraft data, GASEPF and GASEPV respectively. These data sets represent a small single- engined general aviation aircraft with fixed-pitch and variable-pitch propellers respectively. Tables of entries are presented in Annex I (Tables I-11 I-17) 2.7.21. Method for the Calculation of Helicopter Noise For the calculation of helicopter noise, the same calculation method used for fixed-wing aircraft (outlined in Section 2.7.14) may be used, provided helicopters are treated as propeller aircraft and engine-installation effects, associated with jet aircraft are not applied. Tables of entries for two different data sets are presented in Annex I (Tables I-18 I-27). 2.7.22. Noise associated with Engine Testing (Run-Up) Operations, taxiing and auxiliary power units In such cases where it is considered that noise associated with engine testing and auxiliary power-units are to be modelled, these are modelled according to the chapter on industrial noise. Although it is normally not the case, noise from aircraft engine tests (sometimes referred to as ‘engine run-ups’) at airports can make a contribution to noise impacts. Usually carried out for engineering purposes to check engine performance, aircraft are safely positioned away from buildings, aircraft, vehicular and/or personnel movements to avoid any jet-blast related damage. For additional safety and noise control reasons, airports, particularly those with maintenance facilities that can lead to frequent engine tests, can install so-called ‘noise pens’, 3-sided baffled enclosures specially designed to deflect and dissipate jet blast and noise. Investigating the noise impact of such facilities, which can be further attenuated and reduced by the use of additional earth bunds or substantial noise barrier fencing, is best accomplished by treating the noise pen as a source of industrial noise and using an appropriate noise and sound propagation model. 2.7.23. Calculation of cumulative levels Sections 2.7.14 to 2.7.19 describe the calculation of the event sound noise level of a single aircraft movement at a single observer location. The total noise exposure at that location is calculated by accumulating the event levels of all noise-significant aircraft movements, i.e. all movements, inbound or outbound, that influence the cumulative level. 2.7.24. Weighted equivalent sound levels Time-weighted equivalent sound levels, which account for all significant aircraft sound energy received, shall be expressed in a generic manner by the formula " # t XN L ¼10�lg 0 � g �10LE,i=10 þC (2.7.56) eq,W T i 0 i¼1 The summation is performed over all N noise events during the time interval T to which the noise index 0 applies. L is the single event noise exposure level of the i-th noise event. g is a time-of-day dependent E,i i weighting factor (usually defined for day, evening and night periods). Effectively g is a multiplier for the number i of flights occurring during the specific periods. The constant C can have different meanings (normalising constant, seasonal adjustment etc.).L 168/88 EN Official Journal of the European Union 1.7.2015 Using the relationship g ¼10Δi=10 i where Δ is the decibel weighting for the i-th period, equation (2.7.56) can be rewritten as i " # t XN L ¼10�lg 0 10ðLE,iþΔiÞ=10 þC (2.7.57) eq,W T 0 i¼1 i.e. the time-of-day weighting is expressed by an additive level offset. 2.7.25. The weighted number of operations The cumulative noise level is estimated by summing the contributions from all different types or categories of aircraft using the different flight routes which comprise the airport scenario. To describe this summation process the following subscripts are introduced: i index for aircraft type or category j index for flight track or subtrack (if subtracks are defined) k index for flight track segment Many noise indices — especially equivalent sound levels — include time-of-day weighting factors g in their i definition (equations (2.7.56) and (2.7.57)). The summation process can be simplified by introducing a ‘weighted number of operations’ M = (g · N + g · N + g · N ) (2.7.58) ij day ij,day evening ij,evening night ij,night The values N represent the numbers of operations of aircraft type/category i on track (or subtrack) j during the ij day, evening and night period respectively (1). From equation (2.7.57) the (generic) cumulative equivalent sound level L at the observation point (x,y) is eq " # XXX t L ðx,yÞ¼10�lg 0 � M �10LE,ijkðx,yÞ=10 þC (2.7.59) eq,W T ij 0 i j k T is the reference time period. It depends on — as well as the weighting factors g — the specific definition 0 i of the weighted index used (e.g. L ). L is the single event noise level contribution from segment k of track DEN E,ijk or subtrack j for an operation of aircraft of category i. The estimation of L is described in detail in E,ijk Sections 2.7.14 to 2.7.19. (1) The time periods may differ from these three, depending on the definition of the noise index used.1.7.2015 EN Official Journal of the European Union L 168/89 2.7.26. Standard grid calculation and refinement When noise contours are obtained by interpolation between index values at rectangularly spaced grid points, their accuracy depends on the choice of the grid spacing (or mesh size) Δ , especially within cells where large G gradients in the spatial distribution of the index cause tight curvature of the contours (see Figure 2.7.s). Interpo­ lation errors are reduced by narrowing the grid spacing, but as this increases the number of grid points, the computation time is increased. Optimising a regular grid mesh involves balancing modelling accuracy and run time. Figure 2.7.s Standard grid and grid refinement A marked improvement in computing efficiency that delivers more accurate results is to use an irregular grid to refine the interpolation in critical cells. The technique, depicted in Figure 2.7.s, is to tighten the mesh locally, leaving the bulk of the grid unchanged. This is very straightforward and achieved by the following steps: (1) Define a refinement threshold difference ΔL for the noise index. R (2) Calculate the basic grid for a spacing Δ . G (3) Check the differences ΔL of the index values between adjacent grid nodes. (4) If there are any differences ΔL > DL , define a new grid with a spacing Δ /2 and estimate the levels for the R G new nodes in the following way: 8 8 ><ΔL ≤ ΔL ><by linear interpolation from the adjacent ones. R If calculate the new value >: >: ΔL > ΔL completely anew from the basic input data. RL 168/90 EN Official Journal of the European Union 1.7.2015 (5) Repeat steps 1-4 until all differences are less than the threshold difference. (6) Estimate the contours by linear interpolation. If the array of index values is to be aggregated with others (e.g. when calculating weighted indices by summing separate day, evening and night contours) care is required to ensure that the separate grids are identical. 2.7.27. Use of rotated grids In many practical cases, the true shape of a noise contour tends to be symmetrical about a ground track. However if the direction of this track is not aligned with the calculation grid, this can cause result in an asymmetric contour shape. Figure 2.7.t Use of a rotated grid The straightforward way to avoid this effect is to tighten the grid. However this increases computation time. A more elegant solution is to rotate the computation grid so that its direction is parallel to the main ground tracks (i.e. usually parallel to the main runway). Figure 2.7.t shows the effect of such a grid rotation on the contour shape.1.7.2015 EN Official Journal of the European Union L 168/91 2.7.28. Tracing of contours A very time-efficient algorithm that eliminates the need to calculate a complete grid array of index values at the expense of a little more computational complexity is to trace the path of the contour, point by point. This option requires two basic steps to be performed and repeated (see Figure 2.7.u): Figure 2.7.u Concept of tracing algorithm Step 1 is to find a first point P on the contour. This is done by calculating the noise index levels L in 1 equidistant steps along a ‘search ray’ that is expected to cross the required contour of level L . When the C contour is crossed, the difference δ = L – L changes sign. If this happens, the step-width along the ray is halved C and the search direction is reversed. This is done until δ is smaller than a pre-defined accuracy threshold. Step 2, which is repeated until the contour is sufficiently well defined, is to find the next point on the contour L — which is at a specified straight line distance r from the current point. During consecutive angular steps, C index levels and differences δ are calculated at the ends of vectors describing an arc with radius r. By similarly halving and reversing the increments, this time in the directions of the vector, the next contour point is determined within a predefined accuracy. Figure 2.7.v Geometric parameters defining conditions for the tracing algorithm Some constraints shall be imposed to guarantee that the contour is estimated with a sufficient degree of accuracy (see Figure 2.7.v): (1) The length of the chord Δc (the distance between two contour points) shall be within an interval [Δc , min Δc ], e.g. [10 m, 200 m]. max (2) The length ratio between two adjacent chords of lengths Δc and Δc shall be limited, e.g. 0,5 < Δc/ n n+1 n Δc < 2. n + 1L 168/92 EN Official Journal of the European Union 1.7.2015 (3) With respect to a good fit of the chord length to the contour curvature the following condition shall be fulfilled: Φ· max(Δc , Δc) ≤ ε (ε≈ 15 m) n n – 1 n where Φ is the difference in the chord headings. n Experience with this algorithm has shown that, on an average, between 2 and 3 index values have to be calculated to determine a contour point with an accuracy of better than 0,01 dB. Especially when large contours have to be calculated this algorithm speeds up computation time dramatically. However it should be noted that its implementation requires experience, especially when a contour breaks down into separate islands. 2.8. Assigning noise levels and population to buildings For the assessment of the noise exposure of the population only residential buildings shall be considered. No people shall be assigned to other buildings without residential use such as schools, hospitals, office buildings or factories. The assignment of the population to the residential buildings shall be based on the latest official data (depending on the Member State's relevant regulations). Because aircraft calculation are performed on a 100 m × 100 m resolution grid, the specific case of aircraft noise, levels shall be interpolated based on the nearest grid noise levels. Determination of the number of inhabitants of a building The number of inhabitants of a residential building is an important intermediate parameter for the estimation of the exposure to noise. Unfortunately, data on this parameter is not always available. Below it is specified how this parameter can be derived from data more readily available. Symbols used in the following are: BA = base area of the building DFS = dwelling floor space DUFS = dwelling unit floor space H = height of the building FSI = dwelling floor space per inhabitant Inh = number of inhabitants NF = number of floors V = volume of residential buildings For the calculation of the number of inhabitants, either the following case 1 procedure or the case 2 procedure shall be used, depending on the availability of data. CASE 1: the data on the number of inhabitants is available 1A: The number of inhabitants is known or has been estimated on the basis of dwelling units. In this case the number of inhabitants of a building is the sum of the number of inhabitants of all dwelling units in the building: Xn Inh ¼ Inh (2.8.1) building dwellinguniti i¼11.7.2015 EN Official Journal of the European Union L 168/93 1B: The number of inhabitants is known only for entities larger than a building, e.g. sides of city blocks, city blocks, districts or even an entire municipality. In this case the number of inhabitants of a building is estimated based on the volume of the building: V Inh ¼ building�Inh (2.8.2) building V total total The index ‘total’ here refers to the respective entity considered. The volume of the building is the product of its base area and its height: V = BA × H (2.8.3) building building building If the height of the building is not known, it shall be estimated based on the number of floors NF , building assuming an average height per floor of 3 m: H = NF × 3 m (2.8.4) building building If the number of floors is also not known, a default value for the number of floors representative of the district or the borough shall be used. The total volume of residential buildings in the entity considered V is calculated as the sum of the volumes of total all residential buildings in the entity: Xn V ¼ V (2.8.5) total buildingi i¼1 CASE 2: no data on the number of inhabitants is available In this case the number of inhabitants is estimated based on the average dwelling floor space per inhabitant FSI. If this parameter is not known, a national default value shall be used. 2A: The dwelling floor space is known on the basis of dwelling units. In this case the number of inhabitants of each dwelling unit is estimated as follows: DUFS Inh ¼ i (2.8.6) dwellinguniti FSI The number of inhabitants of the building can now be estimated as in CASE 1A above. 2B: The dwelling floor space is known for the entire building, i.e. the sum of the dwelling floor spaces of all dwelling units in the building is known. In this case the number of inhabitants is estimated as follows: DFS Inh ¼ building (2.8.7) building FSI 2C: The dwelling floor space is known only for entities larger than a building, e.g. sides of city blocks, city blocks, districts or even an entire municipality. In this case the number of inhabitants of a building is estimated based on the volume of the building as described in CASE 1B above with the total number of inhabitants estimated as follows: DFS Inh ¼ total (2.8.8) total FSI 2D: The dwelling floor space is unknown. In this case the number of inhabitants of a building is estimated as described in CASE 2B above with the dwelling floor space estimated as follows: DFS = BA × 0,8 × NF (2.8.9) building building buildingL 168/94 EN Official Journal of the European Union 1.7.2015 The factor 0,8 is the conversion factor gross floor area ! dwelling floor space. If a different factor is known to be representative of the area it shall be used instead and clearly documented. If the number of floors of the building is not known, it shall be estimated based on the height of the building, H , typically resulting in a non-integer number of floors: building H NF ¼ building (2.8.10) building 3 m If neither the height of the building nor the number of floors is known, a default value for the number of floors representative of the district or the borough shall be used. Assigning receiver points to the façades of buildings The assessment of population exposure to noise is based on receiver point levels at 4 m above the terrain level in front of building façades of residential buildings. For the calculation of the number of inhabitants, either the following case 1 procedure or the case 2 procedure shall be used for land based noise sources. For aircraft noise calculated according to 2.6, all population of a building is associated to the nearest noise calculation point on the grid. CASE 1 Figure a Example of location of receivers around a building following CASE 1 procedure (a) Segments of a length of more than 5 m are split up into regular intervals of the longest possible length, but less than or equal to 5 m. Receiver points are placed in the middle of each regular interval. (b) Remaining segments above a length of 2,5 m are represented by one receiver point in the middle of each segment.1.7.2015 EN Official Journal of the European Union L 168/95 (c) Remaining adjacent segments with a total length of more than 5 m are treated as polyline objects in a manner similar to that described in (a) and (b). (d) The number of inhabitants allocated to a receiver point, shall be weighted by the length of the represented façade so that the sum over all receiver points represents the total number of inhabitants. (e) Only for buildings with floor sizes that indicate a single dwelling per floor level, the most exposed façade noise level is directly used for the statistics and related to the number of inhabitants. CASE 2 Figure b Example of location of receivers around a building following CASE 2 procedure (a) Façades are considered separately or are split up every 5 m from the start position onwards, with a receiver position placed at the half-way distance of the façade or the 5 m segment (b) The remaining section has its receiver point in its mid-point. (c) The number of inhabitants allocated to a receiver point, shall be weighted by the length of the represented façade so that the sum over all receiver points represents the total number of inhabitants. (d) Only for buildings with floor sizes that indicate a single dwelling per floor level, the most exposed façade noise level is directly used for the statistics and related to the number of inhabitants. 3. INPUT DATA Input data to be used as appropriate in association with the methods described above are given in Appendix F to Appendix I. In cases where input data provided in Appendix F to Appendix I are not applicable or cause deviations from the true value that do not meet the conditions presented under 2.1.2 and 2.6.2, other values can be used, provided that the values used and the methodology used to derive them are sufficiently documented, including demonstrating their suitability. This information shall be made publicly available. 4. MEASUREMENT METHODS In cases when, for any reason, measurements are performed, these shall be in accordance with the principles governing long term average measurements stated in ISO 1996-1:2003 and ISO 1996-2:2007 or, for aircraft noise, ISO 20906:2009.L 168/96 EN Official Journal of the European Union 1.7.2015 Appendix A Data requirements Section 2.7.6 of the main text describes in general terms the requirements for case-specific data describing an airport and its operations that are needed for noise contour calculations. The following datasheets are filled with example data for a hypothetical airport. Specific data formats will generally depend on the requirements and needs for the particular noise modelling system as well as the study scenario. Note: It is recommended that geographic information (reference points etc.) be specified in Cartesian coordinates. The choice of the particular coordinate system usually depends on the maps available. A1 GENERAL AIRPORT DATA A2 RUNWAY DESCRIPTION For displaced thresholds, runway description may be repeated or displaced thresholds can be described in the ground track description section.1.7.2015 EN Official Journal of the European Union L 168/97 A3 GROUND TRACK DESCRIPTION In the absence of radar data the following information is needed to describe particular ground tracks.L 168/98 EN Official Journal of the European Union 1.7.2015 A4 AIR TRAFFIC DESCRIPTION1.7.2015 EN Official Journal of the European Union L 168/99 A5 FLIGHT PROCEDURE DATA SHEET Example aircraft for a Chapter 3 Boeing 727-200 as derived from radar using the guidance set out in Section 2.7.9 of the main text.L 168/100 EN Official Journal of the European Union 1.7.2015 Example for a procedural profile based on A/C-data stored in ANP database:1.7.2015 EN Official Journal of the European Union L 168/101 Appendix B Flight performance calculations Terms and symbols The terms and symbols used in this appendix are consistent with those conventionally used by aircraft performance engineers. Some basic terms are explained briefly below for the benefit of users not familiar with them. To minimise conflict with the main body of the method, symbols are mostly defined separately within this appendix. Quantities that are referenced in the main body of the method are assigned common symbols; a few that are used differently in this appendix are marked with an asterisk (*). There is some juxtaposition of US and SI units; again this is to preserve conventions that are familiar to users from different disciplines. Terms Break point See Flat Rating Calibrated airspeed (Otherwise termed equivalent or indicated airspeed.) The speed of the aircraft relative to the air as indicated by a calibrated instrument on the aircraft. The true airspeed, which is normally greater, can be calculated from the calibrated airspeed knowing the air density. Corrected net thrust Net thrust is the propulsive force exerted by an engine on the airframe. At a given power setting (EPR or N ) this falls with air density as altitude increases; corrected net 1 thrust is the thrust at sea level. Flat rating For specific maximum component temperatures, the engine thrust falls as the ambient air temperature rises — and vice-versa. This means that there is a critical air tempera­ ture above which the rated thrust cannot be achieved. For most modern engines this is called the 'flat rated temperature' because, at lower air temperatures the thrust is auto­ matically limited to the rated thrust to maximise service life. The thrust falls anyway at temperatures above the flat rated temperature — which is often called the break point or break temperature. Speed Magnitude of aircraft velocity vector (relative to aerodrome coordinate system) Rated thrust The service life of an aircraft engine is very dependent upon the operating tempera­ tures of its components. The greater the power or trust generated, the higher the tem­ peratures and the shorter the life. To balance performance and life requirements flat rated engines are assigned thrust ratings for take-off, climb and cruise which define normal maximum power settings. Thrust setting parameter The pilot cannot select a particular engine thrust; rather s/he chooses an appropriate setting of this parameter which is displayed in the cockpit. It is usually either the en­ gine pressure ratio (EPR) or low- pressure rotor (or fan) rotational speed (N ). 1 Symbols Quantities are dimensionless unless otherwise stated. Symbols and abbreviations not listed below are used only locally and defined in the text. Subscripts 1 and 2 denote conditions at the start and end of a segment respectively. Overbars denote segment mean values, i.e. average of start and end values. a Average acceleration, ft/s2 a Maximum acceleration available, ft/s2 max A, B, C, D Flap coefficients E, F, G , H Engine thrust coefficients A,B F Net thrust per engine, lbf nL 168/102 EN Official Journal of the European Union 1.7.2015 F/δ Corrected net thrust per engine, lbf n G Climb gradient G′ Engine-out climb gradient G Mean runway gradient, positive uphill R g Gravitational acceleration, ft/s2 ISA International Standard Atmosphere N * No of engines supplying thrust R Drag-to-lift ratio C /C D L ROC Segment rate of climb (ft/min) s Ground distance covered along ground track, ft s Take-off distance into an 8 kt headwind, ft TO8 s Take-off distance corrected for w and G , ft TOG R s Take-off distance into headwind w, ft TOw T Air temperature, °C T Breakpoint temperature, °C B V Groundspeed, kt V Calibrated airpeed, kt C V True airspeed, kt T W Aeroplane weight, lb w Headwind speed, kt Δs Still air segment length projected onto ground track, ft Δs Segment length ground projection corrected for headwind, ft w δ p/p, the ratio of the ambient air pressure at the aeroplane to the standard air pressure at mean sea level: o p = 101,325 kPa (or 1 013,25 mb) o ε Bank angle, radians γ Climb/descent angle, radians θ (T + 273,15)/(T + 273,15) the ratio of the air temperature at altitude to the standard air temperature at 0 mean sea level: T = 15,0 °C 0 σ * ρ/ρ = Ratio of air density at altitude to mean sea level value (also, σ = δ/θ) 0 B1 INTRODUCTION Flight path synthesis In the main, this appendix recommends procedures for calculating an aeroplane flight profile, based on specified aerodynamic and powerplant parameters, aircraft weight, atmospheric conditions, ground track and operating procedure (flight configuration, power setting, forward speed, vertical speed, etc.). The operating procedure is described by a set of procedural steps that prescribe how to fly the profile.1.7.2015 EN Official Journal of the European Union L 168/103 The flight profile, for takeoff or approach, is represented by a series of straight-line segments, the ends of which are termed profile points. It is calculated using aerodynamic and thrust equations containing numerous coefficients and constants which must be available for the specific combination of airframe and engine. This calculation process is described in the text as the process of flight path synthesis. Apart from the aircraft performance parameters, which can be obtained from the ANP database, these equations require specification of (1) aeroplane gross weight, (2) the number of engines, (3) air temperature, (4) runway elevation, and (5) the procedural steps (expressed in terms of power settings, flap deflections, airspeed and, during acceleration, average rate-of-climb/descent) for each segment during takeoff and approach. Each segment is then classified as a ground roll, take-off or landing, constant speed climb, power cutback, accelerating climb with or without flap retraction, descent with or without deceleration and/or flap deployment, or final landing approach. The flight profile is built up step by step, the starting parameters for each segment being equal to those at the end of the preceding segment. The aerodynamic-performance parameters in the ANP database are intended to yield a reasonably accurate representation of an aeroplane's actual flight path for the specified reference conditions (see Section 2.7.6 of the main text). But the aerodynamic parameters and engine coefficients have been shown to be adequate for air temperatures up to 43 °C, aerodrome altitudes up to 4 000 ft and across the range of weights specified in the ANP database. The equations thus permit the calculation of flight paths for other conditions; i.e. non-reference aeroplane weight, wind speed, air temperature, and runway elevation (air pressure), normally with sufficient accuracy for computing contours of average sound levels around an airport. Section B-4 explains how the effects of turning flight are taken into account for departures. This allows bank angle to be accounted for when calculating the effects of lateral directivity (installation effects). Also, during turning flight, climb gradients will generally be reduced depending in the radius of the turn and the speed of the aeroplane. (The effects of turns during the landing approach are more complex and are not covered at present. However these will rarely influence noise contours significantly.) Sections B-5 to B-9 describe the recommended methodology for generating departure flight profiles, based on ANP database coefficients and procedural steps. Sections B-10 and B-11 describe the methodology used to generate approach flight profiles, based on ANP database coefficients and flight procedures. Section B-12 provides worked examples of the calculations. Separate sets of equations are provided to determine the net thrust produced by jet engines and propellers respectively. Unless noted otherwise, the equations for aerodynamic performance of an aeroplane apply equally to jet and propeller- powered aeroplanes. Mathematical symbols used are defined at the beginning of this appendix and/or where they are first introduced. In all equations the units of coefficients and constants must of course be consistent with the units of the corresponding parameters and variables. For consistency with the ANP database, the conventions of aircraft performance engineering are followed in this appendix; distances and heights in feet (ft), speed in knots (kt), mass in pounds (lb), force in pounds- force (high-temperature corrected net thrust), and so on — even though some dimensions (e.g. atmospheric ones) are expressed in SI units. Modellers using other unit systems should be very careful to apply appropriate conversion factors when adopting the equations to their needs. Flight path analysis In some modelling applications the flight path information is provided not as procedural steps but as coordinates in position and time, usually determined by analysis of radar data. This is discussed in Section 2.7.7 of the main text. In this case the equations presented in this Appendix are used ‘in reverse’; the engine thrust parameters are derived from the aircraft motion rather than vice-versa. In general, once the flight path data has been averaged and reduced to segment form, each segment being classified by climb or descent, acceleration or deceleration, and thrust and flap changes, this is relatively straightforward by comparison with synthesis which often involves iterative processes.L 168/104 EN Official Journal of the European Union 1.7.2015 B2 ENGINE THRUST The propulsive force produced by each engine is one of five quantities that need to be defined at the ends of each flight path segment (the others being height, speed, power setting and bank angle). Net thrust represents the component of engine gross thrust that is available for propulsion. For aerodynamic and acoustical calculations, the net thrust is referred to standard air pressure at mean sea level. This is known as corrected net thrust, F/δ. n This will be either the net thrust available when operating at a specified thrust rating, or the net thrust that results when the thrust-setting parameter is set to a particular value. For a turbojet or turbofan engine operating at a specific thrust rating, corrected net thrust is given by the equation F/δ = E + F · V + G · h + G · h2 + H · T (B-1) n c A B where F is the net thrust per engine, lbf n δ is the ratio of the ambient air pressure at the aeroplane to the standard air pressure at mean sea level, i.e., to 101,325 kPa (or 1 013,25 mb) [ref. 1] F/δ is the corrected net thrust per engine, lbf n V is the calibrated airspeed, kt C T is the ambient air temperature in which the aeroplane is operating, °C, and E, F, G , G , H are engine thrust constants or coefficients for temperatures below the engine flat rating temperature A B at the thrust rating in use (on the current segment of the takeoff/climbout or approach flight path), lb.s/ft, lb/ft, lb/ft2, lb/°C. Obtainable from the ANP database. Data are also provided in the ANP database to allow calculation of non-rated thrust as a function of a thrust setting parameter. This is defined by some manufacturers as engine pressure ratio EPR, and by others as low-pressure rotor speed, or fan speed, N . When that parameter is EPR, equation B-1 is replaced by 1 F/δ = E + F · V + G · h + G · h2 + H · T + K · EPR + K · EPR2 (B-2) n C A B 1 2 where K and K are coefficients, from the ANP database that relate corrected net thrust and engine pressure ratio in the 1 2 vicinity of the engine pressure ratio of interest for the specified aeroplane Mach number. When engine rotational speed N is the parameter used by the cockpit crew to set thrust, the generalised thrust equation 1 becomes � � � � 2 N N F =δ¼E þF �V þG �h þG �h2þH �T þK � pffi1ffiffi þK � pffi1ffiffi (B-3) n C A B 3 4 θ θ where N is the rotational speed of the engine's low-pressure compressor (or fan) and turbine stages, % 1 θ = (T + 273)/288,15, the ratio of the absolute total temperature at the engine inlet to the absolute standard air temperature at mean sea level [ref. 1]. N pffi1ffiffi is the corrected low pressure rotor speed, %; and θ K , K are constants derived from installed engine data encompassing the N speeds of interest. 3 4 11.7.2015 EN Official Journal of the European Union L 168/105 Note that for a particular aeroplane E, F, G , G and H in equations B-2 and B-3 might have different values from those A B in equation B-1. Not every term in the equation will always be significant. For example, for flat-rated engines operating in air temperatures below the break point (typically 30 °C), the temperature term may not be required. For engines not flat rated, ambient temperature must be considered when designating rated thrust. Above the engine flat rating temperature, a different set of engine thrust coefficients (E, F, G , G and H) must be used to determine the thrust level available. A B high Normal practice would then be to compute F/δ using both the low temperature and high temperature coefficients and n to use the higher thrust level for temperatures below the flat rating temperature and use the lower calculated thrust level for temperature above the flat rating temperature. Where only low temperature thrust coefficients are available, the following relationship may be used: (F/δ) = F · V + (E + H · T )·(1 – 0,006 · T)/(1 – 0,006 · T ) (B-4) n high C B B where (F/δ) high-temperature corrected net thrust (lbf), n high T breakpoint temperature (in the absence of a definitive value assume a default value of 30 °C). B The ANP database provides values for the constants and coefficients in equations B-1 to B-4. For propeller driven aeroplanes, corrected net thrust per engine should be read from graphs or calculated using the equation F/δ = (326 · η · P/V )/δ (B-5) n p T where η is the propeller efficiency for a particular propeller installation and is a function of propeller rotational speed and aeroplane flight speed V is the true airspeed, kt T P is net propulsive power for the given flight condition, e.g. max takeoff or max climb power, hp p Parameters in equation B-5 are provided in the ANP database for maximum takeoff thrust and maximum climb thrust settings. True airspeed V is estimated from the calibrated airspeed V using the relationship T C pffiffiffi V ¼V = σ (B-6) T C where σ is the ratio of the air density at the aeroplane to the mean sea-level value. Guidance on operation with reduced takeoff thrust Often, aircraft takeoff weights are below maximum allowable and/or the available runway field length exceeds the minimum required with the use of maximum takeoff thrust. In these cases, it is common practice to reduce engine thrust below maximum levels in order to prolong engine life and, sometimes, for noise abatement purposes. Engine thrust can only be reduced to levels that maintain a required margin of safety. The calculation procedure used by airline operators to determine the amount of thrust reduction is regulated accordingly: it is complex and takes into account numerous factors including takeoff weight, ambient air temperature, declared runway distances, runway elevation and runway obstacle clearance criteria. Therefore the amount of thrust reduction varies from flight to flight.L 168/106 EN Official Journal of the European Union 1.7.2015 As they can have a profound effect upon departure noise contours, modellers should take reasonable account of reduced thrust operations and, to make best possible provision, to seek practical advice from operators. If such advice is not available it is still advisable to make some allowance by alternative means. It is impractical to mirror the operators' calculations for noise modelling purposes; nor would they be appropriate alongside the conventional simplifications and approximations which are made for the purposes of calculating long term average noise levels. As a practicable alternative the following guidance is provided. It should be emphasised that considerable research is ongoing in this area and thus, this guidance is subject to change. Analysis of FDR data has shown that the level of thrust reduction is strongly correlated with ratio of the actual takeoff weight to the Regulated Takeoff Weight (RTOW), down to a fixed lower limit (1); i.e. F/δ = (F/δ) · W/W (B-7) n n max RTOW where (F/δ) is the maximum rated thrust, W is the actual gross take-off weight and W is the Regulated Takeoff n max RTOW Weight. The RTOW is the maximum takeoff weight that can be safely used, whilst satisfying takeoff field length, engine-out and obstacle requirements. It is a function of the available runway length, airfield elevation, temperature, headwind, and flap angle. This information can be obtained from operators and should be more readily available than data on actual levels of reduced thrust. Alternatively, it may be computed using data contained in aircraft flight manuals. Reduced Climb Thrust When employing reduced take-off thrust, operators often, but not always, reduce climb thrust from below maximum levels (2). This prevents situations occurring where, at the end of the initial climb at take-off thrust, power has to be increased rather than cut back. However, it is more difficult to establish a rationale for a common basis here. Some operators use fixed detents below maximum climb thrust, sometimes referred to as Climb 1 and Climb 2, typically reducing climb thrust by 10 and 20 percent respectively relative to maximum. It is recommended that whenever reduced takeoff thrust is used, climb thrust levels also be reduced by 10 percent. B3 VERTICAL PROFILES OF AIR TEMPERATURE, PRESSURE, DENSITY AND WINDSPEED For the purposes of this document, the variations of temperature, pressure and density with height above mean sea level are taken to be those of the International Standard Atmosphere. The methodologies described below have been validated for aerodrome altitudes up to 4 000 ft above sea level and for air temperatures up to 43 °C (109 °F). Although, in reality, mean wind velocity varies with both height and time, it is not usually practicable to take account of this for noise contour modelling purposes. Instead, the flight performance equations given below are based on the common assumption that the aeroplane is heading directly into a (default) headwind of 8 kt at all times — regardless of compass bearing (although no explicit account of mean wind velocity is taken in sound propagation calculations). Methods for adjusting the results for other headwind speeds are provided. B4 THE EFFECTS OF TURNS The remainder of this appendix explains how to calculate the required properties of the segments joining the profile points s,z that define the two-dimensional flight path in the vertical plane above the ground track. Segments are defined in sequence in the direction of motion. At the end of any one segment (or at the start of roll in the case of the first for a departure) where the operational parameters and the next procedural step are defined, the need is to calculate the climb angle and track distance to the point where the required height and/or speed are reached. (1) Airworthiness authorities normally stipulate a lower thrust limit, often 25 percent below maximum. (2) To which thrust is reduced after the initial climb at take-off power.1.7.2015 EN Official Journal of the European Union L 168/107 If the track is straight, this will be covered by a single profile segment, the geometry of which can then be determined directly (albeit sometimes with a degree of iteration). But if a turn starts or ends, or changes in radius or direction, before the required end-conditions are reached, a single segment would be insufficient because the aircraft lift and drag change with bank angle. To account for the effects of the turn on the climb, additional profile segments are required to implement the procedural step — as follows. The construction of the ground track is described in Section 2.7.13 of the text. This is done independently of any aircraft flight profile (although with care not to define turns that could not be flown under normal operating constraints). But as the flight profile — height and speed as a function of track distance — is affected by turns so that the flight profile cannot be determined independently of the ground track. To maintain speed in a turn the aerodynamic wing lift has to be increased, to balance centrifugal force as well as the aircraft weight. This in turn increases drag and, consequently the propulsive thrust required. The effects of the turn are expressed in the performance equations as functions of bank angle ε which, for an aircraft in level flight turning at constant speed on a circular path, is given by � � 2,85�V2 ε¼tan − 1 (B-8) r �g where V is the groundspeed, kt r is the turn radius, ft and g is the acceleration due to gravity, ft/s2 All turns are assumed to have a constant radius and second-order effects associated with non-level flight paths are disregarded; bank angles are based on the turn radius r of the ground track only. To implement a procedural step a provisional profile segment is first calculated using the bank angle ε at the start point — as defined by equation B-8 for the track segment radius r. If the calculated length of the provisional segment is such that it does not cross the start or end of a turn, the provisional segment is confirmed and attention turns to the next step. But if the provisional segment crosses one or more starts or ends of turns (where ε changes) (1), the flight parameters at the first such point are estimated by interpolation (see Section 2.7.13), saved along with its coordinates as end-point values, and the segment truncated. The second part of the procedural step is then applied from that point — once more assuming provisionally that it can be completed in a single segment with the same end conditions but with the new start point and new bank angle. If this second segment then passes another change of turn radius/direction, a third segment will be required — and so on until the end-conditions are achieved. Approximate method It will be apparent that accounting fully for the effects of turns, as described above, involves considerable computational complexity because the climb profile of any aircraft has to be calculated separately for each ground track that it follows. But changes to the vertical profile caused by turns usually have a markedly smaller influence on the contours than the changes of bank angle, and some users may prefer to avoid the complexity — at the cost of some loss of precision — by disregarding the effects of turns on profiles while still accounting for the bank angle in the calculation of lateral sound emission (see Section 2.7.19). Under this approximation profile points for a particular aircraft operation are calculated once only, assuming a straight ground track (for which ε = 0). (1) To avoid contour discontinuities caused by instantaneous changes of bank angle at the junctions between straight and turning flight, sub-segments are introduced into the noise calculations to allow linear transitions of bank angle over the first and last 5° of the turn. These are not necessary in the performance calculations; the bank angle is always given by equation B-8.L 168/108 EN Official Journal of the European Union 1.7.2015 B5 TAKEOFF GROUND ROLL Take-off thrust accelerates the aeroplane along the runway until lift-off. Calibrated airspeed is then assumed to be constant throughout the initial part of the climbout. Landing gear, if retractable, is assumed to be retracted shortly after lift-off. For the purpose of this document, the actual takeoff ground-roll is approximated by an equivalent take-off distance (into a default headwind of 8 kt), s , defined as shown in Figure B-1, as the distance along the runway from brake release to TO8 the point where a straight line extension of the initial landing-gear-retracted climb flight path intersects the runway. Figure B-1 Equivalent takeoff distance On a level runway, the equivalent takeoff ground-roll distance s in feet is determined from TO8 B �θ �ðW=δÞ2 S ¼ 8 (B-9) TO8 N �ðF =δÞ n where B is a coefficient appropriate to a specific aeroplane/flap-deflection combination for the ISA reference conditions, 8 including the 8-knot headwind, ft/lbf W is the aeroplane gross weight at brake release, lbf N is the number of engines supplying thrust. Note: Since equation B-9 accounts for variation of thrust with airspeed and runway elevation, for a given aeroplane the coefficient B depends only on flap deflection. 8 For headwind other than the default 8 kt, the takeoff ground-roll distance is corrected by using: ðV − wÞ2 S ¼S � C (B-10) TOw TO8 ðV − 8Þ2 C where S is the ground-roll distance corrected for headwind w, ft TOw V (in this equation) is the calibrated speed at takeoff rotation, kt C w is the headwind, kt1.7.2015 EN Official Journal of the European Union L 168/109 The takeoff ground-roll distance is also corrected for runway gradient as follows: α S TOG ¼S TOw� ðα − g �G Þ (B-11) R where S is the ground-roll distance (ft) corrected for headwind and runway gradient, TOG pffiffiffi a is the average acceleration along the runway, equal to ðV � σÞ2=ð2�s Þ, ft/s2 C TOw G is the runway gradient; positive when taking-off uphill R B6 CLIMB AT CONSTANT SPEED This type of segment is defined by the aeroplane's calibrated airspeed, flap setting, and the height and bank angle at its end, together with the headwind speed (default 8 kt). As for any segment, the segment start parameters including corrected net thrust are put equal to those at the end of the preceding segment — there are no discontinuities (except of flap angle and bank angle which, in these calculations, are allowed to change in steps). The net thrusts at the segment end are first calculated using the appropriate equation from B-1 to B-5. The average geometric climb angle g (see Figure B-1) is then given by (B-12) where the over-bars denote mid-segment values (= average of start-point and end-point values — generally the mid-segment values) and K is a speed-dependent constant equal to 1,01 when V ≤ 200 kt or 0,95 otherwise. This constant accounts for the C effects on climb gradient of climbing into an 8-knot headwind and the acceleration inherent in climbing at constant calibrated airspeed (true speed increases as air density diminishes with height). R is the ratio of the aeroplane's drag coefficient to its lift coefficient appropriate to the given flap setting. The landing gear is assumed to be retracted. ε Bank angle, radians The climb angle is corrected for headwind w using: ðV − 8Þ γ ¼γ � C (B-13) w ðV − wÞ C where γ is the average climb angle corrected for headwind. w The distance that the aeroplane traverses along the ground track, Δs, while climbing at angle γ, from an initial altitude w h to a final altitude h is given by 1 2 ðh − h Þ Δ ¼ 2 1 (B-14) S tan γ wL 168/110 EN Official Journal of the European Union 1.7.2015 As a rule, two distinct phases of a departure profile involve climb at constant airspeed. The first, sometime referred to as the initial climb segment is immediately after lift-off, where safety requirements dictate that the aeroplane is flown at a minimum airspeed of least the takeoff safety speed. This is a regulated speed and should be achieved by 35 ft above the runway during normal operation. However, it is common practice to maintain an initial climb speed slightly beyond the takeoff safety speed, usually by 10-20 kt, as this tends to improve the initial climb gradient achieved. The second is after flap retraction and initial acceleration, referred to as continuing climb. During the initial climb, the airspeed is dependent on the takeoff flap setting and the aeroplane gross weight. The calibrated initial climb speed V is calculated using the first order approximation: CTO pffiffiffiffiffi V ¼C � W (B-15) CTO where C is a coefficient appropriate to the flap setting (kt/√lbf), read from the ANP database. For continuing climb after acceleration, the calibrated airspeed is a user input parameter. B7 POWER CUTBACK (TRANSITION SEGMENT) Power is reduced, or cut back, from take-off setting at some point after takeoff in order to extend engine life and often to reduce noise in certain areas. Thrust is normally cut back during either a constant speed climb segment (Section B6) or an acceleration segment (Section B8). As it is a relatively brief process, typically of only 3-5 seconds′ duration, is it modelled by adding a ‘transition segment’ to the primary segment. This is usually taken to cover a horizontal ground distance of 1 000 ft (305 m). Amount of thrust reduction In normal operation the engine thrust is reduced to the maximum climb thrust setting. Unlike the take-off thrust, climb thrust can be sustained indefinitely, usually in practice until the aeroplane has reached its initial cruise altitude. The maximum climb thrust level is determined with equation B-1 using the manufacturer supplied maximum thrust coefficients. However, noise abatement requirements may call for additional thrust reduction, sometimes referred to as a deep cutback. For safety purposes the maximum thrust reduction is limited (1) to an amount determined by the performance of the aeroplane and the number of engines. The minimum ‘reduced-thrust’ level is sometimes referred to as the engine-out ‘reduced thrust’: � � ðF =δÞ ¼ðW =δ 2Þ � sinðarctanð0,01�G′ÞÞ þ R (B-16) n engine:out ðN − 1Þ K cos ε where δ is the pressure ratio at altitude h 2 2 G′ is the engine-out percentage climb gradient: = 0 % for aeroplanes with automatic thrust restoration systems; otherwise, = 1,2 % for 2-engine aeroplane = 1,5 % for 3-engine aeroplane = 1,7 % for 4-engine aeroplane (1) ‘Noise Abatement Procedures’, ICAO Document 8168 ‘PANS-OPS’ Vol.1 Part V, Chapter 3, ICAO 2004.1.7.2015 EN Official Journal of the European Union L 168/111 Constant speed climb segment with cutback The climb segment gradient is calculated using equation B-12, with thrust calculated using either B-1 with maximum climb coefficients, or B-16 for reduced thrust. The climb segment is then broken into two sub-segments, both having the same climb angle. This is illustrated in Figure B-2. Figure B-2 Constant speed climb segment with cutback (illustration — not to scale) The first sub-segment is assigned a 1 000 ft (304 m) ground distance, and the corrected net thrust per engine at the end of 1 000 ft is set equal to the cutback value. (If the original horizontal distance is less than 2 000 ft, one half of the segment is used to cutback thrust.) The final thrust on the second sub-segment is also set equal to the cutback thrust. Thus, the second sub-segment is flown at constant thrust. B8 ACCELERATING CLIMB AND FLAP RETRACTION This usually follows the initial climb. As for all flight segments, the start-point altitude h , true airspeed V , and thrust 1 T1 (F/δ) are those from the end of the preceding segment. The end-point calibrated airspeed V and the average climb rate n 1 C2 ROC are user inputs (bank angle ε is a function of speed and radius of turn). As they are interdependent, the end altitude h , end true airspeed V , end thrust (F/δ) and segment track length Δs have to be calculated by iteration; the end 2 T2 n 2 altitude h is guessed initially and then recalculated repeatedly using equations B-16 and B-17 until the difference 2 between successive estimates is less than a specified tolerance, e.g. one foot. A practical initial estimate is h = h + 250 feet. 2 1 The segment track length (horizontal distance covered) is estimated as: S ¼0,95�k2�ðV2 − V2 Þ=2 ðα − G �gÞ (B-17) seg T2 T1 max where 0,95 is a factor to account for effect of 8 kt headwind when climbing at 160 kt k is a constant to convert knots to ft/sec = 1,688 ft/s per ktL 168/112 EN Official Journal of the European Union 1.7.2015 pffiffiffiffiffi V = true airspeed at segment end, kt: V ¼V = σ T2 T2 C2 2 where σ = air density ratio at end altitude h 2 2 α = maximum acceleration in level flight (ft/s2) max = G = climb gradient where ROC = climb rate, ft/min Using this estimate of Δs, the end altitude h ′ is then re-estimated using: 2 h ′ = h + s · G/0,95 (B-18) 2 1 As long as the error jh′ − h j is outside the specified tolerance, the steps B-17 and B-18 are repeated using the current 2 2 iteration segment-end values of altitude h , true airspeed V , corrected net thrust per engine (F/δ) . When the error is 2 T2 n 2 within the tolerance, the iterative cycle is terminated and the acceleration segment is defined by the final segment-end values. Note: If during the iteration process (a – G·g) < 0,02 g, the acceleration may be too small to achieve the desired V max C2 in a reasonable distance. In this case, the climb gradient can be limited to G = a /g – 0,02, in effect reducing max the desired climb rate in order to maintain acceptable acceleration. If G < 0,01 it should be concluded there is not enough thrust to achieve the acceleration and climb rate specified; the calculation should be terminated and the procedure steps revised (1). The acceleration segment length is corrected for headwind w by using: ðV − wÞ ΔS ¼Δ � T (B-19) w S ðV − 8Þ T Accelerating segment with cutback Thrust cutback is inserted into an acceleration segments in the same way as for a constant speed segment; by turning its first part into a transition segment. The cutback thrust level is calculated as for the constant-speed cutback thrust procedure, using equation B-1 only. Note it is not generally possible to accelerate and climb whilst maintaining the minimum engine-out thrust setting. The thrust transition is assigned a 1 000 ft (305 m) ground distance, and the corrected net thrust per engine at the end of 1 000 ft is set equal to the cutback value. The speed at the end of the segment is determined by iteration for a segment length of 1 000 ft. (If the original horizontal distance is less than 2 000 ft, one half of the segment is used for thrust change.) The final thrust on the second sub-segment is also set equal to the cutback thrust. Thus, the second sub-segment is flown at constant thrust. B9 ADDITIONAL CLIMB AND ACCELERATION SEGMENTS AFTER FLAP RETRACTION If additional acceleration segments are included in the climbout flight path, equations B-12 to B-19 should be used again to calculate the ground-track distance, average climb angle, and height gain for each. As before, the final segment height must be estimated by iteration. B10 DESCENT AND DECELERATION Approach flight normally requires the aeroplane to descend and decelerate in preparation for the final approach segment where the aeroplane is configured with approach flap and gear down. The flight mechanics are unchanged from the departure case; the main difference is that the height and speed profile is generally known, and it is the engine thrust levels that must be estimated for each segment. The basic force balance equation is: R�cos γþsin γþα=g F =δ¼W � (B-20) n N �δ (1) In either case the computer model should be programmed to inform the user of the inconsistency.1.7.2015 EN Official Journal of the European Union L 168/113 Equation B-20 may be used in two distinct ways. First the aeroplane speeds at the start and end of a segment may be defined, along with a descent angle (or level segment distance) and initial and final segment altitudes. In this case the deceleration may be calculated using: ðV =cos γÞ2 − ðV =cos γÞ2 α¼ 2 1 (B-21) ð2�Δ =cos γÞ S where Δs is the ground distance covered and V and V and are the initial and final groundspeeds calculated using 1 2 V �cos γ V¼ Cpffiffiffi − w (B-22) σ Equations B-20, B-21 and B-22 confirm that whilst decelerating over a specified distance at a constant rate of descent, a stronger headwind will result in more thrust being required to maintain the same deceleration, whilst a tailwind will require less thrust to maintain the same deceleration. In practice most, if not all decelerations during approach flight are performed at idle thrust. Thus for the second application of equation B-20, thrust is defined at an idle setting and the equation is solved iteratively to determine (1) the deceleration and (2) the height at the end of the deceleration segment — in a similar manner to the departure acceleration segments. In this case, deceleration distance can be very different with head and tail winds and it is sometimes necessary to reduce the descent angle in order to obtain reasonable results. For most aeroplanes, idle thrust is not zero and, for many, it is also a function of flight speed. Thus, equation B-20 is solved for the deceleration by inputting an idle thrust; the idle thrust is calculated using an equation of the form: (F/δ) = E + F · V + G · h + G · h2 + H · T (B-23) n idle idle idle C A,idle B,idle idle where (E , F , G , G and H ) are idle thrust engine coefficients available in the ANP database. idle idle A,idle B,idle idle B11 LANDING APPROACH The landing approach calibrated airspeed, V , is related to the landing gross weight by an equation of the same form as CA equation B-11, namely pffiffiffiffiffi V �D � W (B-24) CA where the coefficient D (kt/√lbf) corresponds to the landing flap setting. The corrected net thrust per engine during descent along the approach glideslope is calculated by solving equation B-12 for the landing weight W and a drag-to-lift ratio R appropriate for the flap setting with landing gear extended. The flap setting should be that typically used in actual operations. During landing approach, the glideslope descent angle γ may be assumed constant. For jet-powered and multi-engine propeller aeroplanes, γ is typically – 3°. For single-engine, propeller-powered aeroplanes, γ is typically – 5°. The average corrected net thrust is calculated by inverting equation B-12 using K = 1,03 to account for the deceleration inherent in flying a descending flight path into an 8-knot reference headwind at the constant calibrated airspeed given by equation B-24, i.e. (B-25)L 168/114 EN Official Journal of the European Union 1.7.2015 For headwinds other than 8 kt, average corrected net thrust becomes (B-26) The horizontal distance covered is calculated by: ðh − h Þ Δ ¼ 2 1 (B-27) S tan γ (positive since h > h and γ is negative). 1 21.7.2015 EN Official Journal of the European Union L 168/115 Appendix C Modelling of lateral ground track spreading It is recommended that, in the absence of radar data, lateral ground track dispersion be modelled on the assumption that the spread of tracks perpendicular to the backbone track follows a Gaussian normal distribution. Experience has shown that this assumption is a reasonable one in most cases. Assuming a Gaussian distribution with a standard deviation S, illustrated in Figure C-1, about 98,8 percent of all movements fall within boundaries of ± 2,5·S (i.e. within a swathe of width of 5·S). Figure C-1 Subdivision of a ground track into 7 subtracks (The width of the swathe is 5 times the standard deviation of the ground track spreading) A Gaussian distribution can normally be modelled adequately using 7 discrete sub-tracks evenly spaced between the ± 2,5·S boundaries of the swathe as shown in Figure C-1. However, the adequacy of the approximation depends on the relationship of the sub-track track separation to the heights of the aircraft above. There may be situations (very tight or very dispersed tracks) where a different number of subtracks is more appropriate. Too few subtracks cause ‘fingers’ to appear in the contour. Tables C-1 and C-2 show the parameters for a subdivision into between 5 and 13 subtracks. Table C-1 shows the location of the particular subtracks, Table C-2 the corresponding percentage of movements on each subtrack.L 168/116 EN Official Journal of the European Union 1.7.2015 Table C-1 Location of 5, 7, 9, 11 or 13 subtracks (The overall width of the swathe (containing 98 % of all movements) is 5 times the standard deviation) Location of subtracks for subdivision into Subtrack number 5 subtracks 7 subtracks 9 subtracks 11 subtracks 13 subtracks 12/13 ± 2,31·S 10/11 ± 2,27·S ± 1,92·S 8/9 ± 2,22·S ± 1,82·S ± 1,54·S 6/7 ± 2,14·S ± 1,67·S ± 1,36·S ± 1,15·S 4/5 ± 2,00·S ± 1,43·S ± 1,11·S ± 0,91·S ± 0,77·S 2/3 ± 1,00·S ± 0,71·S ± 0,56·S ± 0,45·S ± 0,38·S 1 0 0 0 0 0 Table C-2 Percentage of movements on 5, 7, 9, 11 or 13 subtracks (The overall width of the swathe (containing 98 % of all movements) is 5 times the standard deviation) Percentage of movements on subtrack for subdivision into Subtrack number 5 subtracks 7 subtracks 9 subtracks 11 subtracks 13 subtracks 12/13 1,1 % 10/11 1,4 % 2,5 % 8/9 2,0 % 3,5 % 4,7 % 6/7 3,1 % 5,7 % 7,1 % 8,0 % 4/5 6,3 % 10,6 % 12,1 % 12,1 % 11,5 % 2/3 24,4 % 22,2 % 19,1 % 16,6 % 14,4 % 1 38,6 % 28,2 % 22,2 % 18,6 % 15,6 %1.7.2015 EN Official Journal of the European Union L 168/117 Appendix D Recalculation of NPD-data for non-reference conditions The noise level contributions from each segment of the flight path are derived from the NPD-data stored in the internat­ ional ANP database. However it must be noted that these data have been normalised using average atmospheric attenuation rates defined in SAE AIR-1845. Those rates are averages of values determined during aircraft noise certifi­ cation testing in Europe and the USA. The wide variation of atmospheric conditions (temperature and relative humidity) in those tests is shown in Figure D-1. Figure D-1 Meteorological conditions recorded during noise certification tests The curves overlaid on Figure D-1, calculated using an industry standard atmospheric attenuation model ARP 866A, illustrate that across the test conditions a substantial variation of high frequency (8 kHz) sound absorption would be expected (although the variation of overall absorption would be rather less).L 168/118 EN Official Journal of the European Union 1.7.2015 Because the attenuation rates, given in Table D-1, are arithmetic averages, the complete set cannot be associated with a single reference atmosphere (i.e. with specific values of temperature and relative humidity). They can only thought of as properties of a purely notional atmosphere — referred to as the ‘AIR-1845 atmosphere’. Table D-1 Average atmospheric attenuation rates used to normalise NPD data in the ANP database Centre frequency of 1/3-octave Centre frequency of 1/3-octave Attenuation rate [dB/100 m] Attenuation rate [dB/100 m] band [Hz] band [Hz] 50 0,033 800 0,459 63 0,033 1 000 0,590 80 0,033 1 250 0,754 100 0,066 1 600 0,983 125 0,066 2 000 1,311 160 0,098 2 500 1,705 200 0,131 3 150 2,295 250 0,131 4 000 3,115 315 0,197 5 000 3,607 400 0,230 6 300 5,246 500 0,295 8 000 7,213 630 0,361 10 000 9,836 The attenuation coefficients in Table D-1 may be assumed valid over reasonable ranges of temperature and humidity. However, to check whether adjustments may be necessary, ARP-866A should be used to calculate average atmospheric absorption coefficients for the average airport temperature T and relative humidity RH. Where, from a comparison of these with those in Table D-1, it is judged that adjustment is required the following methodology should be used. The ANP database provides the following NPD data for each power setting: — maximum sound level versus slant distance, L (d) max — time integrated level versus distance for the reference airspeed, L(d), and E — unweighted reference sound spectrum at a slant distance of 305 m (1 000 ft), L (d ) where n = frequency band n,ref ref (ranging from 1 to 24 for 1/3-octave bands with centre frequencies from 50 Hz to 10 kHz), all data being normalised to the AIR-1845 atmosphere.1.7.2015 EN Official Journal of the European Union L 168/119 Adjustment of the NPD curves to user-specified conditions T and RH is performed in three steps: 1. First the reference spectrum is corrected to remove the SAE AIR-1845 atmospheric attenuation α : n,ref L(d ) = L (d ) + α · d (D-1) n ref n,ref ref n,ref ref where L(d ) is the unattenuated spectrum at d = 305 m and α is the coefficient of atmospheric absorption for n ref ref n,ref the frequency band n taken from Table D-1 (but expressed in dB/m). 2. Next the corrected spectrum is adjusted to each of the 10 standard NPD distances d using attenuation rates for both i (i) the SAE AIR-1845 atmosphere and (ii) the user-specified atmosphere (based on SAE ARP-866A). (i) For the SAE AIR-1845 atmosphere: L (d) = L(d ) – 20,lg(d/d ) – α · d (D-2) n,ref i n ref i ref n,ref i (ii) For the user atmosphere: L (T,RH,d) = L(d ) – 20,lg(d/d ) – α (T,RH) · d (D-3) n,866A i n ref i ref n,866A i where α is the coefficient of atmospheric absorption for the frequency band n (expressed in dB/m) calculated n,866A using SAE ARP-866A with temperature T, and relative humidity RH. 3. At each NPD distance d the two spectra are A-weighted and decibel-summed to determine the resulting A-weighted i levels L and L — which are then subtracted arithmetically: A,866A A,ref X24 X24 ΔLðT,RH,d Þ¼L − L ¼10�lg 10 ðL n,866AðT,RH,d iÞ − A nÞ=10 − 10�lg 10 ðL n,refðd iÞ − A nÞ=10 (D-4) i A,866A A,ref n¼1 n¼1 The increment ΔL is the difference between the NPDs in the user-specified atmosphere and the reference atmosphere. This is added to the ANP database NPD data value to derive the adjusted NPD data. Applying ΔL to adjust both L and L NPDs effectively assumes that different atmospheric conditions affect the max E reference spectrum only and have no effect on the shape of the level-time-history This may be considered valid for typical propagation ranges and typical atmospheric conditions.L 168/120 EN Official Journal of the European Union 1.7.2015 Appendix E The finite segment correction This appendix outlines the derivation of the finite segment correction and the associated energy fraction algorithm described in Section 2.7.19. E1 GEOMETRY The energy fraction algorithm is based on the sound radiation of a ‘fourth-power’ 90-degree dipole sound source. This has directional characteristics which approximate those of jet aircraft sound, at least in the angular region that most influences sound event levels beneath and to the side of the aircraft flight path. Figure E-1 Geometry between flight path and observer location O Figure E-1 illustrates the geometry of sound propagation between the flight path and the observer location O. The aircraft at P is flying in still uniform air with a constant speed on a straight, level flight path. Its closest point of approach to the observer is P . The parameters are: p d distance from the observer to the aircraft d perpendicular distance from the observer to the flight path (slant distance) p q distance from P to P = – V · τ p V speed of the aircraft t time at which the aircraft is at point P t time at which the aircraft is located at the point of closest approach P p p τ flight time = time relative to time at P = t – t p p ψ angle between flight path and aircraft-observer vector It should be noted that, since the flight time τ relative to the point of closest approach is negative when the aircraft is before the observer position (as shown in Figure E-1), the relative distance q to the point of closest approach becomes positive in that case. If the aircraft is ahead of the observer, q becomes negative.1.7.2015 EN Official Journal of the European Union L 168/121 E2 ESTIMATION OF THE ENERGY FRACTION The basic concept of the energy fraction is to express the noise exposure E produced at the observer position from a flight path segment P P (with a start-point P and an end-point P ) by multiplying the exposure E from the whole 1 2 1 2 ∞ infinite path flyby by a simple factor — the energy fraction factor F: E = F · E (E-1) ∞ Since the exposure can be expressed in terms of the time-integral of the mean-square (weighted) sound pressure level, i.e. Z E¼const � p2ðτÞdτ (E-2) to calculate E, the mean-square pressure has to be expressed as a function of the known geometric and operational parameters. For a 90° dipole source, d2 d4 p2 ¼p2� p �sin2ψ¼p2� p (E-3) p d2 p d4 where p2 and p2 are the observed mean-square sound pressures produced by the aircraft as it passes points P and P . p p This relatively simple relationship has been found to provide a good simulation of jet aircraft noise, even though the real mechanisms involved are extremely complex. The term d2/d2 in equation E-3 describes just the mechanism of spherical p spreading appropriate to a point source, an infinite sound speed and a uniform, non-dissipative atmosphere. All other physical effects — source directivity, finite sound speed, atmospheric absorption, Doppler-shift etc. — are implicitly covered by the sin2ψ term. This factor causes the mean square pressure to decrease inversely as d4; whence the expression ‘fourth power’ source. Introducing the substitutions ! ! 2 2 d2 ¼d2þq2 ¼d2þðV�τÞ2 and d ¼1þ V�τ p p d d p p the mean-square pressure can be expressed as a function of time (again disregarding sound propagation time): ! ! 2 − 2 p2 ¼p2� 1þ V �τ (E-4) p d p Putting this into equation (E-2) and performing the substitution V �τ α¼ (E-5) d p the sound exposure at the observer from the flypast between the time interval [τ ,τ ] can be expressed as 1 2 Zα2 E¼const �p2�d p� 1 dα (E-6) p V ð1þα2Þ2 α1 The solution of this integral is: � � E¼const �p2�d p�1 α 2 þarctan α − α 1 − arctan α (E-7) p V 2 1þα2 2 1þα2 1 2 1L 168/122 EN Official Journal of the European Union 1.7.2015 Integration over the interval [–∞,+∞] (i.e. over the whole infinite flight path) yields the following expression for the total exposure E : ∞ E ¼const �π �p2�d p (E-8) ∞ 2 p V and hence the energy fraction according to equation E-1 is � � 1 α α F¼ 2 þarctan α − 1 − arctan α (E-9) π 1þα2 2 1þα2 1 2 1 E3 CONSISTENCY OF MAXIMUM AND TIME INTEGRATED METRICS — THE SCALED DISTANCE A consequence of using the simple dipole model to define the energy fraction is that it implies a specific theoretical difference ΔL between the event noise levels L and L. If the contour model is to be internally consistent, this needs to max E equal the difference of the values determined from the NPD curves. A problem is that the NPD data are derived from actual aircraft noise measurements — which do not necessarily accord with the simple theory. The theory therefore needs an added element of flexibility. But in principal the variables α and α are determined by geometry and aircraft 1 2 speed — thus leaving no further degrees of freedom. A solution is provided by the concept of a scaled distance d as λ follows. The exposure level L as tabulated as a function of d in the ANP database for a reference speed V , can be expressed as E,∞ p ref 2 3 R∞ p2�dt 6 7 L E,∞ðV refÞ¼10�lg 6 4 − p∞ 2�t 7 5 (E-10) 0 ref where p is a standard reference pressure and t is a reference time (= 1 s for SEL). For the actual speed V it becomes 0 ref � � V L ðVÞ¼L ðV Þþ10�lg ref (E-11) E,∞ E,∞ ref V Similarly the maximum event level L can be written max " # p2 L ¼10�lg p (E-12) max p2 0 For the dipole source, using equations E-8, E-11 and E-12, noting that (from equations E-2 and E-8) Z∞ p2�dt¼π �p2�d p, the difference ΔL can be written: 2 p V − ∞ " � � # " # ΔL¼L − L ¼10�lg V � π p2d p � 1 − 10�lg p2 p (E-13) E,∞ max V 2 p V p2�t p2 ref 0 ref 0 This can only be equated to the value of ΔL determined from the NPD data if the slant distance d used to calculate the p energy fraction is substituted by a scaled distance d given by λ 2 d ¼ �V �t �10 ðLE,∞ − LmaxÞ=10 (E-14a) λ π ref ref or 2 d ¼d �10 ðLE,∞ − LmaxÞ=10 with d ¼ �V �t (E-14b) λ 0 0 π ref ref1.7.2015 EN Official Journal of the European Union L 168/123 Replacing d by d in equation E-5 and using the definition q = Vτ from Figure E-1 the parameters α and α in equation p λ 1 2 E-9 can be written (putting q = q at the start-point and q – λ = q at the endpoint of a flight path segment of length λ) 1 2 as − q − q þλ α ¼ 1 and α ¼ 1 (E-15) 1 d 2 d λ λ Having to replace the slant actual distance by scaled distance diminishes the simplicity of the fourth-power 90 degree dipole model. But as it is effectively calibrated in situ using data derived from measurements, the energy fraction algorithm can be regarded as semi-empirical rather than a pure theoretical.L 168/124 EN Official Journal of the European Union 1.7.2015 Appendix F Database for road traffic source This appendix presents the database for most of the existing road noise sources to be used to calculate road traffic noise following the method described in 2.2 Road traffic noise. Table F-1 Coefficients A and B for rolling noise and A and B for propulsion noise R,i,m R,i,m P,i,m P,i,m Coeffi­ Category 63 125 250 500 1 000 2 000 4 000 8 000 cient A 79,7 85,7 84,5 90,2 97,3 93,9 84,1 74,3 R B 30 41,5 38,9 25,7 32,5 37,2 39 40 R 1 A 94,5 89,2 88 85,9 84,2 86,9 83,3 76,1 P B – 1,3 7,2 7,7 8 8 8 8 8 P A 84 88,7 91,5 96,7 97,4 90,9 83,8 80,5 R B 30 35,8 32,6 23,8 30,1 36,2 38,3 40,1 R 2 A 101 96,5 98,8 96,8 98,6 95,2 88,8 82,7 P B – 1,9 4,7 6,4 6,5 6,5 6,5 6,5 6,5 P A 87 91,7 94,1 100,7 100,8 94,3 87,1 82,5 R B 30 33,5 31,3 25,4 31,8 37,1 38,6 40,6 R 3 A 104,4 100,6 101,7 101 100,1 95,9 91,3 85,3 P B 0 3 4,6 5 5 5 5 5 P A 0 0 0 0 0 0 0 0 R B 0 0 0 0 0 0 0 0 R 4a A 88 87,5 89,5 93,7 96,6 98,8 93,9 88,7 P B 4,2 7,4 9,8 11,6 15,7 18,9 20,3 20,6 P A 0 0 0 0 0 0 0 0 R B 0 0 0 0 0 0 0 0 R 4b A 95 97,2 92,7 92,9 94,7 93,2 90,1 86,5 P B 3,2 5,9 11,9 11,6 11,5 12,6 11,1 12 P A R B R 5 A P B P1.7.2015 EN Official Journal of the European Union L 168/125 Table F-2 Coefficients a and b for studded tyres i i Coeffi­ Category 63 125 250 500 1 000 2 000 4 000 8 000 cient a 0,0 0,0 0,0 2,6 2,9 1,5 2,3 9,2 i 1 b 0,0 0,0 0,0 – 3,1 – 6,4 – 14,0 – 22,4 – 11,4 i Table F-3 Coefficients C and C for acceleration and deceleration R,m,k P,m,k Category k Cr Cp 1 = crossing – 4,5 5,5 1 2 = roundabout – 4,4 3,1 1 = crossing – 4 9 2 2 = roundabout – 2,3 6,7 1 = crossing – 4 9 3 2 = roundabout – 2,3 6,7 1 = crossing 0 0 4a 2 = roundabout 0 0 1 = crossing 0 0 4b 2 = roundabout 0 0 1 = crossing 5 2 = roundabout Table F-4 Coefficients α and β for road surface i,m m Maxi­ Min mum speed at speed at Cat­ α α α α α α α α Description which it m m m m m m m m ßm which it egory (63 Hz) (125 Hz) (250 Hz) (500 Hz) (1 kHz) (2 kHz) (4 kHz) (8 kHz) is valid is valid [km/h] [km/h] 1 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 2 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 3 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 Reference road — — surface 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5L 168/126 EN Official Journal of the European Union 1.7.2015 Maxi­ Min mum speed at speed at Cat­ α α α α α α α α Description which it m m m m m m m m ßm which it egory (63 Hz) (125 Hz) (250 Hz) (500 Hz) (1 kHz) (2 kHz) (4 kHz) (8 kHz) is valid is valid [km/h] [km/h] 1 0,5 3,3 2,4 3,2 – 1,3 – 3,5 – 2,6 0,5 – 6,5 2 0,9 1,4 1,8 – 0,4 – 5,2 – 4,6 – 3,0 – 1,4 0,2 3 0,9 1,4 1,8 – 0,4 – 5,2 – 4,6 – 3,0 – 1,4 0,2 1-layer ZOAB 50 130 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5 1 0,4 2,4 0,2 – 3,1 – 4,2 – 6,3 – 4,8 – 2,0 – 3,0 2 0,4 0,2 – 0,7 – 5,4 – 6,3 – 6,3 – 4,7 – 3,7 4,7 3 0,4 0,2 – 0,7 – 5,4 – 6,3 – 6,3 – 4,7 – 3,7 4,7 2-layer ZOAB 50 130 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5 1 – 1,0 1,7 – 1,5 – 5,3 – 6,3 – 8,5 – 5,3 – 2,4 – 0,1 2 1,0 0,1 – 1,8 – 5,9 – 6,1 – 6,7 – 4,8 – 3,8 – 0,8 3 1,0 0,1 – 1,8 – 5,9 – 6,1 – 6,7 – 4,8 – 3,8 – 0,8 2-layer ZOAB 80 130 (fine) 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5 1 1,1 – 1,0 0,2 1,3 – 1,9 – 2,8 – 2,1 – 1,4 – 1,0 2 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 3 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 SMA-NL5 40 80 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5 1 0,3 0,0 0,0 – 0,1 – 0,7 – 1,3 – 0,8 – 0,8 – 1,0 2 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 3 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 SMA-NL8 40 80 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 51.7.2015 EN Official Journal of the European Union L 168/127 Maxi­ Min mum speed at speed at Cat­ α α α α α α α α Description which it m m m m m m m m ßm which it egory (63 Hz) (125 Hz) (250 Hz) (500 Hz) (1 kHz) (2 kHz) (4 kHz) (8 kHz) is valid is valid [km/h] [km/h] 1 1,1 – 0,4 1,3 2,2 2,5 0,8 – 0,2 – 0,1 1,4 2 0,0 1,1 0,4 – 0,3 – 0,2 – 0,7 – 1,1 – 1,0 4,4 3 0,0 1,1 0,4 – 0,3 – 0,2 – 0,7 – 1,1 – 1,0 4,4 Brushed down 70 120 concrete 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5 1 – 0,2 – 0,7 0,6 1,0 1,1 – 1,5 – 2,0 – 1,8 1,0 2 – 0,3 1,0 – 1,7 – 1,2 – 1,6 – 2,4 – 1,7 – 1,7 – 6,6 Optimised 3 – 0,3 1,0 – 1,7 – 1,2 – 1,6 – 2,4 – 1,7 – 1,7 – 6,6 brushed down 70 80 concrete 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5 1 1,1 – 0,5 2,7 2,1 1,6 2,7 1,3 – 0,4 7,7 2 0,0 3,3 2,4 1,9 2,0 1,2 0,1 0,0 3,7 3 0,0 3,3 2,4 1,9 2,0 1,2 0,1 0,0 3,7 Fine broomed 70 120 concrete 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5 1 1,1 1,0 2,6 4,0 4,0 0,1 – 1,0 – 0,8 – 0,2 2 0,0 2,0 1,8 1,0 – 0,7 – 2,1 – 1,9 – 1,7 1,7 3 0,0 2,0 1,8 1,0 – 0,7 – 2,1 – 1,9 – 1,7 1,7 Worked surface 50 130 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5 1 8,3 8,7 7,8 5,0 3,0 – 0,7 0,8 1,8 2,5 2 8,3 8,7 7,8 5,0 3,0 – 0,7 0,8 1,8 2,5 Hard elements 3 8,3 8,7 7,8 5,0 3,0 – 0,7 0,8 1,8 2,5 in herring- 30 60 bone 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5L 168/128 EN Official Journal of the European Union 1.7.2015 Maxi­ Min mum speed at speed at Cat­ α α α α α α α α Description which it m m m m m m m m ßm which it egory (63 Hz) (125 Hz) (250 Hz) (500 Hz) (1 kHz) (2 kHz) (4 kHz) (8 kHz) is valid is valid [km/h] [km/h] 1 12,3 11,9 9,7 7,1 7,1 2,8 4,7 4,5 2,9 2 12,3 11,9 9,7 7,1 7,1 2,8 4,7 4,5 2,9 Hard elements 3 12,3 11,9 9,7 7,1 7,1 2,8 4,7 4,5 2,9 not in herring- 30 60 bone 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5 1 7,8 6,3 5,2 2,8 – 1,9 – 6,0 – 3,0 – 0,1 – 1,7 2 0,2 0,7 0,7 1,1 1,8 1,2 1,1 0,2 0,0 3 0,2 0,7 0,7 1,1 1,8 1,2 1,1 0,2 0,0 Quiet hard 30 60 elements 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5 1 1,1 0,1 – 0,7 – 1,3 – 3,1 – 4,9 – 3,5 – 1,5 – 2,5 2 1,6 1,3 0,9 – 0,4 – 1,8 – 2,1 – 0,7 – 0,2 0,5 3 1,6 1,3 0,9 – 0,4 – 1,8 – 2,1 – 0,7 – 0,2 0,5 Thin layer A 40 130 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 5 1 0,4 – 1,3 – 1,3 – 0,4 – 5,0 – 7,1 – 4,9 – 3,3 – 1,5 2 1,6 1,3 0,9 – 0,4 – 1,8 – 2,1 – 0,7 – 0,2 0,5 3 1,6 1,3 0,9 – 0,4 – 1,8 – 2,1 – 0,7 – 0,2 0,5 Thin layer B 40 130 4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 51.7.2015 EN Official Journal of the European Union L 168/129 Appendix G Database for railway source This appendix presents the database for most of the existing railway noise sources to be used to calculate railway noise following the method described in 2.3 Railway noise. Table G-1 Coefficients L and L for rail and wheel roughness r,TR,i r,VEH,i L r,VEH,i Wavelength Cast iron tread Min Max Composite brake Disk brake brake 1 000 mm – 15,0 25,0 2,2 – 4,0 – 5,9 800 mm – 15,0 25,0 2,2 – 4,0 – 5,9 630 mm – 15,0 25,0 2,2 – 4,0 – 5,9 500 mm – 15,0 25,0 2,2 – 4,0 – 5,9 400 mm – 15,0 25,0 2,2 – 4,0 – 5,9 315 mm – 15,0 25,0 2,2 – 4,0 – 5,9 250 mm – 15,0 25,0 2,2 – 4,0 2,3 200 mm – 15,0 25,0 2,2 – 4,0 2,8 160 mm – 15,0 25,0 2,4 – 4,0 2,6 120 mm – 15,0 25,0 0,6 – 4,0 1,2 100 mm – 15,0 25,0 2,6 – 4,0 2,1 80 mm – 15,0 25,0 5,8 – 4,3 0,9 63 mm – 15,0 25,0 8,8 – 4,6 – 0,3 50 mm – 15,0 25,0 11,1 – 4,9 – 1,6 40 mm – 15,0 25,0 11,0 – 5,2 – 2,9 31,5 mm – 15,0 25,0 9,8 – 6,3 – 4,9 25 mm – 15,0 25,0 7,5 – 6,8 – 7,0 20 mm – 15,0 25,0 5,1 – 7,2 – 8,6 16 mm – 15,0 25,0 3,0 – 7,3 – 9,3 12 mm – 15,0 25,0 1,3 – 7,3 – 9,5 10 mm – 15,0 25,0 0,2 – 7,1 – 10,1 8 mm – 15,0 25,0 – 0,7 – 6,9 – 10,3L 168/130 EN Official Journal of the European Union 1.7.2015 L r,VEH,i Wavelength Cast iron tread Min Max Composite brake Disk brake brake 6,3 mm – 15,0 25,0 – 1,2 – 6,7 – 10,3 5 mm – 15,0 25,0 – 1,0 – 6,0 – 10,8 4 mm – 15,0 25,0 0,3 – 3,7 – 10,9 3,2 mm – 15,0 25,0 0,2 – 2,4 – 9,5 2,5 mm – 15,0 25,0 1,3 – 2,6 – 9,5 2 mm – 15,0 25,0 3,1 – 2,5 – 9,5 1,6 mm – 15,0 25,0 3,1 – 2,5 – 9,5 1,2 mm – 15,0 25,0 3,1 – 2,5 – 9,5 1 mm – 15,0 25,0 3,1 – 2,5 – 9,5 0,8 mm – 15,0 25,0 3,1 – 2,5 – 9,5 L r,VEH,i Wavelength EN ISO 3095:2013 Average network Min Max (Well maintained and (Normally maintained very smooth) smooth) 1 000 mm – 15,0 22,0 17,1 11,0 800 mm – 15,0 22,0 17,1 11,0 630 mm – 15,0 22,0 17,1 11,0 500 mm – 15,0 22,0 17,1 11,0 400 mm – 15,0 22,0 17,1 11,0 315 mm – 15,0 22,0 15,0 10,0 250 mm – 15,0 22,0 13,0 9,0 200 mm – 15,0 22,0 11,0 8,0 160 mm – 15,0 22,0 9,0 7,0 120 mm – 15,0 22,0 7,0 6,0 100 mm – 15,0 22,0 4,9 5,0 80 mm – 15,0 22,0 2,9 4,0 63 mm – 15,0 22,0 0,9 3,0 50 mm – 15,0 22,0 – 1,1 2,0 40 mm – 15,0 22,0 – 3,2 1,01.7.2015 EN Official Journal of the European Union L 168/131 L r,VEH,i Wavelength EN ISO 3095:2013 Average network Min Max (Well maintained and (Normally maintained very smooth) smooth) 31,5 mm – 15,0 22,0 – 5,0 0,0 25 mm – 15,0 22,0 – 5,6 – 1,0 20 mm – 15,0 22,0 – 6,2 – 2,0 16 mm – 15,0 22,0 – 6,8 – 3,0 12 mm – 15,0 22,0 – 7,4 – 4,0 10 mm – 15,0 22,0 – 8,0 – 5,0 8 mm – 15,0 22,0 – 8,6 – 6,0 6,3 mm – 15,0 22,0 – 9,2 – 7,0 5 mm – 15,0 22,0 – 9,8 – 8,0 4 mm – 15,0 22,0 – 10,4 – 9,0 3,2 mm – 15,0 22,0 – 11,0 – 10,0 2,5 mm – 15,0 22,0 – 11,6 – 11,0 2 mm – 15,0 22,0 – 12,2 – 12,0 1,6 mm – 15,0 22,0 – 12,8 – 13,0 1,2 mm – 15,0 22,0 – 13,4 – 14,0 1 mm – 15,0 22,0 – 14,0 – 15,0 0,8 mm – 15,0 22,0 – 14,0 – 15,0 Table G-2 Coefficients A for the contact filter 3,i A 3,i Axle load Axle load Axle load Axle load Axle load Wavelength 50 kN — 50 kN — 25 kN — 50 kN — 100 kN — Min Max wheel wheel wheel wheel wheel diameter diameter diameter diameter diameter 360 mm 680 mm 920 mm 920 mm 920 mm 1 000 mm – 30,0 0,0 0,0 0,0 0,0 0,0 0,0 800 mm – 30,0 0,0 0,0 0,0 0,0 0,0 0,0 630 mm – 30,0 0,0 0,0 0,0 0,0 0,0 0,0 500 mm – 30,0 0,0 0,0 0,0 0,0 0,0 0,0 400 mm – 30,0 0,0 0,0 0,0 0,0 0,0 0,0L 168/132 EN Official Journal of the European Union 1.7.2015 A 3,i Axle load Axle load Axle load Axle load Axle load Wavelength 50 kN — 50 kN — 25 kN — 50 kN — 100 kN — Min Max wheel wheel wheel wheel wheel diameter diameter diameter diameter diameter 360 mm 680 mm 920 mm 920 mm 920 mm 315 mm – 30,0 0,0 0,0 0,0 0,0 0,0 0,0 250 mm – 30,0 0,0 0,0 0,0 0,0 0,0 0,0 200 mm – 30,0 0,0 0,0 0,0 0,0 0,0 0,0 160 mm – 30,0 0,0 0,0 0,0 0,0 0,0 0,0 120 mm – 30,0 0,0 0,0 0,0 0,0 0,0 0,0 100 mm – 30,0 0,0 0,0 0,0 0,0 0,0 0,0 80 mm – 30,0 0,0 0,0 0,0 0,0 – 0,2 – 0,2 63 mm – 30,0 0,0 0,0 – 0,2 – 0,2 – 0,5 – 0,6 50 mm – 30,0 0,0 – 0,2 – 0,4 – 0,5 – 0,9 – 1,3 40 mm – 30,0 0,0 – 0,5 – 0,7 – 0,9 – 1,6 – 2,2 31,5 mm – 30,0 0,0 – 1,2 – 1,5 – 1,6 – 2,5 – 3,7 25 mm – 30,0 0,0 – 2,0 – 2,8 – 2,5 – 3,8 – 5,8 20 mm – 30,0 0,0 – 3,0 – 4,5 – 3,8 – 5,8 – 9,0 16 mm – 30,0 0,0 – 4,3 – 7,0 – 5,8 – 8,5 – 11,5 12 mm – 30,0 0,0 – 6,0 – 10,3 – 8,5 – 11,4 – 12,5 10 mm – 30,0 0,0 – 8,4 – 12,0 – 12,0 – 12,0 – 12,0 8 mm – 30,0 0,0 – 12,0 – 12,5 – 12,6 – 13,5 – 14,0 6,3 mm – 30,0 0,0 – 11,5 – 13,5 – 13,5 – 14,5 – 15,0 5 mm – 30,0 0,0 – 12,5 – 16,0 – 14,5 – 16,0 – 17,0 4 mm – 30,0 0,0 – 13,9 – 16,0 – 16,0 – 16,5 – 18,4 3,2 mm – 30,0 0,0 – 14,7 – 16,5 – 16,5 – 17,7 – 19,5 2,5 mm – 30,0 0,0 – 15,6 – 17,0 – 17,7 – 18,6 – 20,5 2 mm – 30,0 0,0 – 16,6 – 18,0 – 18,6 – 19,6 – 21,5 1,6 mm – 30,0 0,0 – 17,6 – 19,0 – 19,6 – 20,6 – 22,4 1,2 mm – 30,0 0,0 – 18,6 – 20,2 – 20,6 – 21,6 – 23,5 1 mm – 30,0 0,0 – 19,6 – 21,2 – 21,6 – 22,6 – 24,5 0,8 mm – 30,0 0,0 – 20,6 – 22,2 – 22,6 – 23,6 – 25,41.7.2015 EN Official Journal of the European Union L 168/133 Table G-3 Coefficients L L and L for transfer functions H,TR,i H,VEH,i H,VEH,SUP (Values are expressed in Sound Power Level per axle) L H,TR,i Mono- Mono- Bi-block block Mono- Bi-block Bi-block Frequency block sleeper on sleeper on block on sleeper on sleeper on Wooden Min Max sleeper on medium medium hard rail soft rail hard rail sleepers soft rail stiffness stiffness pad pad pad pad rail pad rail pad 50 Hz 0,0 140,0 53,3 50,9 50,1 50,9 50,0 49,8 44,0 63 Hz 0,0 140,0 59,3 57,8 57,2 56,6 56,1 55,9 51,0 80 Hz 0,0 140,0 67,2 66,5 66,3 64,3 64,1 64,0 59,9 100 Hz 0,0 140,0 75,9 76,8 77,2 72,3 72,5 72,5 70,8 125 Hz 0,0 140,0 79,2 80,9 81,6 75,4 75,8 75,9 75,1 160 Hz 0,0 140,0 81,8 83,3 84,0 78,5 79,1 79,4 76,9 200 Hz 0,0 140,0 84,2 85,8 86,5 81,8 83,6 84,4 77,2 250 Hz 0,0 140,0 88,6 90,0 90,7 86,6 88,7 89,7 80,9 316 Hz 0,0 140,0 91,0 91,6 92,1 89,1 89,6 90,2 85,3 400 Hz 0,0 140,0 94,5 93,9 94,3 91,9 89,7 90,2 92,5 500 Hz 0,0 140,0 97,0 95,6 95,8 94,5 90,6 90,8 97,0 630 Hz 0,0 140,0 99,2 97,4 97,0 97,5 93,8 93,1 98,7 800 Hz 0,0 140,0 104,0 101,7 100,3 104,0 100,6 97,9 102,8 1 000 Hz 0,0 140,0 107,1 104,4 102,5 107,9 104,7 101,1 105,4 1 250 Hz 0,0 140,0 108,3 106,0 104,2 108,9 106,3 103,4 106,5 1 600 Hz 0,0 140,0 108,5 106,8 105,4 108,8 107,1 105,4 106,4 2 000 Hz 0,0 140,0 109,7 108,3 107,1 109,8 108,8 107,7 107,5 2 500 Hz 0,0 140,0 110,0 108,9 107,9 110,2 109,3 108,5 108,1 3 160 Hz 0,0 140,0 110,0 109,1 108,2 110,1 109,4 108,7 108,4 4 000 Hz 0,0 140,0 110,0 109,4 108,7 110,1 109,7 109,1 108,7 5 000 Hz 0,0 140,0 110,3 109,9 109,4 110,3 110,0 109,6 109,1 6 350 Hz 0,0 140,0 110,0 109,9 109,7 109,9 109,8 109,6 109,1L 168/134 EN Official Journal of the European Union 1.7.2015 L H,TR,i Mono- Mono- Bi-block block Mono- Bi-block Bi-block Frequency block sleeper on sleeper on block on sleeper on sleeper on Wooden Min Max sleeper on medium medium hard rail soft rail hard rail sleepers soft rail stiffness stiffness pad pad pad pad rail pad rail pad 8 000 Hz 0,0 140,0 110,1 110,3 110,4 110,0 110,0 109,9 109,5 10 000 Hz 0,0 140,0 110,6 111,0 111,4 110,4 110,5 110,6 110,2 L H,VEH,i Wheel with Wheel with Wheel with Wheel with Frequency diameter diameter diameter diameter Min Max 920 mm, no 840 mm, no 680 mm, no 1 200 mm, no measure measure measure measure 50 Hz 60,0 140,0 75,4 75,4 75,4 75,4 63 Hz 60,0 140,0 77,3 77,3 77,3 77,3 80 Hz 60,0 140,0 81,1 81,1 81,1 81,1 100 Hz 60,0 140,0 84,1 84,1 84,1 84,1 125 Hz 60,0 140,0 83,3 82,8 82,8 82,8 160 Hz 60,0 140,0 84,3 83,3 83,3 83,3 200 Hz 60,0 140,0 86,0 84,1 83,9 84,5 250 Hz 60,0 140,0 90,1 86,9 86,3 90,4 316 Hz 60,0 140,0 89,8 87,9 88,0 90,4 400 Hz 60,0 140,0 89,0 89,9 92,2 89,9 500 Hz 60,0 140,0 88,8 90,9 93,9 90,1 630 Hz 60,0 140,0 90,4 91,5 92,5 91,3 800 Hz 60,0 140,0 92,4 91,5 90,9 91,5 1 000 Hz 60,0 140,0 94,9 93,0 90,4 93,6 1 250 Hz 60,0 140,0 100,4 98,7 93,2 100,5 1 600 Hz 60,0 140,0 104,6 101,6 93,5 104,6 2 000 Hz 60,0 140,0 109,6 107,6 99,6 115,6 2 500 Hz 60,0 140,0 114,9 111,9 104,9 115,9 3 160 Hz 60,0 140,0 115,0 114,5 108,0 116,01.7.2015 EN Official Journal of the European Union L 168/135 L H,VEH,i Wheel with Wheel with Wheel with Wheel with Frequency diameter diameter diameter diameter Min Max 920 mm, no 840 mm, no 680 mm, no 1 200 mm, no measure measure measure measure 4 000 Hz 60,0 140,0 115,0 114,5 111,0 116,0 5 000 Hz 60,0 140,0 115,5 115,0 111,5 116,5 6 350 Hz 60,0 140,0 115,6 115,1 111,6 116,6 8 000 Hz 60,0 140,0 116,0 115,5 112,0 117,0 10 000 Hz 60,0 140,0 116,7 116,2 112,7 117,7 L H,VEH,SUP,i Frequency Min Max EU standard 50 Hz 0,0 140,0 0,0 63 Hz 0,0 140,0 0,0 80 Hz 0,0 140,0 0,0 100 Hz 0,0 140,0 0,0 125 Hz 0,0 140,0 0,0 160 Hz 0,0 140,0 0,0 200 Hz 0,0 140,0 0,0 250 Hz 0,0 140,0 0,0 316 Hz 0,0 140,0 0,0 400 Hz 0,0 140,0 0,0 500 Hz 0,0 140,0 0,0 630 Hz 0,0 140,0 0,0 800 Hz 0,0 140,0 0,0 1 000 Hz 0,0 140,0 0,0 1 250 Hz 0,0 140,0 0,0 1 600 Hz 0,0 140,0 0,0 2 000 Hz 0,0 140,0 0,0 2 500 Hz 0,0 140,0 0,0 3 160 Hz 0,0 140,0 0,0 4 000 Hz 0,0 140,0 0,0L 168/136 EN Official Journal of the European Union 1.7.2015 L H,VEH,SUP,i Frequency Min Max EU standard 5 000 Hz 0,0 140,0 0,0 6 350 Hz 0,0 140,0 0,0 8 000 Hz 0,0 140,0 0,0 10 000 Hz 0,0 140,0 0,0 Table G-4 Coefficients L for impact noise R,IMPACT,i L R,IMPACT,i Wavelength Single switch/joint/crossing/ Min Max 100 m 1 000 mm – 40 30 22,4 800 mm – 40 30 22,4 630 mm – 40 30 22,4 500 mm – 40 30 23,8 400 mm – 40 30 24,7 315 mm – 40 30 24,7 250 mm – 40 30 23,4 200 mm – 40 30 21,7 160 mm – 40 30 20,2 120 mm – 40 30 20,4 100 mm – 40 30 20,8 80 mm – 40 30 20,9 63 mm – 40 30 19,8 50 mm – 40 30 18 40 mm – 40 30 16 31,5 mm – 40 30 13 25 mm – 40 30 10 20 mm – 40 30 6 16 mm – 40 30 1 12 mm – 40 30 – 41.7.2015 EN Official Journal of the European Union L 168/137 L R,IMPACT,i Wavelength Single switch/joint/crossing/ Min Max 100 m 10 mm – 40 30 – 11 8 mm – 40 30 – 16,5 6,3 mm – 40 30 – 18,5 5 mm – 40 30 – 21 4 mm – 40 30 – 22,5 3,2 mm – 40 30 – 24,7 2,5 mm – 40 30 – 26,6 2 mm – 40 30 – 28,6 1,6 mm – 40 30 – 30,6 1,2 mm – 40 30 – 32,6 1 mm – 40 30 – 34 0,8 mm – 40 30 – 34 Table G-5 Coefficients L for traction noise W,0,idling (Values are expressed in Sound Power Level per vehicle) L W,0,idling Diesel locomotive Diesel locomotive Frequency Min Max Diesel multiple unit Electric locomotive Electric multiple unit (c. 800 kW) (c. 2 200 kW) SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB 50 Hz 0,0 0,0 140,0 140,0 98,9 103,2 99,4 103,7 82,6 86,9 87,9 92,2 80,5 84,8 63 Hz 0,0 0,0 140,0 140,0 94,8 100,0 107,3 112,5 82,5 87,7 90,8 96,0 81,4 86,6 80 Hz 0,0 0,0 140,0 140,0 92,6 95,5 103,1 106,0 89,3 92,2 91,6 94,5 80,5 83,4 100 Hz 0,0 0,0 140,0 140,0 94,6 94,0 102,1 101,5 90,3 89,7 94,6 94,0 82,2 81,6 125 Hz 0,0 0,0 140,0 140,0 92,8 93,3 99,3 99,8 93,5 94,0 94,8 95,3 80,0 80,5 160 Hz 0,0 0,0 140,0 140,0 92,8 93,6 99,3 100,1 99,5 100,3 96,8 97,6 79,7 80,5 200 Hz 0,0 0,0 140,0 140,0 93,0 92,9 99,5 99,4 98,7 98,6 104,0 103,9 79,6 79,5 250 Hz 0,0 0,0 140,0 140,0 94,8 92,7 101,3 99,2 95,5 93,4 100,8 98,7 96,4 94,3 316 Hz 0,0 0,0 140,0 140,0 94,6 92,4 101,1 98,9 90,3 88,1 99,6 97,4 80,5 78,3 400 Hz 0,0 0,0 140,0 140,0 95,7 92,8 102,2 99,3 91,4 88,5 101,7 98,8 81,3 78,4 500 Hz 0,0 0,0 140,0 140,0 95,6 92,8 102,1 99,3 91,3 88,5 98,6 95,8 97,2 94,4 630 Hz 0,0 0,0 140,0 140,0 98,6 96,8 101,1 99,3 90,3 88,5 95,6 93,8 79,5 77,7L 168/138 EN Official Journal of the European Union 1.7.2015 L W,0,idling Diesel locomotive Diesel locomotive Frequency Min Max Diesel multiple unit Electric locomotive Electric multiple unit (c. 800 kW) (c. 2 200 kW) SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB 800 Hz 0,0 0,0 140,0 140,0 95,2 92,7 101,7 99,2 90,9 88,4 95,2 92,7 79,8 77,3 1 000 Hz 0,0 0,0 140,0 140,0 95,1 93,0 101,6 99,5 91,8 89,7 96,1 94,0 86,7 84,6 1 250 Hz 0,0 0,0 140,0 140,0 95,1 92,9 99,3 97,1 92,8 90,6 92,1 89,9 81,7 79,5 1 600 Hz 0,0 0,0 140,0 140,0 94,1 93,1 96,0 95,0 92,8 91,8 89,1 88,1 82,7 81,7 2 000 Hz 0,0 0,0 140,0 140,0 94,1 93,2 93,7 92,8 90,8 89,9 87,1 86,2 80,7 79,8 2 500 Hz 0,0 0,0 140,0 140,0 99,4 98,3 101,9 100,8 88,1 87,0 85,4 84,3 78,0 76,9 3 160 Hz 0,0 0,0 140,0 140,0 92,5 91,5 89,5 88,5 85,2 84,2 83,5 82,5 75,1 74,1 4 000 Hz 0,0 0,0 140,0 140,0 89,5 88,7 87,1 86,3 83,2 82,4 81,5 80,7 72,1 71,3 5 000 Hz 0,0 0,0 140,0 140,0 87,0 86,0 90,5 89,5 81,7 80,7 80,0 79,0 69,6 68,6 6 350 Hz 0,0 0,0 140,0 140,0 84,1 83,4 31,4 30,7 78,8 78,1 78,1 77,4 66,7 66,0 8 000 Hz 0,0 0,0 140,0 140,0 81,5 80,9 81,2 80,6 76,2 75,6 76,5 75,9 64,1 63,5 10 000 Hz 0,0 0,0 140,0 140,0 79,2 78,7 79,6 79,1 73,9 73,4 75,2 74,7 61,8 61,3 Table G-6 Coefficients L , L , α , α for aerodynamic noise W,0,1 W,0,2 1 2 (Values are expressed in Sound Power Level per vehicle (for a vehicle length of 20 m)) Aerodynamic noise given at Min Max 300 km/h α α α α α α Frequency 1 2 1 2 1 2 0 0 100 100 50 50 L L L L L L W,0,1 W,0,2 W,0,1 W,0,2 W,0,1 W,0,2 50 Hz 0 0 140 140 112,6 36,7 63 Hz 0 0 140 140 113,2 38,5 80 Hz 0 0 140 140 115,7 39,0 100 Hz 0 0 140 140 117,4 37,5 125 Hz 0 0 140 140 115,3 36,8 160 Hz 0 0 140 140 115,0 37,1 200 Hz 0 0 140 140 114,9 36,4 250 Hz 0 0 140 140 116,4 36,2 316 Hz 0 0 140 140 115,9 35,9 400 Hz 0 0 140 140 116,3 36,31.7.2015 EN Official Journal of the European Union L 168/139 Aerodynamic noise given at Min Max 300 km/h α α α α α α Frequency 1 2 1 2 1 2 0 0 100 100 50 50 L L L L L L W,0,1 W,0,2 W,0,1 W,0,2 W,0,1 W,0,2 500 Hz 0 0 140 140 116,2 36,3 630 Hz 0 0 140 140 115,2 36,3 800 Hz 0 0 140 140 115,8 36,2 1 000 Hz 0 0 140 140 115,7 36,5 1 250 Hz 0 0 140 140 115,7 36,4 1 600 Hz 0 0 140 140 114,7 105,2 2 000 Hz 0 0 140 140 114,7 110,3 2 500 Hz 0 0 140 140 115,0 110,4 3 160 Hz 0 0 140 140 114,5 105,6 4 000 Hz 0 0 140 140 113,1 37,2 5 000 Hz 0 0 140 140 112,1 37,5 6 350 Hz 0 0 140 140 110,6 37,9 8 000 Hz 0 0 140 140 109,6 38,4 10 000 Hz 0 0 140 140 108,8 39,2 Table G-7 Coefficients C for structural radiation bridge C bridge Predominantly concrete or Predominantly steel bridges min max masonry bridges with any with ballasted track trackform 0 9 1 4L 168/140 EN Official Journal of the European Union 1.7.2015 Appendix H Database for industrial source This appendix presents a few examples for input values for some industrial noise sources that may be used to calculate industrial noise following the method described in 2.4 Industrial noise. As industrial noise sources are extremely specific for each industrial site, appropriate values are obtained from local, national or international databases or measurements as appropriate. Table H-1 Coefficients L , L and ΔL (x, y, z) for sound power W W' W,dir,xyz ΔL (x, y, z)=0 W,dir,xyz L is expressed as sound power per metre for line source, or per squared metre for area source. W' Type of Source direc­ Description 63 125 250 500 1 000 2 000 4 000 8 000 source tivity Grit blasting PointSource FreeField 108,77 110,37 112,77 107,77 104,37 98,07 97,07 86,97 — outside — with nozzle Rotary kiln LineSource FreeField 79,27 84,17 86,67 89,27 93,07 93,47 92,07 87,77 Ship yard AreaSource HemiSpher­ 67,17 69,07 74,57 62,17 63,97 66,77 70,97 68,07 ical Gas terminal AreaSource HemiSpher­ 74,17 70,07 65,57 64,17 59,97 57,77 51,97 56,07 ical1.7.2015 EN Official Journal of the European Union L 168/141 Appendix I Database for aircraft source — NPD data This appendix presents the database for most of the existing aircraft noise sources to be used to calculate aircraft noise following the method described in 2.6 Aircraft noise. Table I-1 Aerodynamic coefficients ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 1900D A 35-A 0,915858 0,130495 1900D A A_40D 0,416345 0,140491 1900D A ZERO-A 0,106643 1900D D 17-D 0,060076 0,858496 0,072968 1900D D ZERO-D 0,094383 707320 A D-25 0,307537 0,107756 707320 A D-40 0,279116 0,134567 707320 A D-50 0,275511 0,15472 707320 A U-25 0,098219 707320 D 14 0,004514 0,312431 0,089316 707320 D INT 0,072743 707320 D ZERO 0,05617 707QN A D-25 0,307537 0,107756 707QN A D-40 0,279116 0,134567 707QN A D-50 0,275511 0,15472 707QN A U-25 0,098219 707QN D 14 0,004514 0,312431 0,089316 707QN D INT 0,072743 707QN D ZERO 0,05617 717200 A A_0U 0,06456 717200 A A_13D 0,109249 717200 A A_13U 0,095353 717200 A A_18D 0,11009 717200 A A_18U 0,095015 717200 A A_40D 0,416345 0,140491 717200 D T_00B 0,06L 168/142 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 717200 D T_00C 0,06 717200 D T_05H 0,011607 0,483254 0,075 717200 D T_05M 0,011795 0,489068 0,075 717200 D T_13A 0,010862 0,469923 0,078 720B A D-30 0,350247 0,109478 720B A D-50 0,339412 0,148843 720B A U-30 0,09805 720B D 20 0,00573 0,356426 0,091933 720B D 30 0,005238 0,340735 0,104243 720B D INT 0,074052 720B D ZERO 0,05617 727100 A D-25 0,350485 0,128359 727100 A D-30 0,343897 0,145903 727100 A D-40 0,335992 0,186604 727100 A U-15 0,090698 727100 A U-25 0,113154 727100 D 2 0,0857 727100 D 5 0,008692 0,415048 0,088916 727100 D 15 0,008301 0,392649 0,095459 727100 D 25 0,007389 0,371567 0,115623 727100 D ZERO 0,0636 727D15 A D-25 0,383689 0,109535 727D15 A D-30 0,368 0,1437 727D15 A D-40 0,36 0,1844 727D15 A U-15 0,089969 727D15 A U-25 0,109535 727D15 D 2 0,0857 727D15 D 5 0,00924 0,409 0,0869 727D15 D 15 0,00826 0,388 0,0929 727D15 D 20 0,007712 0,376653 0,108897 727D15 D 25 0,00763 0,367 0,1112 727D15 D ZERO 0,0594 727D17 A D-25 0,383689 0,1248211.7.2015 EN Official Journal of the European Union L 168/143 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 727D17 A D-30 0,368 0,1437 727D17 A D-40 0,36 0,1844 727D17 A U-15 0,089969 727D17 A U-25 0,109535 727D17 D 2 0,0857 727D17 D 5 0,00924 0,409 0,0869 727D17 D 15 0,00826 0,388 0,0929 727D17 D 20 0,007712 0,376653 0,108897 727D17 D 25 0,00763 0,367 0,1112 727D17 D ZERO 0,0594 727EM1 A D-25 0,350485 0,128359 727EM1 A D-30 0,343897 0,145903 727EM1 A D-40 0,335992 0,186604 727EM1 A U-15 0,090698 727EM1 A U-25 0,113154 727EM1 D 2 0,0857 727EM1 D 5 0,008692 0,415048 0,088916 727EM1 D 15 0,008301 0,392649 0,095459 727EM1 D 25 0,007389 0,371567 0,115623 727EM1 D ZERO 0,0636 727EM2 A D-25 0,383689 0,109535 727EM2 A D-30 0,368 0,1437 727EM2 A D-40 0,36 0,1844 727EM2 A U-15 0,089969 727EM2 A U-25 0,109535 727EM2 D 2 0,0857 727EM2 D 5 0,00924 0,409 0,0869 727EM2 D 15 0,00826 0,388 0,0929 727EM2 D 20 0,007712 0,376653 0,108897 727EM2 D 25 0,00763 0,367 0,1112 727EM2 D ZERO 0,0594 727Q15 A D-25 0,383689 0,109535 727Q15 A D-30 0,368 0,1437L 168/144 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 727Q15 A D-40 0,36 0,1844 727Q15 A U-15 0,089969 727Q15 A U-25 0,109535 727Q15 D 2 0,0857 727Q15 D 5 0,00924 0,409 0,0869 727Q15 D 15 0,00826 0,388 0,0929 727Q15 D 20 0,007712 0,376653 0,108897 727Q15 D 25 0,00763 0,367 0,1112 727Q15 D ZERO 0,0594 727Q7 A D-25 0,350485 0,128359 727Q7 A D-30 0,343897 0,145903 727Q7 A D-40 0,335992 0,186604 727Q7 A U-15 0,090698 727Q7 A U-25 0,113154 727Q7 D 2 0,0857 727Q7 D 5 0,008692 0,415048 0,088916 727Q7 D 15 0,008301 0,392649 0,095459 727Q7 D 25 0,007389 0,371567 0,115623 727Q7 D ZERO 0,0636 727Q9 A D-25 0,372885 0,124565 727Q9 A D-30 0,367614 0,142606 727Q9 A D-40 0,359182 0,184273 727Q9 A U-15 0,090523 727Q9 A U-25 0,109315 727Q9 D 2 0,0857 727Q9 D 5 0,00924 0,409 0,0869 727Q9 D 15 0,00826 0,388 0,0929 727Q9 D 20 0,007712 0,376653 0,108897 727Q9 D 25 0,00763 0,367 0,1112 727Q9 D ZERO 0,0594 727QF A D-15 0,1182 727QF A D-25 0,1359 727QF A D-30 0,3658 0,16021.7.2015 EN Official Journal of the European Union L 168/145 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 727QF A D-40 0,3568 0,2003 727QF A U-05 0,08709 727QF A U-15 0,09676 727QF A U-25 0,1201 727QF A U-ZERO 0,06027 727QF D 2 0,081 727QF D 5 0,00849 0,4242 0,0921 727QF D 15 0,007525 0,412 0,1005 727QF D 25 0,0069 0,3885 0,1222 727QF D ZERO 0,06599 737 A D-25 0,452885 0,113106 737 A D-30 0,442783 0,124898 737 A D-40 0,432682 0,155057 737 A U-15 0,088617 737 A U-25 0,097687 737 D 5 0,011593 0,475473 0,085235 737 D 10 0,010935 0,457438 0,093192 737 D 25 0,010293 0,436124 0,109993 737 D INT 0,07477 737 D ZERO 0,0643 737300 A D-15 0,4639 0,1103 737300 A D-30 0,434 0,1247 737300 A D-40 0,4215 0,1471 737300 D 1 0,0126 0,4958 0,069 737300 D 5 0,0116 0,477215 0,0742 737300 D 15 0,0111 0,4572 0,0872 737300 D ZERO 0,062 7373B2 A D-15 0,4639 0,1103 7373B2 A D-30 0,434 0,1247 7373B2 A D-40 0,4215 0,1471 7373B2 D 1 0,0124 0,4958 0,0761 7373B2 D 5 0,011511 0,477758 0,0794 7373B2 D 15 0,011 0,4575 0,0872 7373B2 D T_01 0,067L 168/146 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 7373B2 D T_05 0,074679 7373B2 D ZERO 0,062 737400 A D-15 0,4779 0,1079 737400 A D-30 0,4338 0,1251 737400 A D-40 0,423 0,151 737400 D 1 0,0713 737400 D 5 0,0117 0,4834 0,0798 737400 D 15 0,0109 0,4596 0,0924 737400 D ZERO 0,0628 737500 A D-15 0,4538 0,1084 737500 A D-30 0,4281 0,1253 737500 A D-40 0,4166 0,151 737500 D 1 0,0712 737500 D 5 0,01138 0,474697 0,0803 737500 D 15 0,0109 0,4541 0,0925 737500 D ZERO 0,061 737700 A A_15 0,4122 0,1048 737700 A A_30 0,3986 0,1194 737700 A A_40 0,3907 0,1434 737700 D T_00H 0,063 737700 D T_01 0,0097 0,4329 0,062 737700 D T_05A 0,07 737700 D T_10 0,0089 0,4112 0,0858 737700 D T_15 0,0087 0,406 0,0889 737700 D T_25 0,0086 0,4021 0,0932 737700 D T_5 0,0093 0,4251 0,0749 737700 D T_ZERO 0,0552 737800 D T_00 0,05625 737800 D T_01 0,06253 737800 D T_05 0,009633 0,435043 0,0737 737D17 A D-25 0,451848 0,113169 737D17 A D-30 0,443779 0,1252521.7.2015 EN Official Journal of the European Union L 168/147 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 737D17 A D-40 0,434096 0,156502 737D17 A U-15 0,106085 737D17 A U-25 0,097127 737D17 D 5 0,011677 0,473007 0,087424 737D17 D 10 0,010956 0,456114 0,096364 737D17 D 25 0,010406 0,436124 0,10878 737D17 D INT 0,07586 737D17 D ZERO 0,0643 737N17 A D-25 0,451848 0,113169 737N17 A D-30 0,443779 0,125252 737N17 A D-40 0,434096 0,156502 737N17 A U-15 0,106085 737N17 A U-25 0,097127 737N17 D 5 0,011677 0,473007 0,087424 737N17 D 10 0,010956 0,456114 0,096364 737N17 D 25 0,010406 0,436124 0,10878 737N17 D INT 0,07586 737N17 D ZERO 0,0643 737N9 A D-25 0,452885 0,113106 737N9 A D-30 0,442783 0,124898 737N9 A D-40 0,432682 0,155057 737N9 A U-15 0,088617 737N9 A U-25 0,097687 737N9 D 5 0,011593 0,475473 0,085235 737N9 D 10 0,010935 0,457438 0,093192 737N9 D 25 0,010293 0,436124 0,109993 737N9 D INT 0,07477 737N9 D ZERO 0,0643 737QN A D-25 0,452885 0,113106 737QN A D-30 0,442783 0,124898 737QN A D-40 0,432682 0,155057 737QN A U-15 0,088617 737QN A U-25 0,097687L 168/148 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 737QN D 5 0,011593 0,475473 0,085235 737QN D 10 0,010935 0,457438 0,093192 737QN D 25 0,010293 0,436124 0,109993 737QN D INT 0,07477 737QN D ZERO 0,0643 74710Q A D-20 0,217555 0,109467 74710Q A D-25 0,210537 0,116953 74710Q A D-30 0,202116 0,142564 74710Q A U-20 0,091737 74710Q D 5 0,07456 74710Q D 10 0,002333 0,212212 0,092196 74710Q D 20 0,002187 0,202456 0,099504 74710Q D ZERO 0,05693 747200 A D-20 0,217555 0,109467 747200 A D-25 0,210537 0,116953 747200 A D-30 0,202116 0,142564 747200 A U-20 0,091737 747200 D 5 0,074042 747200 D 10 0,00235 0,211659 0,091154 747200 D 20 0,002207 0,203133 0,098616 747200 D ZERO 0,05693 74720A A D-25 0,2105 0,118 74720A A D-30 0,2017 0,1438 74720A D 5 0,0722 74720A D 10 0,00234 0,2115 0,08917 74720A D 20 0,002186 0,2029 0,09728 74720A D ZERO 0,05524 74720B A D-25 0,2113 0,1207 74720B A D-30 0,2016 0,1444 74720B D 5 0,07276 74720B D 10 0,002351 0,213 0,0886 74720B D 20 0,002196 0,2045 0,09867 74720B D ZERO 0,056931.7.2015 EN Official Journal of the European Union L 168/149 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 747400 A D-25 0,2143 0,1171 747400 A D-30 0,2064 0,141 747400 D 5 0,069 747400 D 10 0,002104 0,21338 0,0823 747400 D 20 0,0021 0,2062 0,0916 747400 D T_00H 0,053 747400 D T_01 0,057691 747400 D T_05 0,071 747400 D T_05C 0,057569 747400 D T_10 0,002101 0,207131 0,110782 747400 D T_10H 0,1 747400 D ZERO 0,3111 0,0508 7478 A F_20 0,192660 0,128462 7478 A F_30 0,189605 0,143406 7478 D F_0 0,052717 7478 D F_1 0,064841 7478 D F_10 0,002000 0,204760 0,083321 7478 D F_5 0,073443 747SP A D-20 0,216415 0,110347 747SP A D-25 0,209991 0,116897 747SP A D-30 0,202497 0,143096 747SP A U-20 0,092569 747SP D 5 0,076123 747SP D 10 0,002357 0,210572 0,095316 747SP D 20 0,002179 0,201901 0,103296 747SP D ZERO 0,05693 757300 D T_00 0,05554 757300 D T_01 0,05943 757300 D T_05 0,006931 0,38754 0,07993 757PW A D-25 0,3234 0,1186 757PW A D-30 0,3179 0,1342 757PW D 5 0,006243 0,360271 0,0722 757PW D 15 0,00611 0,3454 0,0782L 168/150 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 757PW D 20 0,00573 0,33 0,0864 757PW D T_00 0,055346 757PW D T_01 0,0609 757PW D T_05 0,360271 0,0682 757PW D ZERO 0,4699 0,0548 757RR A D-25 0,3238 0,1178 757RR A D-30 0,3191 0,1337 757RR D 5 0,006319 0,36165 0,07 757RR D 15 0,00614 0,3454 0,0758 757RR D 20 0,0057 0,33 0,0847 757RR D INT 0,0621 757RR D T_00 0,0525 757RR D T_01 0,058316 757RR D T_05 0,0635 757RR D ZERO 0,4699 0,0541 767300 A D-25 0,2627 0,121 767300 A D-30 0,2555 0,1329 767300 D 5 0,00409 0,297 0,075 767300 D 15 0,00381 0,2853 0,0824 767300 D 20 0,00367 0,2788 0,0866 767300 D INT 0,0641 767300 D ZERO 0,0531 767400 A L_25_D 0,2601 0,1156 767400 A L_30_D 0,2536 0,1265 767400 D T_00_U 0,0492 767400 D T_05_U 0,0043 0,2972 0,0674 767400 D T_05A 0,055 767400 D T_05B 0,06 767400 D T_15_U 0,0041 0,2876 0,0736 767400 D T_20_U 0,003624 0,2775 0,0794 767CF6 A D-25 0,29009 0,1075 767CF6 A D-30 0,28096 0,1232 767CF6 D 1 0,00557 0,31625 0,06461.7.2015 EN Official Journal of the European Union L 168/151 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 767CF6 D 5 0,0053 0,30576 0,0685 767CF6 D 15 0,00504 0,29249 0,074 767CF6 D 20 0,0049 0,28496 0,0779 767CF6 D ZERO 0,0489 767JT9 A D-25 0,29009 0,1085 767JT9 A D-30 0,28096 0,1258 767JT9 D 1 0,00504 0,31625 0,0658 767JT9 D 5 0,00472 0,30576 0,0705 767JT9 D 15 0,00436 0,29249 0,0756 767JT9 D 20 0,00417 0,28496 0,0802 767JT9 D ZERO 0,052 777200 A D20 0,2204 0,09765 777200 A D25 0,2133 0,1158 777200 A D30 0,203 0,133 777200 D 15 0,002867 0,2299 0,07432 777200 D 20 0,002751 0,2239 0,08186 777200 D T_00 0,3218 0,05065 777200 D T_00H 0,052 777200 D T_00L 0,048 777200 D T_01 0,2921 0,05555 777200 D T_01H 0,06 777200 D T_05 0,002475 0,239429 0,06898 777200 D T_05A 0,063456 777200 D T_05C 0,092 777200 D T_05CH 0,085 777300 A L_25_D 0,2156 0,116 777300 A L_30_D 0,2071 0,1322 777300 D T_00_U 0,0504 777300 D T_05_U 0,0031 0,2586 0,0645 777300 D T_15_U 0,0028 0,2454 0,0704 777300 D T_20_U 0,0027 0,2363 0,0783 7773ER A F_20 0,225340 0,104970 7773ER A F_30 0,209490 0,134910L 168/152 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 7773ER D FLAP_0 0,050171 7773ER D FLAP_1 0,054934 7773ER D FLAP_5 0,002710 0,240000 0,066100 7878R A F_00 0,393870 0,045060 7878R A F_01 0,329760 0,047700 7878R A F_05 0,288410 0,067150 7878R A FLAP20 0,260280 0,088050 7878R A FLAP30 0,246840 0,105000 7878R D FLAP_0 0,050055 7878R D FLAP_1 0,052026 7878R D FLAP_5 0,002949 0,256410 0,071636 A300-622R A 1 0,071539 A300-622R A 2_D 0,094763 A300-622R A 2_U 0,072592 A300-622R A 3_D 0,274926 0,102372 A300-622R A FULL_D 0,253296 0,125036 A300-622R A ZERO 0,052053 A300-622R D 0 0,053127 A300-622R D 1500 0,004121 0,292 0,072348 A300B4-203 A D-15 0,28237 0,10607 A300B4-203 A D-25 0,27151 0,125568 A300B4-203 D 1 0,005307 0,324359 0,090223 A300B4-203 D 8 0,004239 0,291059 0,093067 A300B4-203 D 15 0,00402 0,278999 0,102935 A300B4-203 D ZERO 0,063491 A310-304 A 1 0,068197 A310-304 A 2_D 0,096731 A310-304 A 2_U 0,072778 A310-304 A 3_D 0,274926 0,106084 A310-304 A FULL_D 0,253296 0,129438 A310-304 A ZERO 0,054935 A310-304 D 0 0,055191 A310-304 D 1500 0,004875 0,313705 0,0720161.7.2015 EN Official Journal of the European Union L 168/153 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R A319-131 A 1_A 0,06317 A319-131 A 2_D 0,098119 A319-131 A 2_U 0,071826 A319-131 A 3_D 0,379931 0,098121 A319-131 A FULL_D 0,355927 0,124534 A319-131 A ZERO_A 0,056446 A319-131 D 1 0,071598 A319-131 D 1+F 0,007077 0,376764 0,072635 A319-131 D ZERO 0,05429 A320-211 A 1_A 0,061662 A320-211 A 2_D 0,096267 A320-211 A 2_U 0,067463 A320-211 A 3_D 0,385223 0,101204 A320-211 A FULL_D 0,37052 0,11586 A320-211 A ZERO_A 0,057558 A320-211 D 1 0,066827 A320-211 D 1+F 0,007701 0,394884 0,071403 A320-211 D ZERO 0,056281 A320-232 A 1_A 0,059086 A320-232 A 2_D 0,095899 A320-232 A 2_U 0,06679 A320-232 A 3_D 0,379853 0,100263 A320-232 A FULL_D 0,369833 0,121141 A320-232 A ZERO_A 0,054309 A320-232 D 1 0,065822 A320-232 D 1+F 0,007626 0,395674 0,069873 A320-232 D ZERO 0,05332 A321-232 A 1_A 0,064258 A321-232 A 2_D 0,101798 A321-232 A 2_U 0,074849 A321-232 A 3_D 0,368096 0,112676 A321-232 A FULL_D 0,357761 0,119073 A321-232 A ZERO_A 0,057183L 168/154 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R A321-232 D 1 0,071631 A321-232 D 1+F 0,007524 0,390238 0,075946 A321-232 D ZERO 0,056647 A330-301 A 1_A 0,057783 A330-301 A 2_D 0,081654 A330-301 A 2_U 0,064098 A330-301 A 3_D 0,229065 0,092737 A330-301 A FULL_D 0,222802 0,100779 A330-301 A ZERO_A 0,047685 A330-301 D 1 0,059866 A330-301 D 1+F 0,002905 0,247076 0,061736 A330-301 D ZERO 0,046057 A330-343 A 1_A 0,055464 A330-343 A 2_D 0,083569 A330-343 A 2_U 0,063042 A330-343 A 3_D 0,229705 0,092555 A330-343 A FULL_D 0,222498 0,10202 A330-343 A ZERO_A 0,046224 A330-343 D 1 0,05926 A330-343 D 1+F 0,0029 0,245211 0,062365 A330-343 D ZERO 0,044593 A340-211 A 1_A 0,063657 A340-211 A 2_D 0,092945 A340-211 A 2_U 0,071673 A340-211 A 3_D 0,224603 0,101734 A340-211 A FULL_D 0,220432 0,108554 A340-211 A ZERO_A 0,051221 A340-211 D 1 0,068547 A340-211 D 1+F 0,002605 0,223635 0,073134 A340-211 D ZERO 0,048646 A340-642 A 1_A 0,054416 A340-642 A 2_D 0,087508 A340-642 A 2_U 0,0679961.7.2015 EN Official Journal of the European Union L 168/155 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R A340-642 A 3_D 0,213821 0,100473 A340-642 A FULL_D 0,20733 0,105616 A340-642 A ZERO_A 0,051608 A340-642 D 1 0,06118 A340-642 D 1+F 0,002423 0,225716 0,06743 A340-642 D ZERO 0,051433 A380-841 A A_1+F 0,055657 A380-841 A A_2_D 0,081906 A380-841 A A_2_U 0,064109 A380-841 A A_3_D 0,154745 0,101662 A380-841 A A_FULL 0,154745 0,107331 A380-841 A ZERO_A 0,050279 A380-841 D D_1 0,053173 A380-841 D D_1+F 0,00125 0,159626 0,068055 A380-841 D ZERO 0,050472 A380-861 A A_1+F 0,058557 A380-861 A A_2_D 0,081967 A380-861 A A_2_U 0,06558 A380-861 A A_3_D 0,154745 0,101738 A380-861 A A_FULL 0,154745 0,108118 A380-861 A ZERO_A 0,048776 A380-861 D D_1 0,053241 A380-861 D D_1+F 0,00125 0,159567 0,070602 A380-861 D ZERO 0,049623 BAC111 A D-45 0,49076 0,139207 BAC111 A U-INT 0,106398 BAC111 D 8 0,01569 0,54382 0,082179 BAC111 D INT1 0,07359 BAC111 D ZERO 0,065 BAE146 A D-18 0,61667 0,119715 BAE146 A D-24 0,61667 0,138371 BAE146 A D-33 0,45555 0,153186 BAE146 A U-18 0,0818L 168/156 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R BAE146 A U-24 0,095298 BAE146 D 18 0,009678 0,49296 0,13241 BAE146 D 24 0,008979 0,45846 0,1412 BAE146 D 30 0,008173 0,43179 0,15287 BAE146 D ZERO 0,083096 BAE300 A D-18 0,60557 0,116925 BAE300 A D-24 0,60557 0,134808 BAE300 A D-33 0,4511 0,149009 BAE300 A U-18 0,08058 BAE300 A U-24 0,093519 BAE300 D 18 0,009449 0,49847 0,1279 BAE300 D 24 0,008341 0,462 0,1352 BAE300 D 30 0,00775 0,43351 0,14711 BAE300 D ZERO 0,081866 BEC58P A D-15 0,14885 BEC58P A D-30 1,33492 0,16 BEC58P D TO 0,100258 1,28098 0,1377 BEC58P D ZERO 0,125381 CIT3 A D-40 0,966375 0,147159 CIT3 A D-INTR 0,130842 CIT3 D 10 0,092263 CIT3 D 20 0,04284 0,947523 0,114525 CIT3 D ZERO 0,07 CL600 A D-45 0,766248 0,169002 CL600 A D-INTR 0,128747 CL600 D 10 0,079246 CL600 D 20 0,028225 0,780719 0,088492 CL600 D ZERO 0,07 CL601 A D-45 0,769487 0,163669 CL601 A D-INTR 0,122639 CL601 D 10 0,075805 CL601 D 20 0,032183 0,780565 0,081609 CL601 D ZERO 0,071.7.2015 EN Official Journal of the European Union L 168/157 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R CNA172 A 10-D 1,3132 0,0994 CNA172 A 30-D 1,2526 0,1516 CNA172 A ZERO-D 0,096 CNA172 D 10-C 0,0992 1,0304 0,1446 CNA172 D CRUISE 0,096 CNA172 D ZERO-C 0,1025 1,1112 0,0831 CNA182 A F10APP 0,122 CNA182 A F30APP 1,285 0,151 CNA182 D F-20D 0,058 1,204 0,17 CNA182 D ZERO 0,127 CNA182 D ZERO-A 0,127 CNA182 D ZERO-C 0,097 CNA182 D ZERO-T 0,103 CNA206 A 10_D 0,105632 CNA206 A 40_D 1,23852 0,169084 CNA206 D 20_T 0,055005 1,02562 0,136998 CNA206 D ZERO_C 0,09563 CNA206 D ZERO_T 0,055005 1,02562 0,106327 CNA208 A F30APP 0,867722 0,099468 CNA208 A ZERO-A 0,089802 CNA208 D F-20D 0,033202 0,74833 0,105087 CNA208 D ZERO 0,05003 0,887307 0,089802 CNA208 D ZERO-C 0,087252 CNA208 D ZERO-T 0,060282 CNA20T A 10_D 0,109615 CNA20T A 40_D 1,32574 0,211577 CNA20T D 20_T 0,054669 1,045287 0,13795 CNA20T D ZERO_C 0,101535 CNA20T D ZERO_T 0,054669 0,959417 0,099791 CNA441 A D-INTR 0,141579 CNA441 A D-L 1,02329 0,162936 CNA441 D TO 0,072722 1,10834 0,120222 CNA441 D ZERO 0,096518L 168/158 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R CNA500 A D-35 0,991547 0,147335 CNA500 A D-INTR 0,113809 CNA500 D 1 0,080282 CNA500 D 12 0,054342 0,956752 0,090564 CNA500 D ZERO 0,07 CNA510 A A_15 1,073624 0,088506 CNA510 A A_35 1,002913 0,126185 CNA510 D D_15 0,07051 1,179843 0,097415 CNA510 D ZERO_C 0,088914 CNA510 D ZERO_D 0,090811 1,347624 0,103158 CNA525C A A_15 1,012614 0,106795 CNA525C A A_35 0,946574 0,126615 CNA525C D D-15 0,053355 0,993147 0,096525 CNA525C D ZERO_C 0,085 CNA525C D ZERO_D 0,061279 1,065348 0,09129 CNA55B A A_15 1,01427 0,118086 CNA55B A A_35 0,9553 0,200794 CNA55B D D_15 0,05628 1,080923 0,128052 CNA55B D ZERO_C 0,10833 CNA55B D ZERO_D 0,063189 1,159835 0,119835 CNA560E D 15 0,054336 1,014289 0,122203 CNA560E A 15 U 0,919106 0,099403 CNA560E A 35 D 0,870372 0,130841 CNA560E D 7 0,059522 1,061591 0,11951 CNA560E D ZERO 0,122635 CNA560U D 15 0,038136 1,069934 0,13523 CNA560U D 7 0,041179 1,10518 0,12699 CNA560U A 7_APP 0,12699 CNA560U A D 15 0,86464 0,088125 CNA560U A D 35 0,811918 0,132402 CNA560U D ZERO 0,07 CNA560XL D 15 0,030657 1,045811 0,13852 CNA560XL D 7 0,035712 1,095308 0,135051.7.2015 EN Official Journal of the European Union L 168/159 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R CNA560XL A D 15U 0,91189 0,08555 CNA560XL A D 35D 0,86179 0,126192 CNA560XL D ZERO 0,074551 CNA680 D 15 0,027468 0,725152 0,127804 CNA680 A 15 GU 0,717794 0,093247 CNA680 A 35 GD 0,662727 0,146827 CNA680 D 7 0,030105 0,764412 0,122083 CNA680 D ZERO 0,105329 CNA750 A 15_GD 0,753068 0,174519 CNA750 A 15_GU 0,753068 0,146147 CNA750 A 35_GD 0,714646 0,250382 CNA750 A 5_GU 0,799175 0,118139 CNA750 D 5 0,038446 0,82511 0,122657 CNA750 D 15 0,034761 0,787004 0,12822 CNA750 D ZERO 0,096475 CONCRD A D-L 0,349148 0,205927 CONCRD A U-L 0,183067 CONCRD D CL1 0,13294 CONCRD D TO 0,008051 0,338363 0,13294 CONCRD D ZERO 0,13294 CRJ9-ER A 20 0,0976 CRJ9-ER A D-45 0,5801 0,1551 CRJ9-ER A U-45 0,1504 CRJ9-ER A ZERO 0,0655 CRJ9-ER D 0-204 0,0599 CRJ9-ER D 0-250 0,0641 CRJ9-ER D D-8 0,0177 0,5902 0,0978 CRJ9-ER D U-8 0,0775 CRJ9-LR A 20 0,0976 CRJ9-LR A D-45 0,5801 0,1551 CRJ9-LR A U-45 0,1504 CRJ9-LR A ZERO 0,0655 CRJ9-LR D 0-204 0,0599L 168/160 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R CRJ9-LR D 0-250 0,0641 CRJ9-LR D D-8 0,0177 0,5902 0,0978 CRJ9-LR D U-8 0,0775 CVR580 A D-28 0,51972 0,118937 CVR580 A D-40 0,49138 0,124222 CVR580 D 10 0,028303 0,540116 0,130717 CVR580 D INTR 0,102858 CVR580 D ZERO 0,075 DC1010 A D-35 0,251236 0,132645 DC1010 A D-50 0,244243 0,164729 DC1010 A U-35 0,127457 DC1010 A U-50 0,161155 DC1010 D 5 0,079893 DC1010 D 10 0,00356 0,261942 0,101376 DC1010 D INT 0,068522 DC1010 D ZERO 0,057149 DC1030 A D-35 0,2534 0,13 DC1030 A U-20 0,104 DC1030 D 20 0,003091 0,2434 0,104 DC1030 D INT1 0,09454 DC1030 D INT2 0,07307 DC1030 D ZERO 0,06519 DC1040 A D-35 0,254879 0,121114 DC1040 A D-50 0,247241 0,151007 DC1040 A U-35 0,114222 DC1040 A U-50 0,145481 DC1040 D 5 0,082503 DC1040 D 15 0,004009 0,272697 0,111044 DC1040 D INT 0,071264 DC1040 D ZERO 0,060025 DC3 A D-45 0,597793 0,155222 DC3 A U-INT 0,133361 DC3 D TO 0,019837 0,619256 0,1237841.7.2015 EN Official Journal of the European Union L 168/161 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R DC3 D ZERO 0,1115 DC6 A D-INTR 0,10199 DC6 A D-L 0,294594 0,125979 DC6 D TO 0,007829 0,430006 0,08204 DC6 D ZERO 0,078 DC850 A D-35 0,328558 0,129965 DC850 A D-50 0,313281 0,149354 DC850 A U-35 0,126751 DC850 A U-50 0,145337 DC850 D 15 0,005206 0,323443 0,090417 DC850 D 25 0,004708 0,315832 0,103092 DC850 D INT 0,074401 DC850 D ZERO 0,058535 DC860 A D-35 0,312879 0,117758 DC860 A D-50 0,304526 0,130913 DC860 A U-35 0,115049 DC860 A U-50 0,12766 DC860 D 12 0,004899 0,320082 0,090214 DC860 D 23 0,004572 0,304797 0,095953 DC860 D INT 0,071703 DC860 D ZERO 0,05319 DC870 A D-35 0,312879 0,117758 DC870 A D-50 0,304526 0,130913 DC870 A U-35 0,115049 DC870 A U-50 0,12766 DC870 D 12 0,004899 0,320082 0,090214 DC870 D 23 0,004572 0,304797 0,095953 DC870 D INT 0,071703 DC870 D ZERO 0,05319 DC8QN A D-35 0,312879 0,117758 DC8QN A D-50 0,304526 0,130913 DC8QN A U-35 0,115049 DC8QN A U-50 0,12766L 168/162 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R DC8QN D 12 0,004899 0,320082 0,090214 DC8QN D 23 0,004572 0,304797 0,095953 DC8QN D INT 0,071703 DC8QN D ZERO 0,05319 DC910 A D-35 0,480101 0,134177 DC910 A D-50 0,445486 0,157948 DC910 A U-15 0,087963 DC910 A U-35 0,130625 DC910 A U-50 0,153365 DC910 D 5 0,012996 0,49557 0,07757 DC910 D 15 0,010618 0,477234 0,087963 DC910 D INT 0,076753 DC910 D ZERO 0,075935 DC930 A D-35 0,470211 0,135075 DC930 A D-50 0,438965 0,165052 DC930 A U-15 0,092489 DC930 A U-35 0,131559 DC930 A U-50 0,155925 DC930 D 5 0,012098 0,4899 0,084985 DC930 D 15 0,010507 0,471774 0,092489 DC930 D INT 0,076701 DC930 D ZERO 0,068416 DC93LW A D-35 0,470211 0,135075 DC93LW A D-50 0,438965 0,165052 DC93LW A U-15 0,092489 DC93LW A U-35 0,131559 DC93LW A U-50 0,155925 DC93LW D 5 0,012098 0,4899 0,084985 DC93LW D 15 0,010507 0,471774 0,092489 DC93LW D INT 0,076701 DC93LW D ZERO 0,068416 DC950 A D-35 0,468147 0,135234 DC950 A D-50 0,442406 0,1600181.7.2015 EN Official Journal of the European Union L 168/163 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R DC950 A U-15 0,092489 DC950 A U-35 0,131677 DC950 A U-50 0,155399 DC950 D 5 0,012098 0,4899 0,084985 DC950 D 15 0,010507 0,471774 0,092489 DC950 D INTR 0,076701 DC950 D ZERO 0,068416 DC95HW A D-35 0,468147 0,135234 DC95HW A D-50 0,442406 0,160018 DC95HW A U-15 0,092489 DC95HW A U-35 0,131677 DC95HW A U-50 0,155399 DC95HW D 5 0,012098 0,4899 0,084985 DC95HW D 15 0,010507 0,471774 0,092489 DC95HW D INTR 0,076701 DC95HW D ZERO 0,068416 DC9Q7 A D-35 0,480101 0,134177 DC9Q7 A D-50 0,445486 0,157948 DC9Q7 A U-15 0,087963 DC9Q7 A U-35 0,130625 DC9Q7 A U-50 0,153365 DC9Q7 D 5 0,012996 0,49557 0,07757 DC9Q7 D 15 0,010618 0,477234 0,087963 DC9Q7 D INT 0,076753 DC9Q7 D ZERO 0,075935 DC9Q9 A D-35 0,470211 0,135075 DC9Q9 A D-50 0,438965 0,165052 DC9Q9 A U-15 0,092489 DC9Q9 A U-35 0,131559 DC9Q9 A U-50 0,155925 DC9Q9 D 5 0,012098 0,4899 0,084985 DC9Q9 D 15 0,010507 0,471774 0,092489 DC9Q9 D INT 0,076701L 168/164 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R DC9Q9 D ZERO 0,068416 DHC6 A D-INTR 0,125975 DHC6 A D-L 0,577068 0,176949 DHC6 D INTR 0,090222 DHC6 D TO 0,031032 0,787095 0,105443 DHC6 D ZERO 0,075 DHC6QP A D-INTR 0,125975 DHC6QP A D-L 0,577068 0,176949 DHC6QP D INTR 0,090222 DHC6QP D TO 0,031032 0,787095 0,105443 DHC6QP D ZERO 0,075 DHC7 A D-25 0,51353 0,127688 DHC7 A D-INTR 0,117133 DHC7 D 10 0,117133 DHC7 D 25 0,009556 0,466702 0,159266 DHC7 D ZERO 0,075 DHC8 A D-15 0,54969 0,092335 DHC8 A D-35 0,50961 0,10086 DHC8 A D-5 0,60123 0,087745 DHC8 A U-15 0,080204 DHC8 A U-5 0,073647 DHC8 D 5 0,017289 0,61342 0,07808 DHC8 D 15 0,017361 0,56668 0,08519 DHC8 D ZERO 0,072424 DHC830 A D-10 0,62986 0,091024 DHC830 A D-15 0,60123 0,094958 DHC830 A D-35 0,55542 0,103483 DHC830 A U-10 0,079221 DHC830 A U-15 0,084139 DHC830 D 5 0,017836 0,61764 0,070652 DHC830 D 10 0,015165 0,570532 0,076309 DHC830 D 15 0,014403 0,549595 0,080292 DHC830 D INT 0,019987 0,659514 0,0675721.7.2015 EN Official Journal of the European Union L 168/165 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R DHC830 D ZERO 0,068308 DO228 A F30APP 0,75885 0,11911 DO228 A ZERO-A 0,10717 DO228 D FLAPS1 0,02196 0,80401 0,09042 DO228 D ZERO 0,02745 0,86388 0,10717 DO228 D ZERO-C 0,14459 DO228 D ZERO-T 0,09218 DO328 A F32APP 0,638 0,0961 DO328 A ZERO-A 0,0916 DO328 D F12-D 0,016 0,666 0,0664 DO328 D ZERO 0,0916 DO328 D ZERO-C 0,1206 ECLIPSE500 A A_A_DN 1,273746 0,133462 ECLIPSE500 A A_T_DN 0,178304 ECLIPSE500 D TO_DN 0,100203 1,381422 0,105314 ECLIPSE500 D TO_UP 1,381422 0,086185 ECLIPSE500 D UP_DN 1,690947 0,103009 ECLIPSE500 D UP_UP 1,690947 0,073313 EMB120 A D-25 0,837 0,0801 EMB120 A D-45 0,782 0,1305 EMB120 D 15 0,0297 0,82 0,1014 EMB120 D ZERO 0,929 0,0834 EMB145 A D-22 0,6836 0,1291 EMB145 A D-45 0,6811 0,1809 EMB145 D 9 0,6503 0,0825 EMB145 D 9-GEAR 0,0218 0,6562 0,1048 EMB145 D ZERO 0,0691 EMB14L A D-22 0,6836 0,1291 EMB14L D 9 0,6503 0,083 EMB14L D 9-GEAR 0,0212 0,6562 0,083 EMB14L D D-45 0,6811 0,1809 EMB14L D ZERO 0,0694 EMB170 D 1 0,015720 0,579870 0,076830L 168/166 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R EMB170 A FULL 0,498900 0,145550 EMB170 D ZERO 0,066180 EMB175 D 1 0,015900 0,578990 0,077300 EMB175 A FULL 0,498200 0,145800 EMB175 D ZERO 0,066000 EMB190 D 1 0,012300 0,494610 0,082600 EMB190 A FULL 0,434400 0,137100 EMB190 D ZERO 0,066400 EMB195 D 1 0,012200 0,494520 0,083100 EMB195 A FULL 0,433600 0,137400 EMB195 D ZERO 0,067400 F10062 A D-42 0,4731 0,1565 F10062 A U-INT 0,1124 F10062 D INT2 0,0904 F10062 D TO 0,0122 0,5162 0,0683 F10062 D ZERO 0,0683 F10065 A D-42 0,4731 0,1565 F10065 A U-INT 0,1129 F10065 D INT2 0,0911 F10065 D TO 0,0123 0,521 0,0693 F10065 D ZERO 0,0693 F28MK2 A D-42 0,5334 0,1677 F28MK2 A U-INTR 0,1248 F28MK2 D 6 0,0171 0,6027 0,0793 F28MK2 D INT2 0,1033 F28MK2 D ZERO 0,0819 F28MK4 A D-42 0,5149 0,1619 F28MK4 A U-INTR 0,1187 F28MK4 D 6 0,01515 0,5731 0,0749 F28MK4 D INT2 0,0971 F28MK4 D ZERO 0,0755 FAL20 A D-25 0,804634 0,117238 FAL20 A D-40 0,792624 0,1363481.7.2015 EN Official Journal of the European Union L 168/167 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R FAL20 D 10 0,035696 0,807797 0,098781 FAL20 D INTR 0,084391 FAL20 D ZERO 0,07 GII A L-0-U 0,0751 GII A L-10-U 0,0852 GII D L-20-D 0,1138 GII D L-39-D 0,5822 0,1742 GII D T-0-U 0,0814 GII D T-10-U 0,0884 GII D T-20-D 0,02 0,634 0,1159 GIIB A L-0-U 0,0722 GIIB A L-10-U 0,0735 GIIB D L-20-D 0,1091 GIIB D L-39-D 0,562984 0,1509 GIIB D T-0-U 0,0738 GIIB D T-10-U 0,0729 GIIB D T-20-D 0,0162 0,583 0,1063 GIV A L-0-U 0,06 GIV A L-39-D 0,5805 0,1403 GIV D L-20-D 0,1063 GIV D T-0-U 0,0586 GIV D T-10-U 0,0666 GIV D T-20-D 0,0146 0,5798 0,1035 GIV D T-20-U 0,0797 GV A L-20-D 0,0974 GV A L-20-U 0,0749 GV A L-39-D 0,4908 0,1328 GV D L-0-U 0,0617 GV D T-0-U 0,058 GV D T-10-U 0,0606 GV D T-20-D 0,01178 0,516 0,0953 GV D T-20-U 0,0743 HS748A A D-30 0,45813 0,13849L 168/168 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R HS748A A D-INTR 0,106745 HS748A D INTR 0,088176 HS748A D TO 0,012271 0,542574 0,101351 HS748A D ZERO 0,075 IA1125 A D-40 0,967478 0,136393 IA1125 A D-INTR 0,118618 IA1125 D 12 0,040745 0,963488 0,100843 IA1125 D INTR 0,085422 IA1125 D ZERO 0,07 L1011 A D-33 0,286984 0,137671 L1011 A D-42 0,256389 0,155717 L1011 D 10 0,004561 0,265314 0,093396 L1011 D 22 0,004759 0,251916 0,105083 L1011 D INTR 0,07959 L1011 D ZERO 0,06243 L10115 A D-33 0,262728 0,140162 L10115 A D-42 0,256123 0,155644 L10115 D 10 0,004499 0,265314 0,093396 L10115 D 22 0,004695 0,251916 0,105083 L10115 D INTR 0,07959 L10115 D ZERO 0,06243 L188 A D-100 0,436792 0,174786 L188 A D-78-% 0,456156 0,122326 L188 D 39-% 0,009995 0,420533 0,142992 L188 D 78-% 0,010265 0,404302 0,159974 L188 D INTR 0,120987 L188 D ZERO 0,082 LEAR25 A D-40 1,28239 0,176632 LEAR25 A D-INTR 0,149986 LEAR25 D 10 0,09667 LEAR25 D 20 0,082866 1,27373 0,12334 LEAR25 D ZERO 0,07 LEAR35 A D-40 1,08756 0,1506881.7.2015 EN Official Journal of the European Union L 168/169 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R LEAR35 A D-INTR 0,129456 LEAR35 D 10 0,089112 LEAR35 D 20 0,043803 1,05985 0,108224 LEAR35 D ZERO 0,07 MD11GE D 10 0,003812 0,2648 0,0843 MD11GE D 15 0,003625 0,2578 0,0891 MD11GE D 20 0,003509 0,2524 0,0947 MD11GE D 25 0,003443 0,2481 0,1016 MD11GE D 0/EXT 0,0692 MD11GE D 0/RET 0,0551 MD11GE D ZERO 0,0551 MD11PW D 10 0,003829 0,265 0,08425 MD11PW D 15 0,003675 0,2576 0,08877 MD11PW D 20 0,003545 0,2526 0,09472 MD11PW D 25 0,003494 0,2487 0,1018 MD11PW D 0/EXT 0,0691 MD11PW D 0/RET 0,05512 MD11PW D ZERO 0,05512 MD81 D 11 0,009276 0,4247 0,07719 MD81 D INT1 0,07643 MD81 D INT2 0,06313 MD81 D INT3 0,06156 MD81 D INT4 0,06366 MD81 D T_15 0,009369 0,420798 0,0857 MD81 D T_INT 0,0701 MD81 D T_ZERO 0,061 MD81 D ZERO 0,06761 MD82 D 11 0,009248 0,4236 0,07969 MD82 D INT1 0,07625 MD82 D INT2 0,06337 MD82 D INT3 0,06196 MD82 D INT4 0,0634 MD82 D T_15 0,009267 0,420216 0,086L 168/170 EN Official Journal of the European Union 1.7.2015 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R MD82 D T_INT 0,065 MD82 D T_ZERO 0,061 MD82 D ZERO 0,06643 MD83 D 11 0,009301 0,4227 0,0798 MD83 D INT1 0,07666 MD83 D INT2 0,0664 MD83 D INT3 0,06247 MD83 D INT4 0,06236 MD83 D T_15 0,009384 0,420307 0,086 MD83 D T_INT 0,0664 MD83 D T_ZERO 0,0611 MD83 D ZERO 0,06573 MD9025 A D-28 0,4118 0,1181 MD9025 A D-40 0,4003 0,1412 MD9025 A U-0 0,4744 0,0876 MD9025 D EXT/06 0,010708 0,458611 0,070601 MD9025 D EXT/11 0,009927 0,441118 0,073655 MD9025 D EXT/18 0,009203 0,421346 0,083277 MD9025 D EXT/24 0,008712 0,408301 0,090279 MD9025 D RET/0 0,05186 MD9028 A D-28 0,4118 0,1181 MD9028 A D-40 0,4003 0,1412 MD9028 A U-0 0,4744 0,0876 MD9028 D EXT/06 0,010993 0,463088 0,070248 MD9028 D EXT/11 0,010269 0,446501 0,072708 MD9028 D EXT/18 0,009514 0,426673 0,082666 MD9028 D EXT/24 0,008991 0,413409 0,090018 MD9028 D RET/0 0,05025 MU3001 A D-30 1,07308 0,147487 MU3001 A D-INTR 0,114684 MU3001 D 1 0,065703 1,1529 0,08188 MU3001 D 10 0,055318 1,0729 0,09285 MU3001 D ZERO 0,071.7.2015 EN Official Journal of the European Union L 168/171 ACFT_ID OP_TYPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R PA30 A 27-A 1,316667 0,104586 PA30 A ZERO-A 0,078131 PA30 D 15-D 0,100146 1,166667 0,154071 PA30 D ZERO-D 0,067504 PA42 A 30-DN 1,09213 0,14679 PA42 A ZERO-A 0,087856 PA42 D ZER-DN 0,06796 1,011055 0,08088 PA42 D ZERO 0,087856 PA42 D ZERO-C 0,139096 PA42 D ZERO-T 0,07651 SD330 A D-15 0,746802 0,109263 SD330 A D-35 0,702872 0,143475 SD330 D 10 0,031762 0,727556 0,138193 SD330 D INTR 0,106596 SD330 D ZERO 0,075 SF340 A D-35 0,75674 0,147912 SF340 A D-INTR 0,111456 SF340 D 5 0,105831 SF340 D 15 0,026303 0,746174 0,136662 SF340 D ZERO 0,075Table I-2 Aircrafts Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID 1900D Beech 1900D/PT6A67 Turbo­ 2 Large Commercial 16 950 14 940 1 696 3 367 1 PT6A67 CNT (lb) 213 109 Prop prop 707 Boeing 707-120/JT3C Jet 4 Heavy Commercial 302 400 188 900 6 682 10 120 1 JT4A CNT (lb) 208 107 Wing 707120 Boeing 707-120B/JT3D-3 Jet 4 Heavy Commercial 302 400 188 900 6 893 14 850 1 JT3D CNT (lb) 208 107 Wing 707320 Boeing 707-320B/JT3D-7 Jet 4 Heavy Commercial 334 000 247 000 5 622 19 000 1 JT3D CNT (lb) 208 107 Wing 707QN Boeing 707-320B/JT3D- Jet 4 Heavy Commercial 334 000 247 000 5 622 19 000 2 JT3DQ CNT (lb) 208 106 Wing 7QN 717200 Boeing 717-200/BR 715 Jet 2 Large Commercial 121 000 110 000 4 600 18 000 3 BR715 CNT (lb) 203 105 Fuselage 720 Boeing 720/JT3C Jet 4 Large Commercial 223 500 155 600 4 871 10 120 1 JT4A CNT (lb) 208 107 Wing 720B Boeing 720B/JT3D-3 Jet 4 Large Commercial 234 000 175 000 5 717 18 000 1 JT3D CNT (lb) 208 107 Wing 727100 Boeing 727-100/JT8D-7 Jet 3 Large Commercial 169 500 142 500 4 867 14 000 1 3JT8D CNT (lb) 201 101 Fuselage 727200 Boeing 727-200/JT8D-7 Jet 3 Large Commercial 217 600 163 300 5 571 11 895 1 3JT8D CNT (lb) 201 101 Fuselage 727D15 Boeing 727-200/JT8D-15 Jet 3 Large Commercial 208 000 169 000 4 922 15 500 1 3JT8D CNT (lb) 201 101 Fuselage 727D17 Boeing 727-200/JT8D-17 Jet 3 Large Commercial 208 000 169 000 5 444 16 000 2 3JT8DQ CNT (lb) 201 101 Fuselage 727EM1 FEDX 727-100/JT8D-7 Jet 3 Large Commercial 169 500 142 500 4 867 14 000 3 3JT8E7 CNT (lb) 201 101 Fuselage L 168/172 EN Official Journal of the European Union 1.7.2015Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID 727EM2 FEDX 727-200/JT8D-15 Jet 3 Large Commercial 208 000 169 000 4 922 15 500 3 3JT8E5 CNT (lb) 201 101 Fuselage 727Q15 Boeing 727-200/JT8D- Jet 3 Large Commercial 208 000 169 000 4 922 15 500 2 3JT8DQ CNT (lb) 201 101 Fuselage 15QN 727Q7 Boeing 727-100/JT8D- Jet 3 Large Commercial 169 500 142 500 4 867 14 000 2 3JT8DQ CNT (lb) 201 101 Fuselage 7QN 727Q9 Boeing 727-200/JT8D-9 Jet 3 Large Commercial 191 000 160 000 5 444 14 500 2 3JT8DQ CNT (lb) 201 101 Fuselage 727QF UPS 727-100 22C 25C Jet 3 Large Commercial 169 000 142 500 4 448 15 380 3 TAY651 CNT (lb) 201 101 Fuselage 737 Boeing 737/JT8D-9 Jet 2 Large Commercial 109 000 98 000 3 900 14 500 1 2JT8DW CNT (lb) 201 101 Wing 737300 Boeing 737-300/CFM56- Jet 2 Large Commercial 135 000 114 000 4 580 20 000 3 CFM563 CNT (lb) 202 102 Wing 3B-1 7373B2 Boeing 737-300/CFM56- Jet 2 Large Commercial 139 500 114 000 4 580 22 000 3 CFM563 CNT (lb) 202 102 Wing 3B-2 737400 Boeing 737-400/CFM56- Jet 2 Large Commercial 150 000 124 000 5 062 23 500 3 CFM563 CNT (lb) 202 102 Wing 3C-1 737500 Boeing 737-500/CFM56- Jet 2 Large Commercial 133 500 111 000 4 551 20 000 3 CFM563 CNT (lb) 202 102 Wing 3C-1 737700 Boeing 737-700/CFM56- Jet 2 Large Commercial 154 500 129 200 4 445 24 000 3 CF567B CNT (lb) 203 104 Wing 7B24 737800 Boeing 737-800/CFM56- Jet 2 Large Commercial 174 200 146 300 5 435 26 300 3 CF567B CNT (lb) 203 104 Wing 7B26 737D17 Boeing 737-200/JT8D-17 Jet 2 Large Commercial 124 000 107 000 4 244 16 000 2 2JT8QW CNT (lb) 201 101 Wing 1.7.2015 EN Official Journal of the European Union L 168/173Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID 737N17 Boeing 737-200/JT8D-17 Jet 2 Large Commercial 124 000 107 000 4 244 16 000 3 2JT8DN CNT (lb) 202 104 Wing Nordam B737 LGW Hushkit 737N9 Boeing 737/JT8D-9 Nor­ Jet 2 Large Commercial 109 000 98 000 3 900 14 500 3 2JT8DN CNT (lb) 202 104 Wing dam B737 LGW Hushkit 737QN Boeing 737/JT8D-9QN Jet 2 Large Commercial 109 000 98 000 3 900 14 500 2 2JT8QW CNT (lb) 201 101 Wing 747100 Boeing 747-100/JT9DBD Jet 4 Heavy Commercial 733 000 516 600 5 727 33 042 2 JT9DBD CNT (lb) 209 107 Wing 74710Q Boeing 747-100/JT9D- Jet 4 Heavy Commercial 733 000 564 000 6 200 45 500 3 JT9DFL CNT (lb) 207 107 Wing 7QN 747200 Boeing 747-200/JT9D-7 Jet 4 Heavy Commercial 775 000 564 000 6 200 45 500 3 JT9DFL CNT (lb) 207 107 Wing 74720A Boeing 747-200/JT9D- Jet 4 Heavy Commercial 785 000 564 000 6 200 46 300 3 JT9D7Q CNT (lb) 207 107 Wing 7A 74720B Boeing 747-200/JT9D- Jet 4 Heavy Commercial 800 000 630 000 6 200 53 000 3 JT9D7Q CNT (lb) 207 107 Wing 7Q 747400 Boeing 747-400/ Jet 4 Heavy Commercial 875 000 652 000 6 989 56 800 3 PW4056 CNT (lb) 207 107 Wing PW4056 7478 Boeing 747-8F/GEnx- Jet 4 Heavy Commercial 987 000 757 000 7 900 68 000 4 GENX67 CNT (lb) 205 107 Wing 2B67 747SP Boeing 747SP/JT9D-7 Jet 4 Heavy Commercial 702 000 475 000 5 911 45 500 3 JT9DFL CNT (lb) 207 107 Wing 757300 Boeing 757-300/RB211- Jet 2 Large Commercial 275 000 224 000 5 651 43 100 3 RR535E CNT (lb) 203 103 Wing 535E4B 757PW Boeing 757-200/ Jet 2 Large Commercial 255 000 210 000 4 790 38 300 3 PW2037 CNT (lb) 203 103 Wing PW2037 L 168/174 EN Official Journal of the European Union 1.7.2015Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID 757RR Boeing 757-200/RB211- Jet 2 Large Commercial 255 000 210 000 4 640 40 100 3 RR535E CNT (lb) 203 103 Wing 535E4 767300 Boeing 767-300/ Jet 2 Heavy Commercial 407 000 320 000 4 710 60 000 3 2CF680 CNT (lb) 203 103 Wing PW4060 767400 Boeing 767-400ER/CF6- Jet 2 Heavy Commercial 450 000 340 000 6 000 58 685 3 CF680C CNT (lb) 205 102 Wing 80C2B(F) 767CF6 Boeing 767-200/CF6- Jet 2 Heavy Commercial 315 500 270 000 4 700 48 000 3 2CF680 CNT (lb) 203 103 Wing 80A 767JT9 Boeing 767-200/JT9D- Jet 2 Heavy Commercial 351 000 270 000 4 744 48 000 3 2CF680 CNT (lb) 203 103 Wing 7R4D 777200 Boeing 777-200/GE90- Jet 2 Heavy Commercial 656 000 470 000 4 450 90 000 3 GE90 CNT (lb) 205 105 Wing 76B 777300 Boeing 777-300/Trent Jet 2 Heavy Commercial 660 000 524 000 6 012 77 000 0 TRENT8 CNT (lb) 203 105 Wing 892 7773ER Boeing 777-300ER/ Jet 2 Heavy Commercial 775 000 554 000 5 805 115 000 3 GE9015 CNT (lb) 204 107 Wing GE90-115B-EIS 7878R Boeing 787-8/T1000-C/ Jet 2 Heavy Commercial 502 500 380 000 5 090 70 000 4 T1KBFP CNT (lb) 205 103 Wing 01 Family Plan Cert A300- Airbus A300-622R/ Jet 2 Heavy Commercial 378 533 308 647 4 735 58 000 3 PW4158 CNT (lb) 202 103 Wing 622R PW4158 A300B4- Airbus A300B4-200/ Jet 2 Heavy Commercial 364 000 295 000 5 367 52 500 3 2CF650 CNT (lb) 203 103 Wing 203 CF6-50C2 A310-304 Airbus A310-304/GE Jet 2 Heavy Commercial 346 126 273 373 4 682 53 500 3 A310 CNT (lb) 204 103 Wing CF6-80C2A2 A319-131 Airbus A319-131/ Jet 2 Large Commercial 166 449 137 789 4 364 22 000 3 V2522A CNT (lb) 205 103 Wing V2522-A5 1.7.2015 EN Official Journal of the European Union L 168/175Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID A320-211 Airbus A320-211/ Jet 2 Large Commercial 169 756 142 198 4 753 25 000 3 CFM565 CNT (lb) 202 103 Wing CFM56-5A1 A320-232 Airbus A320-232/ Jet 2 Large Commercial 169 756 145 505 4 917 26 500 3 V2527A CNT (lb) 205 103 Wing V2527-A5 A321-232 Airbus A321-232/IAE Jet 2 Large Commercial 196 211 166 449 5 587 30 000 3 V2530 CNT (lb) 202 103 Wing V2530-A5 A330-301 Airbus A330-301/GE Jet 2 Heavy Commercial 478 400 383 604 5 966 67 500 3 CF680E CNT (lb) 202 102 Wing CF6-80 E1A2 A330-343 Airbus A330-343/RR Jet 2 Heavy Commercial 513 677 412 264 5 512 71 100 3 TRENT7 CNT (lb) 205 102 Wing Trent 772B A340-211 Airbus A340-211/ Jet 4 Heavy Commercial 573 200 399 036 5 900 31 200 3 CF565C CNT (lb) 206 107 Wing CFM56-5C2 A340-642 Airbus A340-642/RR Jet 4 Heavy Commercial 804 687 564 383 6 919 56 000 4 TRENT5 CNT (lb) 205 102 Wing Trent 556 A380-841 Airbus A380-841/RR Jet 4 Heavy Commercial 1 254 430 862 007 6 752 70 000 4 TRENT9 CNT (lb) 205 105 Wing Trent 970 A380-861 Airbus A380-861/EA Jet 4 Heavy Commercial 1 254 430 862 007 6 837 70 000 4 GP7270 CNT (lb) 206 105 Wing GP7270 BAC111 BAC 111/SPEY MK511- Jet 2 Large Commercial 89 600 82 000 4 449 11 400 2 2JT8D CNT (lb) 201 101 Fuselage 14 BAE146 BAe 146-200/ALF502R- Jet 4 Large Commercial 93 000 81 000 3 770 6 970 3 AL502R CNT (lb) 206 108 Wing 5 BAE300 BAe 146-300/ALF502R- Jet 4 Large Commercial 97 500 84 500 3 960 6 970 3 AL502R CNT (lb) 206 108 Wing 5 BEC58P Raytheon BARON 58P/ Piston 2 Small General Avia­ 6 100 6 100 2 733 779 0 TSIO52 CNT (% of 215 109 Prop TS10-520-L tion Max Static Thrust) L 168/176 EN Official Journal of the European Union 1.7.2015Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID CIT3 Cessna Citation III/ Jet 2 Large General Avia­ 20 000 17 000 2 770 3 650 3 TF7313 CNT (lb) 216 113 Fuselage TFE731-3-100S tion CL600 Canadair CL-600/ Jet 2 Large General Avia­ 36 000 33 000 3 300 7 500 3 AL502L CNT (lb) 216 113 Fuselage ALF502L tion CL601 Canadair CL-601/CF34- Jet 2 Large General Avia­ 43 100 36 000 3 550 9 220 3 CF34 CNT (lb) 216 113 Fuselage 3A tion CNA172 Cessna 172R/Lycoming Piston 1 Small General Avia­ 2 450 2 450 1 695 436 0 IO360L CNT (% of 215 109 Prop IO-360-L2A tion Max Static Thrust) CNA182 Cessna 182H/Continental Piston 1 Small General Avia­ 2 800 2 800 1 544 965 2 O470R CNT (lb) 215 113 Prop O-470-R tion CNA206 Cessna 206H/Lycoming Piston 1 Small General Avia­ 3 600 3 600 1 880 798 0 IO540 Other 215 109 Prop IO-540-AC tion (RPM) CNA208 Cessna 208/PT6A-114 Turbo­ 1 Small General Avia­ 8 750 8 500 1 740 2 300 3 PT6­ CNT (lb) 210 109 Prop prop tion A114 CNA20T Cessna T206H/Lycoming Piston 1 Small General Avia­ 3 600 3 600 1 880 825 0 TIO540 Other 215 109 Prop TIO-540-AJ1A tion (RPM) CNA441 Cessna CONQUEST II Turbo­ 2 Small Commercial 9 900 9 400 1 939 1 535 0 TPE331 CNT (% of 210 111 Prop /TPE331-8 prop Max Static Thrust) CNA500 Cessna Citation II/JT15D- Jet 2 Large General Avia­ 14 700 14 000 3 050 2 500 3 JT15D1 CNT (lb) 216 113 Fuselage 4 tion CNA510 Cessna Mustang Model Jet 2 Small Commercial 8 645 7 200 3 010 1 466 0 PW615F CNT (lb) 203 113 Fuselage 510/PW615F CNA525C Cessna Citation Jet 2 Small Commercial 16 950 15 500 3 010 3 600 4 FJ44-4 CNT (lb) 235 136 Fuselage CJ4 525C /FJ44-4A 1.7.2015 EN Official Journal of the European Union L 168/177Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID CNA55B Cessna 550 Citation Jet 2 Large General Avia­ 14 800 13 500 3 010 2 863 0 PW530A CNT (lb) 203 113 Fuselage Bravo/PW530A tion CNA560E Cessna Citation Encore Jet 2 Small Commercial 16 300 13 680 3 000 3 313 3 2PW535 CNT (lb) 238 138 Fuselage 560/PW535A CNA560U Cessna Citation Ultra Jet 2 Small Commercial 16 300 13 680 2 700 3 029 3 2J155D CNT (lb) 237 113 Fuselage 560/JT15D-5D CNA560XL Cessna Citation Excel Jet 2 Small Commercial 20 000 16 830 3 000 3 824 3 PW545A CNT (lb) 238 137 Fuselage 560/PW545A CNA680 Cessna Citation Sovereign Jet 2 Small Commercial 30 000 24 390 3 010 5 749 3 PW306C CNT (lb) 236 136 Fuselage 680/PW306C CNA750 Cessna Citation X/Rolls Jet 2 Large General Avia­ 35 700 31 800 3 500 6 407 3 AE300C CNT (lb) 202 105 Fuselage Royce Allison AE3007C tion CONCRD Concorde/OLY593 Jet 4 Heavy Commercial 400 000 245 000 10 600 38 100 0 OLY593 CNT (lb) 206 106 Wing CRJ9-ER Bombardier CL-600- Jet 2 Large Commercial 82 500 73 500 5 779 13 525 3 CF348­ CNT (lb) 216 113 Fuselage 2D15/CL-600-2D24/ C5 CF34-8C5 CRJ9-LR Bombardier CL-600- Jet 2 Large Commercial 84 500 75 100 5 680 13 525 3 CF348­ CNT (lb) 216 113 Fuselage 2D15/CL-600-2D24/ C5 CF34-8C5 CVR580 Convair CV-580/ALL Turbo­ 2 Large Commercial 58 000 52 000 4 256 8 100 0 501D13 CNT (% of 214 112 Prop 501-D15 prop Max Static Thrust) DC1010 McDonnell Douglas Jet 3 Heavy Commercial 455 000 363 000 5 820 40 000 3 CF66D CNT (lb) 203 101 Wing DC10-10/CF6-6D DC1030 McDonnell Douglas Jet 3 Heavy Commercial 572 000 403 000 5 418 53 200 3 CF66D CNT (lb) 203 101 Wing DC10-30/CF6-50C2 L 168/178 EN Official Journal of the European Union 1.7.2015Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID DC1040 McDonnell Douglas Jet 3 Heavy Commercial 555 000 403 000 6 020 49 400 3 CF66D CNT (lb) 203 101 Wing DC10-40/JT9D-20 DC3 Douglas DC-3/R1820-86 Piston 2 Large Commercial 28 000 24 500 2 222 3 120 0 2R2800 CNT (% of 213 110 Prop Max Static Thrust) DC6 Douglas DC-6/R2800- Piston 4 Large Commercial 106 000 95 000 3 010 4 180 0 4R2800 CNT (% of 213 110 Prop CB17 Max Static Thrust) DC820 Douglas DC-8-20/JT4A Jet 4 Heavy Commercial 317 600 194 400 6 527 11 850 1 JT4A CNT (lb) 208 107 Wing DC850 Douglas DC-8-50/JT3D- Jet 4 Heavy Commercial 325 000 240 000 5 400 18 000 1 JT3D CNT (lb) 208 107 Wing 3B DC860 Douglas DC-8-60/JT3D-7 Jet 4 Heavy Commercial 355 000 275 000 5 310 19 000 1 JT3D CNT (lb) 208 107 Wing DC870 Douglas DC-8-70/ Jet 4 Heavy Commercial 355 000 258 000 6 500 22 000 3 CFM562 CNT (lb) 206 106 Wing CFM56-2C-5 DC8QN Douglas DC-8-60/JT8D- Jet 4 Heavy Commercial 355 000 275 000 5 310 19 000 2 JT3DQ CNT (lb) 208 106 Wing 7QN DC910 McDonnell Douglas DC- Jet 2 Large Commercial 90 700 81 700 5 030 14 000 1 2JT8D CNT (lb) 201 101 Fuselage 9-10/JT8D-7 DC930 McDonnell Douglas DC- Jet 2 Large Commercial 114 000 102 000 4 680 14 500 1 2JT8D CNT (lb) 201 101 Fuselage 9-30/JT8D-9 DC93LW McDonnell Douglas DC- Jet 2 Large Commercial 114 000 102 000 4 680 14 500 3 2JT8DL CNT (lb) 201 101 Fuselage 9-30/JT8D-9 w/ ABS Lightweight hushkit DC950 McDonnell Douglas DC- Jet 2 Large Commercial 121 000 110 000 4 880 16 000 2 2JT8DQ CNT (lb) 201 101 Fuselage 9-50/JT8D-17 1.7.2015 EN Official Journal of the European Union L 168/179Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID DC95HW McDonnell Douglas DC- Jet 2 Large Commercial 121 000 110 000 4 880 16 000 3 2JT8DH CNT (lb) 201 101 Fuselage 9-50/JT8D17 w/ ABS Heavyweight hushkit DC9Q7 McDonnell Douglas DC- Jet 2 Large Commercial 90 700 81 700 5 030 14 000 2 2JT8DQ CNT (lb) 201 101 Fuselage 9-10/JT8D-7QN DC9Q9 McDonnell Douglas DC- Jet 2 Large Commercial 114 000 102 000 4 680 14 500 2 2JT8DQ CNT (lb) 201 101 Fuselage 9-30/JT8D-9QN DHC6 De Havilland DASH 6/ Turbo­ 2 Small Commercial 12 500 12 300 1 500 2 000 0 PT6A27 CNT (% of 210 109 Prop PT6A-27 prop Max Static Thrust) DHC6QP De Havilland DASH 6/ Turbo­ 2 Small Commercial 12 500 12 300 1 500 2 000 0 RAISQP CNT (% of 210 109 Prop PT6A-27 Raisbeck Quiet prop Max Static PropMod Thrust) DHC7 De Havilland DASH 7/ Turbo­ 4 Large Commercial 41 000 39 000 2 150 2 850 3 PT6A50 CNT (% of 213 112 Prop PT6A-50 prop Max Static Thrust) DHC8 Bombardier de Havilland Turbo­ 2 Large Commercial 34 500 33 900 3 000 4 750 3 PW120 CNT (% of 213 112 Prop DASH 8-100/PW121 prop Max Static Thrust) DHC830 Bombardier de Havilland Turbo­ 2 Large Commercial 43 000 42 000 3 500 4 918 3 PW120 CNT (% of 213 112 Prop DASH 8-300/PW123 prop Max Static Thrust) DO228 Dornier 228-202/TPE Turbo­ 2 Large Commercial 13 669 13 448 2 375 2 240 3 TPE331- CNT (lb) 216 110 Prop 311-5 prop 5 DO328 Dornier 328-100/ Turbo­ 2 Large Commercial 30 843 29 167 3 825 6 745 3 PW119C CNT (lb) 214 109 Prop PW119C prop L 168/180 EN Official Journal of the European Union 1.7.2015Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID ECLIPS­ Eclipse 500/PW610F Jet 2 Small General Avia­ 6 000 5 600 2 389 1 031 3 PW610F CNT (lb) 201 103 Fuselage E500 tion EMB120 Embraer 120 ER/Pratt & Turbo­ 2 Large Commercial 26 433 25 794 5 571 4 000 3 EPW118 CNT (lb) 213 109 Prop Whitney PW118 prop EMB145 Embraer 145 ER/Allison Jet 2 Large Commercial 45 420 41 230 4 232 7 500 3 AE3007 CNT (lb) 216 113 Fuselage AE3007 EMB14L Embraer 145 LR/Allison Jet 2 Large Commercial 48 500 42 550 4 232 7 500 3 AE3007 CNT (lb) 216 113 Fuselage AE3007A1 EMB170 Embraer ERJ170-100 Jet 2 Large Commercial 82 012 72 312 4 029 13 800 3 CF348E CNT (lb) 216 113 Wing EMB175 Embraer ERJ170-200 Jet 2 Large Commercial 85 517 74 957 4 130 13 800 3 CF348E CNT (lb) 216 113 Wing EMB190 Embraer ERJ190-100 Jet 2 Large Commercial 114 199 97 003 4 081 18 500 3 CF3410E CNT (lb) 205 105 Wing EMB195 Embraer ERJ190-200 Jet 2 Large Commercial 115 280 100 972 4 183 18 500 3 CF3410E CNT (lb) 205 105 Wing F10062 Fokker 100/TAY 620-15 Jet 2 Large Commercial 95 000 85 500 4 560 13 900 3 TAY620 CNT (lb) 201 101 Fuselage F10065 Fokker 100/TAY 650-15 Jet 2 Large Commercial 98 000 88 000 4 704 15 100 3 TAY650 CNT (lb) 201 101 Fuselage F28MK2 Fokker F-28-2000/ Jet 2 Large Commercial 65 000 59 000 3 540 9 850 2 RB183 CNT (lb) 216 104 Fuselage RB183MK555 F28MK4 Fokker F-28-4000/ Jet 2 Large Commercial 73 000 64 000 3 546 9 900 2 RB183P CNT (lb) 216 104 Fuselage RB183MK555 FAL20 Dassault FALCON 20/ Jet 2 Large General Avia­ 28 700 27 300 2 490 4 500 2 CF700 CNT (lb) 203 113 Fuselage CF700-2D-2 tion 1.7.2015 EN Official Journal of the European Union L 168/181Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID GII Gulfstream GII/SPEY Jet 2 Large General Avia­ 64 800 58 500 3 200 11 400 2 SPEYHK CNT (lb) 216 104 Fuselage 511-8 tion GIIB Gulfstream GIIB/GIII — Jet 2 Large General Avia­ 69 700 58 500 3 250 11 400 2 SPEYHK CNT (lb) 216 104 Fuselage SPEY 511-8 tion GIV Gulfstream GIV-SP/TAY Jet 2 Large General Avia­ 74 600 66 000 3 190 13 850 3 TAYGIV CNT (lb) 203 113 Fuselage 611-8 tion GV Gulfstream GV/BR 710 Jet 2 Large General Avia­ 90 500 75 300 2 760 14 750 3 BR710 CNT (lb) 205 105 Fuselage tion HS748A Hawker Siddeley HS-748/ Turbo­ 2 Large Commercial 46 500 43 000 3 360 5 150 2 RDA532 CNT (% of 212 110 Prop DART MK532-2 prop Max Static Thrust) IA1125 IAI-1125 ASTRA/ Jet 2 Large General Avia­ 23 500 20 700 3 689 3 700 3 TF7313 CNT (lb) 216 113 Fuselage TFE731-3A tion L1011 Lockheed Martin L-1011/ Jet 3 Heavy Commercial 430 000 358 000 5 693 42 000 3 RB2112 CNT (lb) 203 101 Wing RB211-22B L10115 Lockheed Martin L-1011- Jet 3 Heavy Commercial 510 000 368 000 6 800 50 000 3 RB2112 CNT (lb) 203 101 Wing 500/RB211-224B L188 Lockheed L-188C/ALL Turbo­ 4 Large Commercial 116 000 98 100 4 960 8 000 0 T56A7 CNT (% of 214 112 Prop 501-D13 prop Max Static Thrust) LEAR25 Learjet 25/CJ610-8 Jet 2 Large General Avia­ 15 000 13 500 2 620 2 950 2 CJ610 CNT (lb) 202 113 Fuselage tion LEAR35 Learjet 36/TFE731-2 Jet 2 Large General Avia­ 18 300 15 300 3 076 3 500 3 TF7312 CNT (lb) 216 113 Fuselage tion MD11GE McDonnell Douglas MD- Jet 3 Heavy Commercial 682 400 433 300 5 131 61 500 3 2CF68D CNT (lb) 203 103 Wing 11/CF6-80C2D1F MD11PW McDonnell Douglas MD- Jet 3 Heavy Commercial 682 400 433 300 4 681 60 000 3 PW4460 CNT (lb) 203 103 Wing 11/PW 4460 L 168/182 EN Official Journal of the European Union 1.7.2015Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID MD81 McDonnell Douglas MD- Jet 2 Large Commercial 140 000 128 000 4 860 19 300 3 2JT8D2 CNT (lb) 204 104 Fuselage 81/JT8D-209 MD82 McDonnell Douglas MD- Jet 2 Large Commercial 149 500 130 000 4 920 20 900 3 2JT8D2 CNT (lb) 204 104 Fuselage 82/JT8D-217A MD83 McDonnell Douglas MD- Jet 2 Large Commercial 160 000 139 500 5 200 21 700 3 2JT8D2 CNT (lb) 204 104 Fuselage 83/JT8D-219 MD9025 McDonnell Douglas MD- Jet 2 Large Commercial 156 000 142 000 3 000 25 000 3 V2525 CNT (lb) 205 105 Fuselage 90/V2525-D5 MD9028 McDonnell Douglas MD- Jet 2 Large Commercial 156 000 142 000 3 000 28 000 3 V2525 CNT (lb) 205 105 Fuselage 90/V2528-D5 MU3001 Mitsubishi MU300-10 Jet 2 Large General Avia­ 14 100 13 200 2 800 2 500 3 JT15D5 CNT (lb) 203 113 Fuselage Diamond II/JT15D-5 tion PA28 Piper Warrior PA-28- Piston 1 Small General Avia­ 2 325 2 325 1 695 400 0 O320D3 Other 213 113 Prop 161/O-320-D3G tion (RPM) PA30 Piper Twin Comanche Piston 2 Small General Avia­ 3 600 3 600 1 654 777 0 IO320B CNT (lb) 213 113 Prop PA-30/IO-320-B1A tion PA31 Piper Navajo Chieftain Piston 2 Small General Avia­ 7 000 7 000 1 850 1 481 0 TIO542 Other 213 109 Prop PA-31-350/TIO-5 tion (RPM) PA42 Piper PA-42/PT6A-41 Turbo­ 2 Small General Avia­ 11 200 10 330 3 300 1 800 3 PT6A41 CNT (lb) 213 109 Prop prop tion SABR80 NA Sabreliner 80 Jet 2 Large General Avia­ 33 720 27 290 2 490 3 962 2 CF700 CNT (lb) 203 113 Fuselage tion SD330 Short SD3-30/PT6A- Turbo­ 2 Large Commercial 22 900 22 600 3 650 2 670 3 PT6A45 CNT (% of 211 109 Prop 45AR prop Max Static Thrust) SF340 Saab SF340B/CT7-9B Turbo­ 2 Large Commercial 27 300 26 500 3 470 4 067 3 CT75 CNT (% of 211 110 Prop prop Max Static Thrust) 1.7.2015 EN Official Journal of the European Union L 168/183L 168/184 EN Official Journal of the European Union 1.7.2015 Table I-3 Default approach procedural steps Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 1900D DEFAULT 1 Descend ZERO-A 6 000,0 160,0 3,0 1900D DEFAULT 2 Descend ZERO-A 3 000,0 160,0 3,0 1900D DEFAULT 3 Descend ZERO-A 1 500,0 146,0 3,0 1900D DEFAULT 4 Descend 35-A 1 000,0 118,0 3,0 1900D DEFAULT 5 Land 35-A 57,2 1900D DEFAULT 6 Decelerate 84,0 515,2 40,0 1900D DEFAULT 7 Decelerate 10,0 0,0 10,0 707320 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 707320 DEFAULT 2 Descend 14 3 000,0 160,0 3,0 707320 DEFAULT 3 Descend D-25 1 500,0 145,0 3,0 707320 DEFAULT 4 Descend D-40 1 000,0 131,6 3,0 707320 DEFAULT 5 Land D-40 410,6 707320 DEFAULT 6 Decelerate 124,9 3 695,4 40,0 707320 DEFAULT 7 Decelerate 30,0 0,0 10,0 707QN DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 707QN DEFAULT 2 Descend 14 3 000,0 160,0 3,0 707QN DEFAULT 3 Descend D-25 1 500,0 145,0 3,0 707QN DEFAULT 4 Descend D-40 1 000,0 131,6 3,0 707QN DEFAULT 5 Land D-40 410,6 707QN DEFAULT 6 Decelerate 124,9 3 695,4 40,0 707QN DEFAULT 7 Decelerate 30,0 0,0 10,0 717200 DEFAULT 1 Descend A_0U 6 000,0 250,0 3,01.7.2015 EN Official Journal of the European Union L 168/185 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 717200 DEFAULT 2 Descend A_18U 3 000,0 190,0 3,0 717200 DEFAULT 3 Descend A_18D 1 500,0 160,0 3,0 717200 DEFAULT 4 Descend A_40D 1 000,0 140,0 3,0 717200 DEFAULT 5 Land A_40D 318,6 717200 DEFAULT 6 Decelerate 130,0 2 867,4 40,0 717200 DEFAULT 7 Decelerate 30,0 0,0 8,6 720B DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 720B DEFAULT 2 Descend 20 3 000,0 160,0 3,0 720B DEFAULT 3 Descend U-30 1 500,0 149,0 3,0 720B DEFAULT 4 Descend D-30 1 000,0 139,0 3,0 720B DEFAULT 5 Land D-30 419,1 720B DEFAULT 6 Decelerate 131,9 3 771,9 40,0 720B DEFAULT 7 Decelerate 30,0 0,0 10,0 727100 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 727100 DEFAULT 2 Descend 5 3 000,0 160,0 3,0 727100 DEFAULT 3 Descend D-25 1 500,0 125,5 3,0 727100 DEFAULT 4 Descend D-30 1 000,0 123,2 3,0 727100 DEFAULT 5 Land D-30 342,6 727100 DEFAULT 6 Decelerate 116,8 3 083,4 40,0 727100 DEFAULT 7 Decelerate 30,0 0,0 10,0 727D15 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 727D15 DEFAULT 2 Descend 5 3 000,0 160,0 3,0L 168/186 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 727D15 DEFAULT 3 Descend D-25 1 500,0 149,6 3,0 727D15 DEFAULT 4 Descend D-30 1 000,0 147,6 3,0 727D15 DEFAULT 5 Land D-30 347,6 727D15 DEFAULT 6 Decelerate 140,0 3 128,4 40,0 727D15 DEFAULT 7 Decelerate 30,0 0,0 10,0 727D17 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 727D17 DEFAULT 2 Descend 5 3 000,0 160,0 3,0 727D17 DEFAULT 3 Descend D-25 1 500,0 149,6 3,0 727D17 DEFAULT 4 Descend D-30 1 000,0 147,6 3,0 727D17 DEFAULT 5 Land D-30 394,6 727D17 DEFAULT 6 Decelerate 140,0 3 551,4 40,0 727D17 DEFAULT 7 Decelerate 30,0 0,0 10,0 727EM1 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 727EM1 DEFAULT 2 Descend 5 3 000,0 160,0 3,0 727EM1 DEFAULT 3 Descend D-25 1 500,0 125,5 3,0 727EM1 DEFAULT 4 Descend D-30 1 000,0 123,2 3,0 727EM1 DEFAULT 5 Land D-30 342,6 727EM1 DEFAULT 6 Decelerate 116,8 3 083,4 40,0 727EM1 DEFAULT 7 Decelerate 30,0 0,0 10,0 727EM2 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 727EM2 DEFAULT 2 Descend 5 3 000,0 160,0 3,0 727EM2 DEFAULT 3 Descend D-25 1 500,0 149,6 3,01.7.2015 EN Official Journal of the European Union L 168/187 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 727EM2 DEFAULT 4 Descend D-30 1 000,0 147,6 3,0 727EM2 DEFAULT 5 Land D-30 347,6 727EM2 DEFAULT 6 Decelerate 140,0 3 128,4 40,0 727EM2 DEFAULT 7 Decelerate 30,0 0,0 10,0 727Q15 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 727Q15 DEFAULT 2 Descend 5 3 000,0 160,0 3,0 727Q15 DEFAULT 3 Descend D-25 1 500,0 149,6 3,0 727Q15 DEFAULT 4 Descend D-30 1 000,0 147,6 3,0 727Q15 DEFAULT 5 Land D-30 347,6 727Q15 DEFAULT 6 Decelerate 140,0 3 128,4 40,0 727Q15 DEFAULT 7 Decelerate 30,0 0,0 10,0 727Q7 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 727Q7 DEFAULT 2 Descend 5 3 000,0 160,0 3,0 727Q7 DEFAULT 3 Descend D-25 1 500,0 125,5 3,0 727Q7 DEFAULT 4 Descend D-30 1 000,0 123,2 3,0 727Q7 DEFAULT 5 Land D-30 342,6 727Q7 DEFAULT 6 Decelerate 116,8 3 083,4 40,0 727Q7 DEFAULT 7 Decelerate 30,0 0,0 10,0 727Q9 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 727Q9 DEFAULT 2 Descend 5 3 000,0 160,0 3,0 727Q9 DEFAULT 3 Descend D-25 1 500,0 145,4 3,0 727Q9 DEFAULT 4 Descend D-30 1 000,0 143,4 3,0L 168/188 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 727Q9 DEFAULT 5 Land D-30 394,6 727Q9 DEFAULT 6 Decelerate 136,0 3 551,4 40,0 727Q9 DEFAULT 7 Decelerate 30,0 0,0 10,0 727QF DEFAULT 1 Descend U-ZERO 6 000,0 250,0 3,0 727QF DEFAULT 2 Descend U-05 3 000,0 160,0 3,0 727QF DEFAULT 3 Descend D-15 1 500,0 150,0 3,0 727QF DEFAULT 4 Descend D-30 1 000,0 131,0 3,0 727QF DEFAULT 5 Land D-30 363,0 727QF DEFAULT 6 Decelerate 121,0 2 686,0 40,0 727QF DEFAULT 7 Decelerate 60,0 0,0 10,0 737 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 737 DEFAULT 2 Descend 5 3 000,0 170,0 3,0 737 DEFAULT 3 Descend D-25 1 500,0 134,5 3,0 737 DEFAULT 4 Descend D-30 1 000,0 131,5 3,0 737 DEFAULT 5 Land D-30 255,6 737 DEFAULT 6 Decelerate 124,8 2 300,4 40,0 737 DEFAULT 7 Decelerate 30,0 0,0 10,0 737300 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 737300 DEFAULT 2 Descend 5 3 000,0 170,0 3,0 737300 DEFAULT 3 Descend D-15 1 500,0 148,6 3,0 737300 DEFAULT 4 Descend D-30 1 000,0 139,0 3,0 737300 DEFAULT 5 Land D-30 316,81.7.2015 EN Official Journal of the European Union L 168/189 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 737300 DEFAULT 6 Decelerate 131,9 2 851,2 40,0 737300 DEFAULT 7 Decelerate 30,0 0,0 10,0 7373B2 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 7373B2 DEFAULT 2 Descend 5 3 000,0 170,0 3,0 7373B2 DEFAULT 3 Descend D-15 1 500,0 148,6 3,0 7373B2 DEFAULT 4 Descend D-30 1 000,0 139,0 3,0 7373B2 DEFAULT 5 Land D-30 316,8 7373B2 DEFAULT 6 Decelerate 131,9 2 851,2 40,0 7373B2 DEFAULT 7 Decelerate 30,0 0,0 10,0 737400 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 737400 DEFAULT 2 Descend 5 3 000,0 170,0 3,0 737400 DEFAULT 3 Descend D-15 1 500,0 159,7 3,0 737400 DEFAULT 4 Descend D-30 1 000,0 144,9 3,0 737400 DEFAULT 5 Land D-30 360,2 737400 DEFAULT 6 Decelerate 137,5 3 241,8 40,0 737400 DEFAULT 7 Decelerate 30,0 0,0 10,0 737500 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 737500 DEFAULT 2 Descend 5 3 000,0 170,0 3,0 737500 DEFAULT 3 Descend D-15 1 500,0 143,4 3,0 737500 DEFAULT 4 Descend D-30 1 000,0 135,3 3,0 737500 DEFAULT 5 Land D-30 314,2 737500 DEFAULT 6 Decelerate 128,4 2 827,8 40,0L 168/190 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 737500 DEFAULT 7 Decelerate 30,0 0,0 10,0 737700 DEFAULT 1 Descend T_ZERO 6 000,0 250,0 3,0 737700 DEFAULT 2 Descend T_5 3 000,0 171,0 3,0 737700 DEFAULT 3 Descend A_15 1 500,0 140,0 3,0 737700 DEFAULT 4 Descend A_40 1 000,0 133,0 3,0 737700 DEFAULT 5 Land A_40 304,7 737700 DEFAULT 6 Decelerate 116,0 2 741,9 40,0 737700 DEFAULT 7 Decelerate 30,0 0,0 10,0 737D17 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 737D17 DEFAULT 2 Descend 5 3 000,0 170,0 3,0 737D17 DEFAULT 3 Descend D-25 1 500,0 140,2 3,0 737D17 DEFAULT 4 Descend D-30 1 000,0 137,7 3,0 737D17 DEFAULT 5 Land D-30 286,6 737D17 DEFAULT 6 Decelerate 130,7 2 579,4 40,0 737D17 DEFAULT 7 Decelerate 30,0 0,0 10,0 737N17 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 737N17 DEFAULT 2 Descend 5 3 000,0 170,0 3,0 737N17 DEFAULT 3 Descend D-25 1 500,0 140,2 3,0 737N17 DEFAULT 4 Descend D-30 1 000,0 137,7 3,0 737N17 DEFAULT 5 Land D-30 286,6 737N17 DEFAULT 6 Decelerate 130,7 2 579,4 40,0 737N17 DEFAULT 7 Decelerate 30,0 0,0 10,01.7.2015 EN Official Journal of the European Union L 168/191 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 737N9 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 737N9 DEFAULT 2 Descend 5 3 000,0 170,0 3,0 737N9 DEFAULT 3 Descend D-25 1 500,0 134,5 3,0 737N9 DEFAULT 4 Descend D-30 1 000,0 131,5 3,0 737N9 DEFAULT 5 Land D-30 255,6 737N9 DEFAULT 6 Decelerate 124,8 2 300,4 40,0 737N9 DEFAULT 7 Decelerate 30,0 0,0 10,0 737QN DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 737QN DEFAULT 2 Descend 5 3 000,0 170,0 3,0 737QN DEFAULT 3 Descend D-25 1 500,0 134,5 3,0 737QN DEFAULT 4 Descend D-30 1 000,0 131,5 3,0 737QN DEFAULT 5 Land D-30 255,6 737QN DEFAULT 6 Decelerate 124,8 2 300,4 40,0 737QN DEFAULT 7 Decelerate 30,0 0,0 10,0 74710Q DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 74710Q DEFAULT 2 Descend 10 3 000,0 160,0 3,0 74710Q DEFAULT 3 Descend D-20 1 500,0 155,0 3,0 74710Q DEFAULT 4 Descend D-30 1 000,0 144,0 3,0 74710Q DEFAULT 5 Land D-30 462,6 74710Q DEFAULT 6 Decelerate 136,6 4 163,4 10,0 74710Q DEFAULT 7 Decelerate 30,0 0,0 10,0 747200 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0L 168/192 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 747200 DEFAULT 2 Descend 10 3 000,0 160,0 3,0 747200 DEFAULT 3 Descend D-20 1 500,0 155,0 3,0 747200 DEFAULT 4 Descend D-30 1 000,0 144,0 3,0 747200 DEFAULT 5 Land D-30 462,6 747200 DEFAULT 6 Decelerate 136,6 4 163,4 10,0 747200 DEFAULT 7 Decelerate 30,0 0,0 10,0 74720A DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 74720A DEFAULT 2 Descend 10 3 000,0 163,7 3,0 74720A DEFAULT 3 Descend D-25 1 500,0 150,0 3,0 74720A DEFAULT 4 Descend D-30 1 000,0 143,7 3,0 74720A DEFAULT 5 Land D-30 462,6 74720A DEFAULT 6 Decelerate 136,3 4 163,4 10,0 74720A DEFAULT 7 Decelerate 30,0 0,0 10,0 74720B DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 74720B DEFAULT 2 Descend 10 3 000,0 171,9 3,0 74720B DEFAULT 3 Descend D-25 1 500,0 158,5 3,0 74720B DEFAULT 4 Descend D-30 1 000,0 151,9 3,0 74720B DEFAULT 5 Land D-30 462,6 74720B DEFAULT 6 Decelerate 144,1 4 163,4 10,0 74720B DEFAULT 7 Decelerate 30,0 0,0 10,0 747400 DEFAULT 1 Descend 5 6 000,0 250,0 3,0 747400 DEFAULT 2 Descend 10 3 000,0 175,4 3,01.7.2015 EN Official Journal of the European Union L 168/193 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 747400 DEFAULT 3 Descend D-25 1 500,0 161,4 3,0 747400 DEFAULT 4 Descend D-30 1 000,0 155,4 3,0 747400 DEFAULT 5 Land D-30 533,6 747400 DEFAULT 6 Decelerate 147,5 4 802,4 10,0 747400 DEFAULT 7 Decelerate 30,0 0,0 10,0 7478 DEFAULT 1 Descend-Idle 6 000,0 278,8 3,0 7478 DEFAULT 2 Level-Idle 3 000,0 279,5 30 000,0 7478 DEFAULT 3 Level-Idle 3 000,0 218,3 10 000,0 7478 DEFAULT 4 Level-Idle 3 000,0 186,1 3 050,0 7478 DEFAULT 5 Level-Idle 3 000,0 174,6 4 500,0 7478 DEFAULT 6 Level F_10 3 000,0 162,3 2 069,0 7478 DEFAULT 7 Descend F_30 3 000,0 157,4 3,0 7478 DEFAULT 8 Land F_30 615,6 7478 DEFAULT 9 Decelerate 150,4 5 540,4 10,0 7478 DEFAULT 10 Decelerate 30,0 0,0 10,0 747SP DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 747SP DEFAULT 2 Descend 10 3 000,0 160,0 3,0 747SP DEFAULT 3 Descend D-20 1 500,0 141,5 3,0 747SP DEFAULT 4 Descend D-30 1 000,0 132,4 3,0 747SP DEFAULT 5 Land D-30 436,6 747SP DEFAULT 6 Decelerate 125,6 3 929,4 10,0 747SP DEFAULT 7 Decelerate 30,0 0,0 10,0L 168/194 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 757PW DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 757PW DEFAULT 2 Descend 5 3 000,0 160,0 3,0 757PW DEFAULT 3 Descend D-25 1 500,0 136,5 3,0 757PW DEFAULT 4 Descend D-30 1 000,0 134,2 3,0 757PW DEFAULT 5 Land D-30 335,7 757PW DEFAULT 6 Decelerate 127,3 3 021,3 40,0 757PW DEFAULT 7 Decelerate 30,0 0,0 10,0 757RR DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 757RR DEFAULT 2 Descend 5 3 000,0 160,0 3,0 757RR DEFAULT 3 Descend D-25 1 500,0 136,7 3,0 757RR DEFAULT 4 Descend D-30 1 000,0 134,7 3,0 757RR DEFAULT 5 Land D-30 322,2 757RR DEFAULT 6 Decelerate 127,8 2 899,8 40,0 757RR DEFAULT 7 Decelerate 30,0 0,0 10,0 767300 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 767300 DEFAULT 2 Descend 5 3 000,0 167,0 3,0 767300 DEFAULT 3 Descend D-25 1 500,0 141,0 3,0 767300 DEFAULT 4 Descend D-30 1 000,0 137,1 3,0 767300 DEFAULT 5 Land D-30 328,5 767300 DEFAULT 6 Decelerate 130,1 2 956,5 10,0 767300 DEFAULT 7 Decelerate 30,0 0,0 10,0 767CF6 DEFAULT 1 Descend 1 6 000,0 250,0 3,01.7.2015 EN Official Journal of the European Union L 168/195 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 767CF6 DEFAULT 2 Descend 5 3 000,0 168,5 3,0 767CF6 DEFAULT 3 Descend D-25 1 500,0 143,0 3,0 767CF6 DEFAULT 4 Descend D-30 1 000,0 138,5 3,0 767CF6 DEFAULT 5 Land D-30 327,6 767CF6 DEFAULT 6 Decelerate 131,4 2 948,4 10,0 767CF6 DEFAULT 7 Decelerate 30,0 0,0 10,0 767JT9 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 767JT9 DEFAULT 2 Descend 5 3 000,0 168,5 3,0 767JT9 DEFAULT 3 Descend D-25 1 500,0 143,0 3,0 767JT9 DEFAULT 4 Descend D-30 1 000,0 138,5 3,0 767JT9 DEFAULT 5 Land D-30 331,6 767JT9 DEFAULT 6 Decelerate 131,4 2 984,4 10,0 767JT9 DEFAULT 7 Decelerate 30,0 0,0 10,0 7773ER DEFAULT 1 Descend-Idle 6 000,0 249,9 3,0 7773ER DEFAULT 2 Level-Idle 3 000,0 249,9 20 776,0 7773ER DEFAULT 3 Level-Idle 3 000,0 210,6 10 088,0 7773ER DEFAULT 4 Level-Idle 3 000,0 185,4 5 926,0 7773ER DEFAULT 5 Descend- 3 000,0 170,4 3,0 Idle 7773ER DEFAULT 6 Descend F_30 2 700,0 147,8 3,0 7773ER DEFAULT 7 Land F_30 427,1 7773ER DEFAULT 8 Decelerate 140,8 3 843,5 10,0 7773ER DEFAULT 9 Decelerate 30,0 0,0 10,0L 168/196 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) 7878R DEFAULT 1 Descend- 6 000,0 249,0 3,0 Idle 7878R DEFAULT 2 Level-Idle 3 000,0 249,5 20 950,0 7878R DEFAULT 3 Level-Idle 3 000,0 214,3 10 000,0 7878R DEFAULT 4 Level-Idle 3 000,0 178,9 5 000,0 7878R DEFAULT 5 Descend-Idle 3 000,0 157,0 3,0 7878R DEFAULT 6 Descend FLAP30 2 725,0 142,3 3,0 7878R DEFAULT 7 Land FLAP30 362,7 7878R DEFAULT 8 Decelerate 135,3 3 264,3 10,0 7878R DEFAULT 9 Decelerate 30,0 0,0 10,0 A300-622R DEFAULT 1 Descend-Idle 6 000,0 250,0 3,3 A300-622R DEFAULT 2 Level-Idle 3 000,0 250,0 14 583,3 A300-622R DEFAULT 3 Level-Idle 3 000,0 210,9 7 398,3 A300-622R DEFAULT 4 Descend-Idle 3 000,0 185,1 3,0 A300-622R DEFAULT 5 Descend-Idle 2 417,0 175,9 3,0 A300-622R DEFAULT 6 Descend-Idle 1 818,0 149,0 3,0 A300-622R DEFAULT 7 Descend FULL_D 1 615,0 133,5 3,0 A300-622R DEFAULT 8 Descend FULL_D 50,0 133,5 3,0 A300-622R DEFAULT 9 Land FULL_D 305,3 A300-622R DEFAULT 10 Decelerate 130,5 2 747,8 10,0 A300-622R DEFAULT 11 Decelerate 30,0 0,0 10,0 A300B4-203 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 A300B4-203 DEFAULT 2 Descend 1 3 000,0 158,5 3,01.7.2015 EN Official Journal of the European Union L 168/197 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) A300B4-203 DEFAULT 3 Descend D-15 1 500,0 148,5 3,0 A300B4-203 DEFAULT 4 Descend D-25 1 000,0 140,0 3,0 A300B4-203 DEFAULT 5 Land D-25 387,6 A300B4-203 DEFAULT 6 Decelerate 132,8 3 488,4 40,0 A300B4-203 DEFAULT 7 Decelerate 30,0 0,0 10,0 A310-304 DEFAULT 1 Descend-Idle 6 000,0 250,0 3,2 A310-304 DEFAULT 2 Level-Idle 3 000,0 250,0 14 609,6 A310-304 DEFAULT 3 Level-Idle 3 000,0 211,6 8 736,9 A310-304 DEFAULT 4 Descend-Idle 3 000,0 180,6 3,0 A310-304 DEFAULT 5 Descend-Idle 2 551,0 169,3 3,0 A310-304 DEFAULT 6 Descend-Idle 2 147,0 148,0 3,0 A310-304 DEFAULT 7 Descend FULL_D 2 000,0 134,6 3,0 A310-304 DEFAULT 8 Descend FULL_D 50,0 134,6 3,0 A310-304 DEFAULT 9 Land FULL_D 302,9 A310-304 DEFAULT 10 Decelerate 131,6 2 726,6 10,0 A310-304 DEFAULT 11 Decelerate 30,0 0,0 10,0 A319-131 DEFAULT 1 Descend-Idle 6 000,0 250,0 3,1 A319-131 DEFAULT 2 Level-Idle 3 000,0 250,0 19 940,9 A319-131 DEFAULT 3 Level-Idle 3 000,0 197,5 4 813,0 A319-131 DEFAULT 4 Descend-Idle 3 000,0 181,4 3,0 A319-131 DEFAULT 5 Descend-Idle 2 610,0 167,7 3,0 A319-131 DEFAULT 6 Descend-Idle 2 114,0 138,4 3,0L 168/198 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) A319-131 DEFAULT 7 Descend FULL_D 1 971,0 125,3 3,0 A319-131 DEFAULT 8 Descend FULL_D 50,0 125,3 3,0 A319-131 DEFAULT 9 Land FULL_D 152,3 A319-131 DEFAULT 10 Decelerate 122,3 1 370,6 40,0 A319-131 DEFAULT 11 Decelerate 30,0 0,0 10,0 A320-211 DEFAULT 1 Descend-Idle 6 000,0 250,0 3,5 A320-211 DEFAULT 2 Level-Idle 3 000,0 250,0 16 811,0 A320-211 DEFAULT 3 Level-Idle 3 000,0 201,1 5 547,9 A320-211 DEFAULT 4 Descend-Idle 3 000,0 182,2 3,0 A320-211 DEFAULT 5 Descend-Idle 2 614,0 173,7 3,0 A320-211 DEFAULT 6 Descend-Idle 1 942,0 141,0 3,0 A320-211 DEFAULT 7 Descend FULL_D 1 823,0 132,6 3,0 A320-211 DEFAULT 8 Descend FULL_D 50,0 132,6 3,0 A320-211 DEFAULT 9 Land FULL_D 303,5 A320-211 DEFAULT 10 Decelerate 129,6 2 731,6 40,0 A320-211 DEFAULT 11 Decelerate 30,0 0,0 10,0 A320-232 DEFAULT 1 Descend-Idle 6 000,0 250,0 2,8 A320-232 DEFAULT 2 Level-Idle 3 000,0 250,0 20 003,3 A320-232 DEFAULT 3 Level-Idle 3 000,0 198,7 4 629,3 A320-232 DEFAULT 4 Descend-Idle 3 000,0 183,5 3,0 A320-232 DEFAULT 5 Descend-Idle 2 613,0 172,8 3,0 A320-232 DEFAULT 6 Descend-Idle 2 033,0 142,2 3,01.7.2015 EN Official Journal of the European Union L 168/199 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) A320-232 DEFAULT 7 Descend FULL_D 1 819,0 133,8 3,0 A320-232 DEFAULT 8 Descend FULL_D 50,0 133,8 3,0 A320-232 DEFAULT 9 Land FULL_D 311,0 A320-232 DEFAULT 10 Decelerate 130,8 2 799,4 40,0 A320-232 DEFAULT 11 Decelerate 30,0 0,0 10,0 A321-232 DEFAULT 1 Descend-Idle 6 000,0 250,0 3,1 A321-232 DEFAULT 2 Level-Idle 3 000,0 250,0 14 717,8 A321-232 DEFAULT 3 Level-Idle 3 000,0 211,2 6 135,2 A321-232 DEFAULT 4 Descend-Idle 3 000,0 191,6 3,0 A321-232 DEFAULT 5 Descend-Idle 2 530,0 175,2 3,0 A321-232 DEFAULT 6 Descend-Idle 2 133,0 149,8 3,0 A321-232 DEFAULT 7 Descend FULL_D 2 003,0 138,5 3,0 A321-232 DEFAULT 8 Descend FULL_D 50,0 138,5 3,0 A321-232 DEFAULT 9 Land FULL_D 345,2 A321-232 DEFAULT 10 Decelerate 135,5 3 106,8 40,0 A321-232 DEFAULT 11 Decelerate 30,0 0,0 10,0 A330-301 DEFAULT 1 Descend-Idle 6 000,0 250,0 3,1 A330-301 DEFAULT 2 Level-Idle 3 000,0 250,0 19 547,2 A330-301 DEFAULT 3 Level-Idle 3 000,0 200,9 10 029,5 A330-301 DEFAULT 4 Descend-Idle 3 000,0 166,0 3,0 A330-301 DEFAULT 5 Descend-Idle 2 547,0 154,0 3,0 A330-301 DEFAULT 6 Descend-Idle 2 292,0 140,5 3,0L 168/200 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) A330-301 DEFAULT 7 Descend FULL_D 2 144,0 130,9 3,0 A330-301 DEFAULT 8 Descend FULL_D 50,0 130,9 3,0 A330-301 DEFAULT 9 Land FULL_D 210,4 A330-301 DEFAULT 10 Decelerate 127,9 1 893,8 10,0 A330-301 DEFAULT 11 Decelerate 30,0 0,0 10,0 A330-343 DEFAULT 1 Descend-Idle 6 000,0 250,0 2,4 A330-343 DEFAULT 2 Level-Idle 3 000,0 250,0 20 711,9 A330-343 DEFAULT 3 Level-Idle 3 000,0 207,9 11 430,4 A330-343 DEFAULT 4 Descend-Idle 3 000,0 174,4 3,0 A330-343 DEFAULT 5 Descend-Idle 2 517,0 165,0 3,0 A330-343 DEFAULT 6 Descend-Idle 2 431,0 161,7 3,0 A330-343 DEFAULT 7 Descend-Idle 2 113,0 146,6 3,0 A330-343 DEFAULT 8 Descend FULL_D 1 938,0 135,5 3,0 A330-343 DEFAULT 9 Descend FULL_D 50,0 135,5 3,0 A330-343 DEFAULT 10 Land FULL_D 378,0 A330-343 DEFAULT 11 Decelerate 132,5 3 402,6 10,0 A330-343 DEFAULT 12 Decelerate 30,0 0,0 10,0 A340-211 DEFAULT 1 Descend-Idle 6 000,0 250,0 3,3 A340-211 DEFAULT 2 Level-Idle 3 000,0 250,0 14 038,7 A340-211 DEFAULT 3 Level-Idle 3 000,0 212,7 10 866,1 A340-211 DEFAULT 4 Descend-Idle 3 000,0 175,6 3,0 A340-211 DEFAULT 5 Descend-Idle 2 471,0 160,3 3,01.7.2015 EN Official Journal of the European Union L 168/201 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) A340-211 DEFAULT 6 Descend-Idle 2 336,0 153,8 3,0 A340-211 DEFAULT 7 Descend-Idle 2 066,0 138,5 3,0 A340-211 DEFAULT 8 Descend FULL_D 1 976,0 132,1 3,0 A340-211 DEFAULT 9 Descend FULL_D 50,0 132,1 3,0 A340-211 DEFAULT 10 Land FULL_D 381,8 A340-211 DEFAULT 11 Decelerate 129,1 3 436,6 10,0 A340-211 DEFAULT 12 Decelerate 30,0 0,0 10,0 A340-642 DEFAULT 1 Descend-Idle 6 000,0 250,0 2,8 A340-642 DEFAULT 2 Level-Idle 3 000,0 250,0 15 853,0 A340-642 DEFAULT 3 Level-Idle 3 000,0 212,1 9 839,2 A340-642 DEFAULT 4 Descend-Idle 3 000,0 188,5 3,0 A340-642 DEFAULT 5 Descend-Idle 2 333,0 178,1 3,0 A340-642 DEFAULT 6 Descend-Idle 2 191,0 173,2 3,0 A340-642 DEFAULT 7 Descend-Idle 1 805,0 155,5 3,0 A340-642 DEFAULT 8 Descend FULL_D 1 650,0 147,8 3,0 A340-642 DEFAULT 9 Descend FULL_D 50,0 147,8 3,0 A340-642 DEFAULT 10 Land FULL_D 280,7 A340-642 DEFAULT 11 Decelerate 144,8 2 526,5 10,0 A340-642 DEFAULT 12 Decelerate 30,0 0,0 10,0 A380-841 DEFAULT 1 Descend-Idle 6 000,0 250,0 3,0 A380-841 DEFAULT 2 Level-Idle 3 000,0 250,0 18 044,6 A380-841 DEFAULT 3 Level A_1+F 3 000,0 11 893,0L 168/202 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) A380-841 DEFAULT 4 Level-Idle 3 000,0 205,0 9 691,6 A380-841 DEFAULT 5 Descend-Idle 3 000,0 172,6 3,0 A380-841 DEFAULT 6 Descend-Idle 2 446,0 161,2 3,0 A380-841 DEFAULT 7 Descend A_FULL 1 976,0 136,3 3,0 A380-841 DEFAULT 8 Descend A_FULL 50,0 136,3 3,0 A380-841 DEFAULT 9 Land A_FULL 636,8 A380-841 DEFAULT 10 Decelerate 136,3 5 731,3 10,0 A380-841 DEFAULT 11 Decelerate 30,0 0,0 10,0 A380-861 DEFAULT 1 Descend-Idle 6 000,0 250,0 2,7 A380-861 DEFAULT 2 Level-Idle 3 000,0 250,0 20 036,1 A380-861 DEFAULT 3 Level A_1+F 3 000,0 11 896,0 A380-861 DEFAULT 4 Level-Idle 3 000,0 205,0 10 213,0 A380-861 DEFAULT 5 Descend-Idle 3 000,0 172,6 3,0 A380-861 DEFAULT 6 Descend-Idle 2 445,0 161,2 3,0 A380-861 DEFAULT 7 Descend A_FULL 1 976,0 136,3 3,0 A380-861 DEFAULT 8 Descend A_FULL 50,0 136,3 3,0 A380-861 DEFAULT 9 Land A_FULL 636,8 A380-861 DEFAULT 10 Decelerate 136,3 5 731,3 10,0 A380-861 DEFAULT 11 Decelerate 30,0 0,0 10,0 BAC111 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 BAC111 DEFAULT 2 Descend INT1 3 000,0 153,3 3,0 BAC111 DEFAULT 3 Descend U-INT 1 500,0 143,3 3,01.7.2015 EN Official Journal of the European Union L 168/203 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) BAC111 DEFAULT 4 Descend D-45 1 000,0 133,3 3,0 BAC111 DEFAULT 5 Land D-45 305,0 BAC111 DEFAULT 6 Decelerate 126,5 2 745,0 40,0 BAC111 DEFAULT 7 Decelerate 30,0 0,0 10,0 BAE146 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 BAE146 DEFAULT 2 Descend 18 3 000,0 180,0 3,0 BAE146 DEFAULT 3 Descend D-24 1 500,0 166,5 3,0 BAE146 DEFAULT 4 Descend D-33 1 000,0 123,0 3,0 BAE146 DEFAULT 5 Land D-33 243,9 BAE146 DEFAULT 6 Decelerate 116,7 2 195,1 40,0 BAE146 DEFAULT 7 Decelerate 30,0 0,0 10,0 BAE300 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 BAE300 DEFAULT 2 Descend 18 3 000,0 180,0 3,0 BAE300 DEFAULT 3 Descend D-24 1 500,0 167,0 3,0 BAE300 DEFAULT 4 Descend D-33 1 000,0 124,4 3,0 BAE300 DEFAULT 5 Land D-33 261,0 BAE300 DEFAULT 6 Decelerate 118,0 2 349,0 40,0 BAE300 DEFAULT 7 Decelerate 30,0 0,0 10,0 BEC58P DEFAULT 1 Descend ZERO 6 000,0 130,0 5,0 BEC58P DEFAULT 2 Descend TO 3 000,0 119,0 5,0 BEC58P DEFAULT 3 Descend D-15 1 500,0 109,0 5,0 BEC58P DEFAULT 4 Descend D-30 1 000,0 99,0 5,0L 168/204 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) BEC58P DEFAULT 5 Land D-30 188,8 BEC58P DEFAULT 6 Decelerate 93,9 1 699,2 40,0 BEC58P DEFAULT 7 Decelerate 30,0 0,0 10,0 BEC58P STD_3DEG 1 Descend ZERO 6 000,0 130,0 3,0 BEC58P STD_3DEG 2 Descend TO 3 000,0 119,0 3,0 BEC58P STD_3DEG 3 Descend D-15 1 500,0 109,0 3,0 BEC58P STD_3DEG 4 Descend D-30 1 000,0 99,0 3,0 BEC58P STD_3DEG 5 Land D-30 188,8 BEC58P STD_3DEG 6 Decelerate 93,9 1 699,2 40,0 BEC58P STD_3DEG 7 Decelerate 30,0 0,0 10,0 BEC58P STD_5DEG 1 Descend ZERO 6 000,0 130,0 5,0 BEC58P STD_5DEG 2 Descend TO 3 000,0 119,0 5,0 BEC58P STD_5DEG 3 Descend D-15 1 500,0 109,0 5,0 BEC58P STD_5DEG 4 Descend D-30 1 000,0 99,0 5,0 BEC58P STD_5DEG 5 Land D-30 188,8 BEC58P STD_5DEG 6 Decelerate 93,9 1 699,2 40,0 BEC58P STD_5DEG 7 Decelerate 30,0 0,0 10,0 CIT3 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 CIT3 DEFAULT 2 Descend 10 3 000,0 139,5 3,0 CIT3 DEFAULT 3 Descend D-INTR 1 500,0 129,5 3,0 CIT3 DEFAULT 4 Descend D-40 1 000,0 119,5 3,0 CIT3 DEFAULT 5 Land D-40 153,91.7.2015 EN Official Journal of the European Union L 168/205 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) CIT3 DEFAULT 6 Decelerate 113,4 1 385,1 40,0 CIT3 DEFAULT 7 Decelerate 30,0 0,0 10,0 CL600 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 CL600 DEFAULT 2 Descend 10 3 000,0 152,1 3,0 CL600 DEFAULT 3 Descend D-INTR 1 500,0 142,1 3,0 CL600 DEFAULT 4 Descend D-45 1 000,0 132,1 3,0 CL600 DEFAULT 5 Land D-45 201,6 CL600 DEFAULT 6 Decelerate 125,3 1 814,4 40,0 CL600 DEFAULT 7 Decelerate 30,0 0,0 10,0 CL601 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 CL601 DEFAULT 2 Descend 10 3 000,0 158,5 3,0 CL601 DEFAULT 3 Descend D-INTR 1 500,0 148,5 3,0 CL601 DEFAULT 4 Descend D-45 1 000,0 138,5 3,0 CL601 DEFAULT 5 Land D-45 224,1 CL601 DEFAULT 6 Decelerate 131,4 2 016,9 40,0 CL601 DEFAULT 7 Decelerate 30,0 0,0 10,0 CNA172 DEFAULT 1 Descend ZERO-D 6 000,0 100,0 3,0 CNA172 DEFAULT 2 Descend ZERO-D 4 000,0 100,0 3,0 CNA172 DEFAULT 3 Descend ZERO-D 3 000,0 80,0 3,0 CNA172 DEFAULT 4 Descend 10-D 1 000,0 80,0 3,0 CNA172 DEFAULT 5 Descend 10-D 600,0 80,0 3,0 CNA172 DEFAULT 6 Descend 10-D 500,0 70,0 3,0L 168/206 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) CNA172 DEFAULT 7 Land 10-D 30,0 CNA172 DEFAULT 8 Decelerate 62,0 530,0 10,0 CNA172 DEFAULT 9 Decelerate 10,0 0,0 10,0 CNA182 DEFAULT 1 Descend ZERO-A 6 000,0 110,0 3,0 CNA182 DEFAULT 2 Descend ZERO-A 4 000,0 90,0 3,0 CNA182 DEFAULT 3 Descend ZERO-A 2 000,0 70,0 3,0 CNA182 DEFAULT 4 Descend F10APP 1 000,0 70,0 3,0 CNA182 DEFAULT 5 Descend F30APP 500,0 65,0 3,0 CNA182 DEFAULT 6 Land F30APP 30,0 CNA182 DEFAULT 7 Decelerate 65,0 560,0 10,0 CNA182 DEFAULT 8 Decelerate 10,0 0,0 10,0 CNA208 DEFAULT 1 Descend ZERO-A 6 000,0 140,0 3,0 CNA208 DEFAULT 2 Descend ZERO-A 4 000,0 124,0 3,0 CNA208 DEFAULT 3 Descend ZERO-A 2 000,0 108,0 3,0 CNA208 DEFAULT 4 Descend F30APP 1 000,0 100,0 3,0 CNA208 DEFAULT 5 Descend F30APP 500,0 80,0 3,0 CNA208 DEFAULT 6 Land F30APP 100,0 CNA208 DEFAULT 7 Decelerate 78,0 815,0 10,0 CNA208 DEFAULT 8 Decelerate 30,0 0,0 10,0 CNA441 DEFAULT 1 Descend ZERO 6 000,0 160,0 3,0 CNA441 DEFAULT 2 Descend TO 3 000,0 113,9 3,0 CNA441 DEFAULT 3 Descend D-INTR 1 500,0 103,9 3,01.7.2015 EN Official Journal of the European Union L 168/207 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) CNA441 DEFAULT 4 Descend D-L 1 000,0 93,9 3,0 CNA441 DEFAULT 5 Land D-L 79,1 CNA441 DEFAULT 6 Decelerate 89,1 711,9 40,0 CNA441 DEFAULT 7 Decelerate 30,0 0,0 10,0 CNA500 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 CNA500 DEFAULT 2 Descend 1 3 000,0 131,3 3,0 CNA500 DEFAULT 3 Descend D-INTR 1 500,0 121,3 3,0 CNA500 DEFAULT 4 Descend D-35 1 000,0 111,3 3,0 CNA500 DEFAULT 5 Land D-35 179,1 CNA500 DEFAULT 6 Decelerate 105,6 1 611,9 40,0 CNA500 DEFAULT 7 Decelerate 30,0 0,0 10,0 CNA510 DEFAULT 1 Descend ZERO_C 6 000,0 250,0 3,0 CNA510 DEFAULT 2 Descend ZERO_C 3 000,0 160,0 3,0 CNA510 DEFAULT 3 Descend A_15 1 500,0 91,1 3,0 CNA510 DEFAULT 4 Descend A_35 1 000,0 85,1 3,0 CNA510 DEFAULT 5 Land A_35 175,5 CNA510 DEFAULT 6 Decelerate 78,1 1 579,5 40,0 CNA510 DEFAULT 7 Decelerate 30,0 0,0 10,0 CNA525C DEFAULT 1 Descend ZERO_C 6 000,0 250,0 3,0 CNA525C DEFAULT 2 Descend ZERO_C 3 000,0 130,0 3,0 CNA525C DEFAULT 3 Descend A_15 1 500,0 119,7 3,0 CNA525C DEFAULT 4 Descend A_35 1 000,0 111,8 3,0L 168/208 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) CNA525C DEFAULT 5 Land A_35 200,0 CNA525C DEFAULT 6 Decelerate 115,0 1 500,0 40,0 CNA525C DEFAULT 7 Decelerate 30,0 0,0 10,0 CNA55B DEFAULT 1 Descend ZERO_C 6 000,0 250,0 3,0 CNA55B DEFAULT 2 Descend ZERO_C 3 000,0 160,0 3,0 CNA55B DEFAULT 3 Descend A_15 1 500,0 111,8 3,0 CNA55B DEFAULT 4 Descend A_35 1 000,0 105,3 3,0 CNA55B DEFAULT 5 Land A_35 175,5 CNA55B DEFAULT 6 Decelerate 100,0 1 580,0 40,0 CNA55B DEFAULT 7 Decelerate 30,0 0,0 10,0 CNA560E DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 CNA560E DEFAULT 2 Descend 15 U 3 000,0 107,5 3,0 CNA560E DEFAULT 3 Descend 35 D 1 500,0 101,8 3,0 CNA560E DEFAULT 4 Descend 35 D 1 000,0 101,8 3,0 CNA560E DEFAULT 5 Land 35 D 200,0 CNA560E DEFAULT 6 Decelerate 100,0 1 000,0 60,0 CNA560E DEFAULT 7 Decelerate 30,0 0,0 10,0 CNA560U DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 CNA560U DEFAULT 2 Descend 7 3 000,0 120,0 3,0 CNA560U DEFAULT 3 Descend D 15 1 500,0 110,0 3,0 CNA560U DEFAULT 4 Descend D 35 1 000,0 101,8 3,0 CNA560U DEFAULT 5 Land D 35 175,01.7.2015 EN Official Journal of the European Union L 168/209 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) CNA560U DEFAULT 6 Decelerate 93,0 1 385,1 60,0 CNA560U DEFAULT 7 Decelerate 30,0 0,0 10,0 CNA560XL DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 CNA560XL DEFAULT 2 Descend ZERO 3 000,0 132,0 3,0 CNA560XL DEFAULT 3 Descend D 15U 1 500,0 122,0 3,0 CNA560XL DEFAULT 4 Descend D 35D 1 000,0 112,0 3,0 CNA560XL DEFAULT 5 Land D 35D 500,0 CNA560XL DEFAULT 6 Decelerate 108,0 2 700,0 60,0 CNA560XL DEFAULT 7 Decelerate 30,0 0,0 10,0 CNA680 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 CNA680 DEFAULT 2 Descend ZERO 3 000,0 160,0 3,0 CNA680 DEFAULT 3 Descend 15 GU 1 500,0 112,0 3,0 CNA680 DEFAULT 4 Descend 35 GD 1 000,0 105,0 3,0 CNA680 DEFAULT 5 Land 35 GD 200,0 CNA680 DEFAULT 6 Decelerate 100,0 1 580,0 60,0 CNA680 DEFAULT 7 Decelerate 30,0 0,0 10,0 CNA750 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 CNA750 DEFAULT 2 Descend 15_GU 3 000,0 127,4 3,0 CNA750 DEFAULT 3 Descend 35_GD 1 500,0 120,9 3,0 CNA750 DEFAULT 4 Descend 35_GD 1 000,0 120,9 3,0 CNA750 DEFAULT 5 Land 35_GD 200,0 CNA750 DEFAULT 6 Decelerate 115,0 1 500,0 40,0L 168/210 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) CNA750 DEFAULT 7 Decelerate 30,0 0,0 10,0 CNA750 FLAP_15 1 Descend ZERO 6 000,0 250,0 3,0 CNA750 FLAP_15 2 Descend 15_GU 3 000,0 127,4 3,0 CNA750 FLAP_15 3 Descend 35_GD 1 500,0 120,9 3,0 CNA750 FLAP_15 4 Descend 35_GD 1 000,0 120,9 3,0 CNA750 FLAP_15 5 Land 35_GD 200,0 CNA750 FLAP_15 6 Decelerate 115,0 1 500,0 40,0 CNA750 FLAP_15 7 Decelerate 30,0 0,0 10,0 CNA750 FLAP_5 1 Descend ZERO 6 000,0 250,0 3,0 CNA750 FLAP_5 2 Descend 5_GU 3 000,0 135,2 3,0 CNA750 FLAP_5 3 Descend 15_GD 1 500,0 127,4 3,0 CNA750 FLAP_5 4 Descend 15_GD 1 000,0 127,4 3,0 CNA750 FLAP_5 5 Land 15_GD 200,0 CNA750 FLAP_5 6 Decelerate 115,0 1 500,0 40,0 CNA750 FLAP_5 7 Decelerate 30,0 0,0 10,0 CONCRD DEFAULT 1 Descend CL1 6 000,0 250,0 3,0 CONCRD DEFAULT 2 Descend ZERO 3 000,0 194,0 3,0 CONCRD DEFAULT 3 Descend U-L 1 500,0 184,0 3,0 CONCRD DEFAULT 4 Descend D-L 1 000,0 164,0 3,0 CONCRD DEFAULT 5 Land D-L 858,6 CONCRD DEFAULT 6 Decelerate 155,5 7 727,4 40,0 CONCRD DEFAULT 7 Decelerate 30,0 0,0 10,01.7.2015 EN Official Journal of the European Union L 168/211 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) CRJ9-ER DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 CRJ9-ER DEFAULT 2 Descend 20 3 500,0 170,0 3,0 CRJ9-ER DEFAULT 3 Descend U-45 1 500,0 160,0 3,0 CRJ9-ER DEFAULT 4 Descend D-45 1 000,0 140,0 3,0 CRJ9-ER DEFAULT 5 Land D-45 415,8 CRJ9-ER DEFAULT 6 Decelerate 143,0 2 528,0 10,0 CRJ9-ER DEFAULT 7 Decelerate 30,0 0,0 10,0 CRJ9-LR DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 CRJ9-LR DEFAULT 2 Descend 20 3 500,0 170,0 3,0 CRJ9-LR DEFAULT 3 Descend U-45 1 500,0 160,0 3,0 CRJ9-LR DEFAULT 4 Descend D-45 1 000,0 141,0 3,0 CRJ9-LR DEFAULT 5 Land D-45 424,7 CRJ9-LR DEFAULT 6 Decelerate 144,0 2 577,0 10,0 CRJ9-LR DEFAULT 7 Decelerate 30,0 0,0 10,0 CVR580 DEFAULT 1 Descend ZERO 6 000,0 200,0 3,0 CVR580 DEFAULT 2 Descend INTR 3 000,0 146,3 3,0 CVR580 DEFAULT 3 Descend D-28 1 500,0 112,4 3,0 CVR580 DEFAULT 4 Descend D-40 1 000,0 106,3 3,0 CVR580 DEFAULT 5 Land D-40 287,6 CVR580 DEFAULT 6 Decelerate 100,9 2 588,4 40,0 CVR580 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC1010 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0L 168/212 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) DC1010 DEFAULT 2 Descend INT 3 000,0 163,7 3,0 DC1010 DEFAULT 3 Descend U-35 1 500,0 153,7 3,0 DC1010 DEFAULT 4 Descend D-35 1 000,0 143,7 3,0 DC1010 DEFAULT 5 Land D-35 428,4 DC1010 DEFAULT 6 Decelerate 136,3 3 855,6 10,0 DC1010 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC1030 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC1030 DEFAULT 2 Descend INT2 3 000,0 172,6 3,0 DC1030 DEFAULT 3 Descend U-20 1 500,0 162,6 3,0 DC1030 DEFAULT 4 Descend D-35 1 000,0 152,6 3,0 DC1030 DEFAULT 5 Land D-35 392,2 DC1030 DEFAULT 6 Decelerate 144,8 3 529,8 10,0 DC1030 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC1040 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC1040 DEFAULT 2 Descend 5 3 000,0 173,5 3,0 DC1040 DEFAULT 3 Descend U-35 1 500,0 163,5 3,0 DC1040 DEFAULT 4 Descend D-35 1 000,0 153,5 3,0 DC1040 DEFAULT 5 Land D-35 446,4 DC1040 DEFAULT 6 Decelerate 145,6 4 017,6 10,0 DC1040 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC3 DEFAULT 1 Descend ZERO 6 000,0 140,0 3,0 DC3 DEFAULT 2 Descend TO 3 000,0 109,0 3,01.7.2015 EN Official Journal of the European Union L 168/213 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) DC3 DEFAULT 3 Descend U-INT 1 500,0 99,0 3,0 DC3 DEFAULT 4 Descend D-45 1 000,0 88,9 3,0 DC3 DEFAULT 5 Land D-45 104,6 DC3 DEFAULT 6 Decelerate 84,3 941,4 34,3 DC3 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC6 DEFAULT 1 Descend ZERO 6 000,0 160,0 3,0 DC6 DEFAULT 2 Descend TO 3 000,0 106,1 3,0 DC6 DEFAULT 3 Descend D-INTR 1 500,0 96,1 3,0 DC6 DEFAULT 4 Descend D-L 1 000,0 86,1 3,0 DC6 DEFAULT 5 Land D-L 175,5 DC6 DEFAULT 6 Decelerate 81,7 1 579,5 40,0 DC6 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC850 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC850 DEFAULT 2 Descend INT 3 000,0 165,6 3,0 DC850 DEFAULT 3 Descend D-35 1 500,0 152,7 3,0 DC850 DEFAULT 4 Descend D-50 1 000,0 145,6 3,0 DC850 DEFAULT 5 Land D-50 390,6 DC850 DEFAULT 6 Decelerate 138,1 3 515,4 40,0 DC850 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC860 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC860 DEFAULT 2 Descend INT 3 000,0 161,5 3,0 DC860 DEFAULT 3 Descend D-35 1 500,0 155,7 3,0L 168/214 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) DC860 DEFAULT 4 Descend D-50 1 000,0 151,5 3,0 DC860 DEFAULT 5 Land D-50 382,5 DC860 DEFAULT 6 Decelerate 143,7 3 442,5 40,0 DC860 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC870 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC870 DEFAULT 2 Descend INT 3 000,0 166,7 3,0 DC870 DEFAULT 3 Descend D-35 1 500,0 150,8 3,0 DC870 DEFAULT 4 Descend D-50 1 000,0 146,7 3,0 DC870 DEFAULT 5 Land D-50 489,6 DC870 DEFAULT 6 Decelerate 139,2 4 406,4 40,0 DC870 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC8QN DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC8QN DEFAULT 2 Descend INT 3 000,0 161,5 3,0 DC8QN DEFAULT 3 Descend D-35 1 500,0 155,7 3,0 DC8QN DEFAULT 4 Descend D-50 1 000,0 151,5 3,0 DC8QN DEFAULT 5 Land D-50 382,5 DC8QN DEFAULT 6 Decelerate 143,7 3 442,5 40,0 DC8QN DEFAULT 7 Decelerate 30,0 0,0 10,0 DC910 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC910 DEFAULT 2 Descend 5 3 000,0 150,2 3,0 DC910 DEFAULT 3 Descend U-15 1 500,0 140,2 3,0 DC910 DEFAULT 4 Descend D-35 1 000,0 130,2 3,01.7.2015 EN Official Journal of the European Union L 168/215 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) DC910 DEFAULT 5 Land D-35 357,3 DC910 DEFAULT 6 Decelerate 123,5 3 215,7 40,0 DC910 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC930 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC930 DEFAULT 2 Descend 5 3 000,0 162,5 3,0 DC930 DEFAULT 3 Descend U-15 1 500,0 152,5 3,0 DC930 DEFAULT 4 Descend D-35 1 000,0 142,5 3,0 DC930 DEFAULT 5 Land D-35 325,8 DC930 DEFAULT 6 Decelerate 135,2 2 932,2 40,0 DC930 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC93LW DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC93LW DEFAULT 2 Descend 5 3 000,0 162,5 3,0 DC93LW DEFAULT 3 Descend U-15 1 500,0 152,5 3,0 DC93LW DEFAULT 4 Descend D-35 1 000,0 142,5 3,0 DC93LW DEFAULT 5 Land D-35 325,8 DC93LW DEFAULT 6 Decelerate 135,2 2 932,2 40,0 DC93LW DEFAULT 7 Decelerate 30,0 0,0 10,0 DC950 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC950 DEFAULT 2 Descend 5 3 000,0 167,3 3,0 DC950 DEFAULT 3 Descend U-15 1 500,0 157,3 3,0 DC950 DEFAULT 4 Descend D-35 1 000,0 147,3 3,0 DC950 DEFAULT 5 Land D-35 343,8L 168/216 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) DC950 DEFAULT 6 Decelerate 139,7 3 094,2 40,0 DC950 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC95HW DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC95HW DEFAULT 2 Descend 5 3 000,0 167,3 3,0 DC95HW DEFAULT 3 Descend U-15 1 500,0 157,3 3,0 DC95HW DEFAULT 4 Descend D-35 1 000,0 147,3 3,0 DC95HW DEFAULT 5 Land D-35 343,8 DC95HW DEFAULT 6 Decelerate 139,7 3 094,2 40,0 DC95HW DEFAULT 7 Decelerate 30,0 0,0 10,0 DC9Q7 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC9Q7 DEFAULT 2 Descend 5 3 000,0 150,2 3,0 DC9Q7 DEFAULT 3 Descend U-15 1 500,0 140,2 3,0 DC9Q7 DEFAULT 4 Descend D-35 1 000,0 130,2 3,0 DC9Q7 DEFAULT 5 Land D-35 357,3 DC9Q7 DEFAULT 6 Decelerate 123,5 3 215,7 40,0 DC9Q7 DEFAULT 7 Decelerate 30,0 0,0 10,0 DC9Q9 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 DC9Q9 DEFAULT 2 Descend 5 3 000,0 162,5 3,0 DC9Q9 DEFAULT 3 Descend U-15 1 500,0 152,5 3,0 DC9Q9 DEFAULT 4 Descend D-35 1 000,0 142,5 3,0 DC9Q9 DEFAULT 5 Land D-35 325,8 DC9Q9 DEFAULT 6 Decelerate 135,2 2 932,2 40,01.7.2015 EN Official Journal of the European Union L 168/217 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) DC9Q9 DEFAULT 7 Decelerate 30,0 0,0 10,0 DHC6 DEFAULT 1 Descend ZERO 6 000,0 120,0 3,0 DHC6 DEFAULT 2 Descend INTR 3 000,0 80,7 3,0 DHC6 DEFAULT 3 Descend D-INTR 1 500,0 70,7 3,0 DHC6 DEFAULT 4 Descend D-L 1 000,0 60,7 3,0 DHC6 DEFAULT 5 Land D-L 39,6 DHC6 DEFAULT 6 Decelerate 57,6 356,4 40,0 DHC6 DEFAULT 7 Decelerate 30,0 0,0 10,0 DHC6QP DEFAULT 1 Descend ZERO 6 000,0 120,0 3,0 DHC6QP DEFAULT 2 Descend INTR 3 000,0 80,7 3,0 DHC6QP DEFAULT 3 Descend D-INTR 1 500,0 70,7 3,0 DHC6QP DEFAULT 4 Descend D-L 1 000,0 60,7 3,0 DHC6QP DEFAULT 5 Land D-L 39,6 DHC6QP DEFAULT 6 Decelerate 57,6 356,4 40,0 DHC6QP DEFAULT 7 Decelerate 30,0 0,0 10,0 DHC7 DEFAULT 1 Descend ZERO 6 000,0 160,0 3,0 DHC7 DEFAULT 2 Descend 10 3 000,0 116,2 3,0 DHC7 DEFAULT 3 Descend D-INTR 1 500,0 106,2 3,0 DHC7 DEFAULT 4 Descend D-25 1 000,0 96,2 3,0 DHC7 DEFAULT 5 Land D-25 98,1 DHC7 DEFAULT 6 Decelerate 91,3 882,9 40,0 DHC7 DEFAULT 7 Decelerate 30,0 0,0 10,0L 168/218 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) DHC8 DEFAULT 1 Descend ZERO 6 000,0 165,0 3,0 DHC8 DEFAULT 2 Descend 5 3 000,0 109,0 3,0 DHC8 DEFAULT 3 Descend D-15 1 500,0 96,0 3,0 DHC8 DEFAULT 4 Descend D-35 1 000,0 89,0 3,0 DHC8 DEFAULT 5 Land D-35 174,6 DHC8 DEFAULT 6 Decelerate 84,4 1 571,4 24,6 DHC8 DEFAULT 7 Decelerate 30,0 0,0 4,1 DHC830 DEFAULT 1 Descend ZERO 6 000,0 179,0 3,0 DHC830 DEFAULT 2 Descend 10 3 000,0 128,0 3,0 DHC830 DEFAULT 3 Descend D-15 1 500,0 116,9 3,0 DHC830 DEFAULT 4 Descend D-35 1 000,0 108,0 3,0 DHC830 DEFAULT 5 Land D-35 219,6 DHC830 DEFAULT 6 Decelerate 102,5 1 976,4 26,1 DHC830 DEFAULT 7 Decelerate 30,0 0,0 4,4 DO228 DEFAULT 1 Descend ZERO-A 6 000,0 200,0 3,0 DO228 DEFAULT 2 Descend ZERO-A 4 000,0 160,0 3,0 DO228 DEFAULT 3 Descend ZERO-A 2 000,0 120,0 3,0 DO228 DEFAULT 4 Descend F30APP 1 000,0 100,0 3,0 DO228 DEFAULT 5 Descend F30APP 50,0 88,0 3,0 DO228 DEFAULT 6 Land F30APP 100,0 DO228 DEFAULT 7 Decelerate 80,0 1 320,9 10,0 DO228 DEFAULT 8 Decelerate 30,0 0,0 10,01.7.2015 EN Official Journal of the European Union L 168/219 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) DO328 DEFAULT 1 Descend ZERO-A 6 000,0 200,0 3,0 DO328 DEFAULT 2 Descend ZERO-A 4 000,0 175,0 3,0 DO328 DEFAULT 3 Descend ZERO-A 2 000,0 150,0 3,0 DO328 DEFAULT 4 Descend F32APP 1 000,0 109,0 3,0 DO328 DEFAULT 5 Descend F32APP 500,0 109,0 3,0 DO328 DEFAULT 6 Land F32APP 50,0 DO328 DEFAULT 7 Decelerate 109,0 2 216,0 10,0 DO328 DEFAULT 8 Decelerate 30,0 0,0 10,0 ECLIPSE500 DEFAULT 1 Descend A_T_DN 6 000,0 170,0 3,0 ECLIPSE500 DEFAULT 2 Descend A_T_DN 5 000,0 160,0 3,0 ECLIPSE500 DEFAULT 3 Descend A_A_DN 3 000,0 100,4 3,0 ECLIPSE500 DEFAULT 4 Descend A_A_DN 2 000,0 100,4 3,0 ECLIPSE500 DEFAULT 5 Descend A_A_DN 1 000,0 100,4 3,0 ECLIPSE500 DEFAULT 6 Descend A_A_DN 100,0 90,4 3,0 ECLIPSE500 DEFAULT 7 Land A_A_DN 144,0 ECLIPSE500 DEFAULT 8 Decelerate 70,0 1 291,0 10,0 ECLIPSE500 DEFAULT 9 Decelerate 20,0 0,0 10,0 EMB120 DEFAULT 1 Descend ZERO 6 000,0 141,5 3,0 EMB120 DEFAULT 2 Descend 15 3 000,0 132,3 3,0 EMB120 DEFAULT 3 Descend D-25 1 500,0 127,4 3,0 EMB120 DEFAULT 4 Descend D-45 1 000,0 119,3 3,0 EMB120 DEFAULT 5 Land D-45 95,0L 168/220 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) EMB120 DEFAULT 6 Decelerate 116,1 855,0 40,0 EMB120 DEFAULT 7 Decelerate 30,0 0,0 10,0 EMB145 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 EMB145 DEFAULT 2 Descend D-22 3 000,0 150,0 3,0 EMB145 DEFAULT 3 Descend D-45 1 500,0 140,0 3,0 EMB145 DEFAULT 4 Descend D-45 1 000,0 134,0 3,0 EMB145 DEFAULT 5 Land D-45 285,5 EMB145 DEFAULT 6 Decelerate 130,0 2 569,5 40,0 EMB145 DEFAULT 7 Decelerate 30,0 0,0 10,0 EMB14L DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 EMB14L DEFAULT 2 Descend D-22 1 500,0 140,0 3,0 EMB14L DEFAULT 3 Descend D-45 1 000,0 140,0 3,0 EMB14L DEFAULT 4 Descend D-45 500,0 138,0 3,0 EMB14L DEFAULT 5 Land D-45 285,5 EMB14L DEFAULT 6 Decelerate 132,0 2 569,5 40,0 EMB14L DEFAULT 7 Decelerate 30,0 0,0 10,0 EMB170 DEFAULT 1 Descend-Idle 6 000,0 250,0 3,0 EMB170 DEFAULT 2 Descend-Idle 3 000,0 180,0 3,0 EMB170 DEFAULT 3 Descend-Idle 2 000,0 140,0 3,0 EMB170 DEFAULT 4 Descend FULL 1 500,0 130,0 3,0 EMB170 DEFAULT 5 Land FULL 267,2 EMB170 DEFAULT 6 Decelerate 120,0 2 405,0 40,01.7.2015 EN Official Journal of the European Union L 168/221 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) EMB170 DEFAULT 7 Decelerate 30,0 0,0 10,0 EMB175 DEFAULT 1 Descend-Idle 6 000,0 250,0 3,0 EMB175 DEFAULT 2 Descend-Idle 3 000,0 180,0 3,0 EMB175 DEFAULT 3 Descend-Idle 2 000,0 140,0 3,0 EMB175 DEFAULT 4 Descend FULL 1 500,0 130,0 3,0 EMB175 DEFAULT 5 Land FULL 276,3 EMB175 DEFAULT 6 Decelerate 120,0 2 487,0 40,0 EMB175 DEFAULT 7 Decelerate 30,0 0,0 10,0 EMB190 DEFAULT 1 Descend-Idle 6 000,0 250,0 3,0 EMB190 DEFAULT 2 Descend- 3 000,0 180,0 3,0 Idle EMB190 DEFAULT 3 Descend- 2 000,0 140,0 3,0 Idle EMB190 DEFAULT 4 Descend FULL 1 500,0 130,0 3,0 EMB190 DEFAULT 5 Land FULL 271,9 EMB190 DEFAULT 6 Decelerate 120,0 2 447,0 40,0 EMB190 DEFAULT 7 Decelerate 30,0 0,0 10,0 EMB195 DEFAULT 1 Descend-Idle 6 000,0 250,0 3,0 EMB195 DEFAULT 2 Descend-Idle 3 000,0 180,0 3,0 EMB195 DEFAULT 3 Descend- 2 000,0 140,0 3,0 Idle EMB195 DEFAULT 4 Descend FULL 1 500,0 130,0 3,0 EMB195 DEFAULT 5 Land FULL 281,1 EMB195 DEFAULT 6 Decelerate 120,0 2 530,0 40,0 EMB195 DEFAULT 7 Decelerate 30,0 0,0 10,0L 168/222 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) F10062 DEFAULT 1 Descend TO 6 000,0 250,0 3,0 F10062 DEFAULT 2 Descend INT2 3 000,0 161,3 3,0 F10062 DEFAULT 3 Descend U-INT 1 500,0 141,3 3,0 F10062 DEFAULT 4 Descend D-42 1 000,0 131,3 3,0 F10062 DEFAULT 5 Land D-42 315,0 F10062 DEFAULT 6 Decelerate 124,5 2 835,0 40,0 F10062 DEFAULT 7 Decelerate 30,0 0,0 10,0 F10065 DEFAULT 1 Descend TO 6 000,0 250,0 3,0 F10065 DEFAULT 2 Descend INT2 3 000,0 163,1 3,0 F10065 DEFAULT 3 Descend U-INT 1 500,0 143,1 3,0 F10065 DEFAULT 4 Descend D-42 1 000,0 133,1 3,0 F10065 DEFAULT 5 Land D-42 328,0 F10065 DEFAULT 6 Decelerate 126,3 2 952,0 40,0 F10065 DEFAULT 7 Decelerate 30,0 0,0 10,0 F28MK2 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 F28MK2 DEFAULT 2 Descend INT2 3 000,0 152,9 3,0 F28MK2 DEFAULT 3 Descend U-INTR 1 500,0 132,9 3,0 F28MK2 DEFAULT 4 Descend D-42 1 000,0 122,9 3,0 F28MK2 DEFAULT 5 Land D-42 223,2 F28MK2 DEFAULT 6 Decelerate 116,6 2 008,8 40,0 F28MK2 DEFAULT 7 Decelerate 30,0 0,0 10,0 F28MK4 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,01.7.2015 EN Official Journal of the European Union L 168/223 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) F28MK4 DEFAULT 2 Descend INT2 3 000,0 153,6 3,0 F28MK4 DEFAULT 3 Descend U-INTR 1 500,0 133,6 3,0 F28MK4 DEFAULT 4 Descend D-42 1 000,0 123,6 3,0 F28MK4 DEFAULT 5 Land D-42 223,7 F28MK4 DEFAULT 6 Decelerate 117,2 2 013,3 40,0 F28MK4 DEFAULT 7 Decelerate 30,0 0,0 10,0 FAL20 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 FAL20 DEFAULT 2 Descend INTR 3 000,0 142,2 3,0 FAL20 DEFAULT 3 Descend D-25 1 500,0 126,1 3,0 FAL20 DEFAULT 4 Descend D-40 1 000,0 124,2 3,0 FAL20 DEFAULT 5 Land D-40 128,7 FAL20 DEFAULT 6 Decelerate 117,9 1 158,3 40,0 FAL20 DEFAULT 7 Decelerate 30,0 0,0 10,0 GII DEFAULT 1 Descend L-0-U 6 000,0 230,0 3,0 GII DEFAULT 2 Descend L-10-U 3 000,0 170,0 3,0 GII DEFAULT 3 Descend L-20-D 1 500,0 153,6 3,0 GII DEFAULT 4 Descend L-20-D 1 000,0 153,6 3,0 GII DEFAULT 5 Descend L-39-D 200,0 143,6 3,0 GII DEFAULT 6 Land L-39-D 790,0 GII DEFAULT 7 Decelerate 117,0 760,0 40,0 GII DEFAULT 8 Decelerate 20,0 0,0 10,0 GIIB DEFAULT 1 Descend L-0-U 6 000,0 230,0 3,0L 168/224 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) GIIB DEFAULT 2 Descend L-10-U 3 000,0 170,0 3,0 GIIB DEFAULT 3 Descend L-20-D 1 500,0 149,2 3,0 GIIB DEFAULT 4 Descend L-20-D 1 000,0 149,2 3,0 GIIB DEFAULT 5 Descend L-39-D 200,0 139,2 3,0 GIIB DEFAULT 6 Land L-39-D 790,0 GIIB DEFAULT 7 Decelerate 113,0 760,0 40,0 GIIB DEFAULT 8 Decelerate 20,0 0,0 10,0 GIV DEFAULT 1 Descend L-0-U 6 000,0 250,0 3,0 GIV DEFAULT 2 Descend L-0-U 3 000,0 160,0 3,0 GIV DEFAULT 3 Descend L-20-D 1 500,0 160,0 3,0 GIV DEFAULT 4 Descend L-39-D 1 000,0 151,5 3,0 GIV DEFAULT 5 Land L-39-D 298,0 GIV DEFAULT 6 Decelerate 80,0 982,0 40,0 GIV DEFAULT 7 Decelerate 20,0 0,0 4,0 GV DEFAULT 1 Descend L-0-U 6 000,0 250,0 3,0 GV DEFAULT 2 Descend L-20-U 3 000,0 160,0 3,0 GV DEFAULT 3 Descend L-20-D 1 500,0 160,0 3,0 GV DEFAULT 4 Descend L-39-D 1 000,0 137,8 3,0 GV DEFAULT 5 Land L-39-D 300,0 GV DEFAULT 6 Decelerate 107,0 1 157,0 40,0 GV DEFAULT 7 Decelerate 20,0 0,0 4,6 HS748A DEFAULT 1 Descend ZERO 6 000,0 160,0 3,01.7.2015 EN Official Journal of the European Union L 168/225 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) HS748A DEFAULT 2 Descend INTR 3 000,0 110,1 3,0 HS748A DEFAULT 3 Descend D-INTR 1 500,0 100,1 3,0 HS748A DEFAULT 4 Descend D-30 1 000,0 90,1 3,0 HS748A DEFAULT 5 Land D-30 207,0 HS748A DEFAULT 6 Decelerate 85,5 1 863,0 40,0 HS748A DEFAULT 7 Decelerate 30,0 0,0 10,0 IA1125 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 IA1125 DEFAULT 2 Descend INTR 3 000,0 152,1 3,0 IA1125 DEFAULT 3 Descend D-INTR 1 500,0 142,1 3,0 IA1125 DEFAULT 4 Descend D-40 1 000,0 132,1 3,0 IA1125 DEFAULT 5 Land D-40 236,6 IA1125 DEFAULT 6 Decelerate 125,3 2 129,4 40,0 IA1125 DEFAULT 7 Decelerate 30,0 0,0 10,0 L1011 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 L1011 DEFAULT 2 Descend 10 3 000,0 160,5 3,0 L1011 DEFAULT 3 Descend D-33 1 500,0 162,9 3,0 L1011 DEFAULT 4 Descend D-42 1 000,0 145,5 3,0 L1011 DEFAULT 5 Land D-42 417,0 L1011 DEFAULT 6 Decelerate 138,1 3 753,0 10,0 L1011 DEFAULT 7 Decelerate 30,0 0,0 10,0 L10115 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 L10115 DEFAULT 2 Descend 10 3 000,0 162,4 3,0L 168/226 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) L10115 DEFAULT 3 Descend D-33 1 500,0 151,2 3,0 L10115 DEFAULT 4 Descend D-42 1 000,0 147,4 3,0 L10115 DEFAULT 5 Land D-42 516,6 L10115 DEFAULT 6 Decelerate 139,8 4 649,4 10,0 L10115 DEFAULT 7 Decelerate 30,0 0,0 10,0 L188 DEFAULT 1 Descend ZERO 6 000,0 200,0 3,0 L188 DEFAULT 2 Descend INTR 3 000,0 147,5 3,0 L188 DEFAULT 3 Descend D-78-% 1 500,0 135,6 3,0 L188 DEFAULT 4 Descend D-100 1 000,0 129,8 3,0 L188 DEFAULT 5 Land D-100 351,0 L188 DEFAULT 6 Decelerate 123,1 3 159,0 40,0 L188 DEFAULT 7 Decelerate 30,0 0,0 10,0 LEAR25 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 LEAR25 DEFAULT 2 Descend 10 3 000,0 161,6 3,0 LEAR25 DEFAULT 3 Descend D-INTR 1 500,0 151,6 3,0 LEAR25 DEFAULT 4 Descend D-40 1 000,0 141,7 3,0 LEAR25 DEFAULT 5 Land D-40 140,4 LEAR25 DEFAULT 6 Decelerate 134,4 1 263,6 40,0 LEAR25 DEFAULT 7 Decelerate 30,0 0,0 10,0 LEAR35 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 LEAR35 DEFAULT 2 Descend 10 3 000,0 144,5 3,0 LEAR35 DEFAULT 3 Descend D-INTR 1 500,0 134,5 3,01.7.2015 EN Official Journal of the European Union L 168/227 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) LEAR35 DEFAULT 4 Descend D-40 1 000,0 127,8 3,0 LEAR35 DEFAULT 5 Land D-40 181,4 LEAR35 DEFAULT 6 Decelerate 121,2 1 632,6 40,0 LEAR35 DEFAULT 7 Decelerate 30,0 0,0 10,0 MD9025 DEFAULT 1 Descend U-0 6 000,0 185,0 3,0 MD9025 DEFAULT 2 Descend D-28 3 000,0 154,0 3,0 MD9025 DEFAULT 3 Descend D-28 1 500,0 150,0 3,0 MD9025 DEFAULT 4 Descend D-40 1 000,0 145,3 3,0 MD9025 DEFAULT 5 Land D-40 346,0 MD9025 DEFAULT 6 Decelerate 130,0 2 100,0 40,0 MD9025 DEFAULT 7 Decelerate 30,0 0,0 9,6 MD9028 DEFAULT 1 Descend U-0 6 000,0 185,0 3,0 MD9028 DEFAULT 2 Descend D-28 3 000,0 154,0 3,0 MD9028 DEFAULT 3 Descend D-28 1 500,0 150,0 3,0 MD9028 DEFAULT 4 Descend D-40 1 000,0 145,3 3,0 MD9028 DEFAULT 5 Land D-40 346,0 MD9028 DEFAULT 6 Decelerate 130,0 2 100,0 40,0 MD9028 DEFAULT 7 Decelerate 30,0 0,0 8,6 MU3001 DEFAULT 1 Descend ZERO 6 000,0 250,0 3,0 MU3001 DEFAULT 2 Descend 1 3 000,0 133,8 3,0 MU3001 DEFAULT 3 Descend D-INTR 1 500,0 123,8 3,0 MU3001 DEFAULT 4 Descend D-30 1 000,0 117,1 3,0L 168/228 EN Official Journal of the European Union 1.7.2015 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) MU3001 DEFAULT 5 Land D-30 156,6 MU3001 DEFAULT 6 Decelerate 111,1 1 409,4 40,0 MU3001 DEFAULT 7 Decelerate 30,0 0,0 10,0 PA30 DEFAULT 1 Descend ZERO-A 6 000,0 120,0 3,0 PA30 DEFAULT 2 Descend 27-A 3 000,0 109,0 3,0 PA30 DEFAULT 3 Descend 27-A 1 500,0 96,0 3,0 PA30 DEFAULT 4 Descend 27-A 1 000,0 87,0 3,0 PA30 DEFAULT 5 Land 27-A 53,5 PA30 DEFAULT 6 Decelerate 70,0 481,1 10,0 PA30 DEFAULT 7 Decelerate 10,0 0,0 10,0 PA42 DEFAULT 1 Descend ZERO-A 6 000,0 151,0 3,0 PA42 DEFAULT 2 Descend ZERO-A 4 000,0 135,0 3,0 PA42 DEFAULT 3 Descend ZERO-A 2 000,0 119,0 3,0 PA42 DEFAULT 4 Descend 30-DN 1 000,0 111,0 3,0 PA42 DEFAULT 5 Descend 30-DN 50,0 111,0 3,0 PA42 DEFAULT 6 Land 30-DN 100,0 PA42 DEFAULT 7 Decelerate 111,0 2 245,9 10,0 PA42 DEFAULT 8 Decelerate 10,0 0,0 10,0 SD330 DEFAULT 1 Descend ZERO 6 000,0 160,0 3,0 SD330 DEFAULT 2 Descend INTR 3 000,0 120,2 3,0 SD330 DEFAULT 3 Descend D-15 1 500,0 106,5 3,0 SD330 DEFAULT 4 Descend D-35 1 000,0 100,2 3,01.7.2015 EN Official Journal of the European Union L 168/229 Descent Start Thrust Step Start Alti­ Start Touchdown ACFTID Profile_ID Step type Flap_ID Angle Distance (ft) (% Max number tude (ft) CAS (kt) Roll (ft) (deg) thrust) SD330 DEFAULT 5 Land D-35 233,1 SD330 DEFAULT 6 Decelerate 95,1 2 097,9 40,0 SD330 DEFAULT 7 Decelerate 30,0 0,0 10,0 SF340 DEFAULT 1 Descend ZERO 6 000,0 160,0 3,0 SF340 DEFAULT 2 Descend 5 3 000,0 136,9 3,0 SF340 DEFAULT 3 Descend D-INTR 1 500,0 126,9 3,0 SF340 DEFAULT 4 Descend D-35 1 000,0 116,9 3,0 SF340 DEFAULT 5 Land D-35 216,9 SF340 DEFAULT 6 Decelerate 110,9 1 952,1 40,0 SF340 DEFAULT 7 Decelerate 30,0 0,0 10,0 Table I-4 (part 1) Default departures procedural steps Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 1900D DEFAULT 1 1 Takeoff MaxTakeoff 17-D 1900D DEFAULT 1 2 Climb MaxTakeoff 17-D 400 1900D DEFAULT 1 3 Accelerate MaxTakeoff 17-D 2 750 128 1900D DEFAULT 1 4 Accelerate MaxClimb ZERO-D 2 950 138 1900D DEFAULT 1 5 Climb MaxClimb ZERO-D 3 000 1900D DEFAULT 1 6 Accelerate MaxClimb ZERO-D 1 500 160 1900D DEFAULT 1 7 Climb MaxClimb ZERO-D 5 500 1900D DEFAULT 1 8 Climb MaxClimb ZERO-D 7 500 1900D DEFAULT 1 9 Climb MaxClimb ZERO-D 10 000L 168/230 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 1900D DEFAULT 2 1 Takeoff MaxTakeoff 17-D 1900D DEFAULT 2 2 Climb MaxTakeoff 17-D 400 1900D DEFAULT 2 3 Accelerate MaxTakeoff 17-D 2 400 128 1900D DEFAULT 2 4 Accelerate MaxClimb ZERO-D 2 650 138 1900D DEFAULT 2 5 Climb MaxClimb ZERO-D 3 000 1900D DEFAULT 2 6 Accelerate MaxClimb ZERO-D 1 500 160 1900D DEFAULT 2 7 Climb MaxClimb ZERO-D 5 500 1900D DEFAULT 2 8 Climb MaxClimb ZERO-D 7 500 1900D DEFAULT 2 9 Climb MaxClimb ZERO-D 10 000 707320 DEFAULT 1 1 Takeoff MaxTakeoff 14 707320 DEFAULT 1 2 Climb MaxTakeoff 14 1 000 707320 DEFAULT 1 3 Accelerate MaxTakeoff 14 2 047 175 707320 DEFAULT 1 4 Accelerate MaxClimb INT 1 000 195 707320 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 707320 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 000 250 707320 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 707320 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 707320 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 707320 DEFAULT 2 1 Takeoff MaxTakeoff 14 707320 DEFAULT 2 2 Climb MaxTakeoff 14 1 0001.7.2015 EN Official Journal of the European Union L 168/231 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 707320 DEFAULT 2 3 Accelerate MaxTakeoff 14 1 905 179 707320 DEFAULT 2 4 Accelerate MaxClimb INT 1 000 199 707320 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 707320 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 000 250 707320 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 707320 DEFAULT 2 8 Climb MaxClimb ZERO 7 500 707320 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 707320 DEFAULT 3 1 Takeoff MaxTakeoff 14 707320 DEFAULT 3 2 Climb MaxTakeoff 14 1 000 707320 DEFAULT 3 3 Accelerate MaxTakeoff 14 1 793 183 707320 DEFAULT 3 4 Accelerate MaxClimb INT 1 000 203 707320 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 707320 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 000 250 707320 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 707320 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 707320 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 707320 DEFAULT 4 1 Takeoff MaxTakeoff 14 707320 DEFAULT 4 2 Climb MaxTakeoff 14 1 000 707320 DEFAULT 4 3 Accelerate MaxTakeoff 14 1 624 189 707320 DEFAULT 4 4 Accelerate MaxClimb INT 1 000 209L 168/232 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 707320 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 707320 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 000 250 707320 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 707320 DEFAULT 4 8 Climb MaxClimb ZERO 7 500 707320 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 707320 DEFAULT 5 1 Takeoff MaxTakeoff 14 707320 DEFAULT 5 2 Climb MaxTakeoff 14 1 000 707320 DEFAULT 5 3 Accelerate MaxTakeoff 14 1 430 197 707320 DEFAULT 5 4 Accelerate MaxClimb INT 1 000 217 707320 DEFAULT 5 5 Climb MaxClimb ZERO 3 000 707320 DEFAULT 5 6 Accelerate MaxClimb ZERO 1 000 250 707320 DEFAULT 5 7 Climb MaxClimb ZERO 5 500 707320 DEFAULT 5 8 Climb MaxClimb ZERO 7 500 707320 DEFAULT 5 9 Climb MaxClimb ZERO 10 000 707320 DEFAULT 6 1 Takeoff MaxTakeoff 14 707320 DEFAULT 6 2 Climb MaxTakeoff 14 1 000 707320 DEFAULT 6 3 Accelerate MaxTakeoff 14 1 259 205 707320 DEFAULT 6 4 Accelerate MaxClimb INT 800 225 707320 DEFAULT 6 5 Climb MaxClimb ZERO 3 000 707320 DEFAULT 6 6 Accelerate MaxClimb ZERO 800 2501.7.2015 EN Official Journal of the European Union L 168/233 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 707320 DEFAULT 6 7 Climb MaxClimb ZERO 5 500 707320 DEFAULT 6 8 Climb MaxClimb ZERO 7 500 707320 DEFAULT 6 9 Climb MaxClimb ZERO 10 000 707320 DEFAULT 7 1 Takeoff MaxTakeoff 14 707320 DEFAULT 7 2 Climb MaxTakeoff 14 1 000 707320 DEFAULT 7 3 Accelerate MaxTakeoff 14 1 151 209 707320 DEFAULT 7 4 Accelerate MaxClimb INT 800 229 707320 DEFAULT 7 5 Climb MaxClimb ZERO 3 000 707320 DEFAULT 7 6 Accelerate MaxClimb ZERO 800 250 707320 DEFAULT 7 7 Climb MaxClimb ZERO 5 500 707320 DEFAULT 7 8 Climb MaxClimb ZERO 7 500 707320 DEFAULT 7 9 Climb MaxClimb ZERO 10 000 707QN DEFAULT 1 1 Takeoff MaxTakeoff 14 707QN DEFAULT 1 2 Climb MaxTakeoff 14 1 000 707QN DEFAULT 1 3 Accelerate MaxTakeoff 14 2 047 175 707QN DEFAULT 1 4 Accelerate MaxClimb INT 1 000 195 707QN DEFAULT 1 5 Climb MaxClimb ZERO 3 000 707QN DEFAULT 1 6 Accelerate MaxClimb ZERO 1 000 250 707QN DEFAULT 1 7 Climb MaxClimb ZERO 5 500 707QN DEFAULT 1 8 Climb MaxClimb ZERO 7 500L 168/234 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 707QN DEFAULT 1 9 Climb MaxClimb ZERO 10 000 707QN DEFAULT 2 1 Takeoff MaxTakeoff 14 707QN DEFAULT 2 2 Climb MaxTakeoff 14 1 000 707QN DEFAULT 2 3 Accelerate MaxTakeoff 14 1 905 179 707QN DEFAULT 2 4 Accelerate MaxClimb INT 1 000 199 707QN DEFAULT 2 5 Climb MaxClimb ZERO 3 000 707QN DEFAULT 2 6 Accelerate MaxClimb ZERO 1 000 250 707QN DEFAULT 2 7 Climb MaxClimb ZERO 5 500 707QN DEFAULT 2 8 Climb MaxClimb ZERO 7 500 707QN DEFAULT 2 9 Climb MaxClimb ZERO 10 000 707QN DEFAULT 3 1 Takeoff MaxTakeoff 14 707QN DEFAULT 3 2 Climb MaxTakeoff 14 1 000 707QN DEFAULT 3 3 Accelerate MaxTakeoff 14 1 793 183 707QN DEFAULT 3 4 Accelerate MaxClimb INT 1 000 203 707QN DEFAULT 3 5 Climb MaxClimb ZERO 3 000 707QN DEFAULT 3 6 Accelerate MaxClimb ZERO 1 000 250 707QN DEFAULT 3 7 Climb MaxClimb ZERO 5 500 707QN DEFAULT 3 8 Climb MaxClimb ZERO 7 500 707QN DEFAULT 3 9 Climb MaxClimb ZERO 10 000 707QN DEFAULT 4 1 Takeoff MaxTakeoff 141.7.2015 EN Official Journal of the European Union L 168/235 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 707QN DEFAULT 4 2 Climb MaxTakeoff 14 1 000 707QN DEFAULT 4 3 Accelerate MaxTakeoff 14 1 624 189 707QN DEFAULT 4 4 Accelerate MaxClimb INT 1 000 209 707QN DEFAULT 4 5 Climb MaxClimb ZERO 3 000 707QN DEFAULT 4 6 Accelerate MaxClimb ZERO 1 000 250 707QN DEFAULT 4 7 Climb MaxClimb ZERO 5 500 707QN DEFAULT 4 8 Climb MaxClimb ZERO 7 500 707QN DEFAULT 4 9 Climb MaxClimb ZERO 10 000 707QN DEFAULT 5 1 Takeoff MaxTakeoff 14 707QN DEFAULT 5 2 Climb MaxTakeoff 14 1 000 707QN DEFAULT 5 3 Accelerate MaxTakeoff 14 1 430 197 707QN DEFAULT 5 4 Accelerate MaxClimb INT 1 000 217 707QN DEFAULT 5 5 Climb MaxClimb ZERO 3 000 707QN DEFAULT 5 6 Accelerate MaxClimb ZERO 1 000 250 707QN DEFAULT 5 7 Climb MaxClimb ZERO 5 500 707QN DEFAULT 5 8 Climb MaxClimb ZERO 7 500 707QN DEFAULT 5 9 Climb MaxClimb ZERO 10 000 707QN DEFAULT 6 1 Takeoff MaxTakeoff 14 707QN DEFAULT 6 2 Climb MaxTakeoff 14 1 000 707QN DEFAULT 6 3 Accelerate MaxTakeoff 14 1 259 205L 168/236 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 707QN DEFAULT 6 4 Accelerate MaxClimb INT 800 225 707QN DEFAULT 6 5 Climb MaxClimb ZERO 3 000 707QN DEFAULT 6 6 Accelerate MaxClimb ZERO 800 250 707QN DEFAULT 6 7 Climb MaxClimb ZERO 5 500 707QN DEFAULT 6 8 Climb MaxClimb ZERO 7 500 707QN DEFAULT 6 9 Climb MaxClimb ZERO 10 000 707QN DEFAULT 7 1 Takeoff MaxTakeoff 14 707QN DEFAULT 7 2 Climb MaxTakeoff 14 1 000 707QN DEFAULT 7 3 Accelerate MaxTakeoff 14 1 151 209 707QN DEFAULT 7 4 Accelerate MaxClimb INT 800 229 707QN DEFAULT 7 5 Climb MaxClimb ZERO 3 000 707QN DEFAULT 7 6 Accelerate MaxClimb ZERO 800 250 707QN DEFAULT 7 7 Climb MaxClimb ZERO 5 500 707QN DEFAULT 7 8 Climb MaxClimb ZERO 7 500 707QN DEFAULT 7 9 Climb MaxClimb ZERO 10 000 717200 DEFAULT 1 1 Takeoff MaxTakeoff T_13A 717200 DEFAULT 1 2 Climb MaxTakeoff T_13A 1 000 717200 DEFAULT 1 3 Climb MaxClimb T_13A 3 000 717200 DEFAULT 1 4 Accelerate MaxClimb T_00B 1 296,4 250 717200 DEFAULT 1 5 Climb MaxClimb T_00B 5 000 717200 DEFAULT 1 6 Climb MaxClimb T_00B 7 5001.7.2015 EN Official Journal of the European Union L 168/237 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 717200 DEFAULT 1 7 Climb MaxClimb T_00B 10 000 717200 DEFAULT 2 1 Takeoff MaxTakeoff T_13A 717200 DEFAULT 2 2 Climb MaxTakeoff T_13A 1 000 717200 DEFAULT 2 3 Climb MaxClimb T_13A 3 000 717200 DEFAULT 2 4 Accelerate MaxClimb T_00B 1 298 250 717200 DEFAULT 2 5 Climb MaxClimb T_00B 5 000 717200 DEFAULT 2 6 Climb MaxClimb T_00B 7 500 717200 DEFAULT 2 7 Climb MaxClimb T_00B 10 000 717200 DEFAULT 3 1 Takeoff MaxTakeoff T_13A 717200 DEFAULT 3 2 Climb MaxTakeoff T_13A 1 000 717200 DEFAULT 3 3 Climb MaxClimb T_13A 3 000 717200 DEFAULT 3 4 Accelerate MaxClimb T_00B 1 229,1 250 717200 DEFAULT 3 5 Climb MaxClimb T_00B 5 000 717200 DEFAULT 3 6 Climb MaxClimb T_00B 7 500 717200 DEFAULT 3 7 Climb MaxClimb T_00B 10 000 717200 DEFAULT 4 1 Takeoff MaxTakeoff T_13A 717200 DEFAULT 4 2 Climb MaxTakeoff T_13A 1 000 717200 DEFAULT 4 3 Climb MaxClimb T_13A 3 000 717200 DEFAULT 4 4 Accelerate MaxClimb T_00B 1 165,9 250 717200 DEFAULT 4 5 Climb MaxClimb T_00B 5 000 717200 DEFAULT 4 6 Climb MaxClimb T_00B 7 500L 168/238 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 717200 DEFAULT 4 7 Climb MaxClimb T_00B 10 000 717200 DEFAULT 5 1 Takeoff MaxTakeoff T_13A 717200 DEFAULT 5 2 Climb MaxTakeoff T_13A 1 000 717200 DEFAULT 5 3 Climb MaxClimb T_13A 3 000 717200 DEFAULT 5 4 Accelerate MaxClimb T_00B 1 142,6 250 717200 DEFAULT 5 5 Climb MaxClimb T_00B 5 000 717200 DEFAULT 5 6 Climb MaxClimb T_00B 7 500 717200 DEFAULT 5 7 Climb MaxClimb T_00B 10 000 717200 DEFAULT 6 1 Takeoff MaxTakeoff T_13A 717200 DEFAULT 6 2 Climb MaxTakeoff T_13A 1 000 717200 DEFAULT 6 3 Climb MaxClimb T_13A 3 000 717200 DEFAULT 6 4 Accelerate MaxClimb T_00B 1 098,3 250 717200 DEFAULT 6 5 Climb MaxClimb T_00B 5 000 717200 DEFAULT 6 6 Climb MaxClimb T_00B 7 500 717200 DEFAULT 6 7 Climb MaxClimb T_00B 10 000 717200 ICAO_B 1 1 Takeoff MaxTakeoff T_13A 717200 ICAO_B 1 2 Climb MaxTakeoff T_13A 1 100 717200 ICAO_B 1 3 Accelerate MaxTakeoff T_13A 2 137,1 186,2 717200 ICAO_B 1 4 Climb MaxClimb T_00B 3 000 717200 ICAO_B 1 5 Accelerate MaxClimb T_00B 1 000 2501.7.2015 EN Official Journal of the European Union L 168/239 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 717200 ICAO_B 1 6 Climb MaxClimb T_00B 5 500 717200 ICAO_B 1 7 Climb MaxClimb T_00B 7 500 717200 ICAO_B 1 8 Climb MaxClimb T_00B 10 000 717200 ICAO_B 2 1 Takeoff MaxTakeoff T_13A 717200 ICAO_B 2 2 Climb MaxTakeoff T_13A 1 000 717200 ICAO_B 2 3 Accelerate MaxTakeoff T_13A 2 003,2 185 717200 ICAO_B 2 4 Climb MaxClimb T_00B 3 000 717200 ICAO_B 2 5 Accelerate MaxClimb T_00B 1 000 250 717200 ICAO_B 2 6 Climb MaxClimb T_00B 5 500 717200 ICAO_B 2 7 Climb MaxClimb T_00B 7 500 717200 ICAO_B 2 8 Climb MaxClimb T_00B 10 000 717200 ICAO_B 3 1 Takeoff MaxTakeoff T_13A 717200 ICAO_B 3 2 Climb MaxTakeoff T_13A 1 000 717200 ICAO_B 3 3 Accelerate MaxTakeoff T_13A 1 874,4 183,8 717200 ICAO_B 3 4 Climb MaxClimb T_00B 3 000 717200 ICAO_B 3 5 Accelerate MaxClimb T_00B 1 000 250 717200 ICAO_B 3 6 Climb MaxClimb T_00B 5 500 717200 ICAO_B 3 7 Climb MaxClimb T_00B 7 500 717200 ICAO_B 3 8 Climb MaxClimb T_00B 10 000 717200 ICAO_B 4 1 Takeoff MaxTakeoff T_13AL 168/240 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 717200 ICAO_B 4 2 Climb MaxTakeoff T_13A 1 000 717200 ICAO_B 4 3 Accelerate MaxTakeoff T_13A 1 756,2 182,7 717200 ICAO_B 4 4 Climb MaxClimb T_00B 3 000 717200 ICAO_B 4 5 Accelerate MaxClimb T_00B 1 000 250 717200 ICAO_B 4 6 Climb MaxClimb T_00B 5 500 717200 ICAO_B 4 7 Climb MaxClimb T_00B 7 500 717200 ICAO_B 4 8 Climb MaxClimb T_00B 10 000 717200 ICAO_B 5 1 Takeoff MaxTakeoff T_13A 717200 ICAO_B 5 2 Climb MaxTakeoff T_13A 1 000 717200 ICAO_B 5 3 Accelerate MaxTakeoff T_13A 1 705,9 192,7 717200 ICAO_B 5 4 Climb MaxClimb T_00B 3 000 717200 ICAO_B 5 5 Accelerate MaxClimb T_00B 1 000 250 717200 ICAO_B 5 6 Climb MaxClimb T_00B 5 500 717200 ICAO_B 5 7 Climb MaxClimb T_00B 7 500 717200 ICAO_B 5 8 Climb MaxClimb T_00B 10 000 717200 ICAO_B 6 1 Takeoff MaxTakeoff T_13A 717200 ICAO_B 6 2 Climb MaxTakeoff T_13A 1 000 717200 ICAO_B 6 3 Accelerate MaxTakeoff T_13A 1 540,3 191,2 717200 ICAO_B 6 4 Climb MaxClimb T_00B 3 000 717200 ICAO_B 6 5 Accelerate MaxClimb T_00B 1 000 2501.7.2015 EN Official Journal of the European Union L 168/241 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 717200 ICAO_B 6 6 Climb MaxClimb T_00B 5 500 717200 ICAO_B 6 7 Climb MaxClimb T_00B 7 500 717200 ICAO_B 6 8 Climb MaxClimb T_00B 10 000 720B DEFAULT 1 1 Takeoff MaxTakeoff 20 720B DEFAULT 1 2 Climb MaxTakeoff 20 1 000 720B DEFAULT 1 3 Accelerate MaxTakeoff 20 2 632 175 720B DEFAULT 1 4 Accelerate MaxClimb INT 1 000 195 720B DEFAULT 1 5 Climb MaxClimb ZERO 3 000 720B DEFAULT 1 6 Accelerate MaxClimb ZERO 1 000 250 720B DEFAULT 1 7 Climb MaxClimb ZERO 5 500 720B DEFAULT 1 8 Climb MaxClimb ZERO 7 500 720B DEFAULT 1 9 Climb MaxClimb ZERO 10 000 720B DEFAULT 2 1 Takeoff MaxTakeoff 20 720B DEFAULT 2 2 Climb MaxTakeoff 20 1 000 720B DEFAULT 2 3 Accelerate MaxTakeoff 20 2 470 179 720B DEFAULT 2 4 Accelerate MaxClimb INT 1 000 199 720B DEFAULT 2 5 Climb MaxClimb ZERO 3 000 720B DEFAULT 2 6 Accelerate MaxClimb ZERO 1 000 250 720B DEFAULT 2 7 Climb MaxClimb ZERO 5 500 720B DEFAULT 2 8 Climb MaxClimb ZERO 7 500L 168/242 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 720B DEFAULT 2 9 Climb MaxClimb ZERO 10 000 720B DEFAULT 3 1 Takeoff MaxTakeoff 20 720B DEFAULT 3 2 Climb MaxTakeoff 20 1 000 720B DEFAULT 3 3 Accelerate MaxTakeoff 20 2 323 183 720B DEFAULT 3 4 Accelerate MaxClimb INT 1 000 203 720B DEFAULT 3 5 Climb MaxClimb ZERO 3 000 720B DEFAULT 3 6 Accelerate MaxClimb ZERO 1 000 250 720B DEFAULT 3 7 Climb MaxClimb ZERO 5 500 720B DEFAULT 3 8 Climb MaxClimb ZERO 7 500 720B DEFAULT 3 9 Climb MaxClimb ZERO 10 000 720B DEFAULT 4 1 Takeoff MaxTakeoff 20 720B DEFAULT 4 2 Climb MaxTakeoff 20 1 000 720B DEFAULT 4 3 Accelerate MaxTakeoff 20 2 125 189 720B DEFAULT 4 4 Accelerate MaxClimb INT 1 000 209 720B DEFAULT 4 5 Climb MaxClimb ZERO 3 000 720B DEFAULT 4 6 Accelerate MaxClimb ZERO 1 000 250 720B DEFAULT 4 7 Climb MaxClimb ZERO 5 500 720B DEFAULT 4 8 Climb MaxClimb ZERO 7 500 720B DEFAULT 4 9 Climb MaxClimb ZERO 10 000 720B DEFAULT 5 1 Takeoff MaxTakeoff 201.7.2015 EN Official Journal of the European Union L 168/243 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 720B DEFAULT 5 2 Climb MaxTakeoff 20 1 000 720B DEFAULT 5 3 Accelerate MaxTakeoff 20 2 005 193 720B DEFAULT 5 4 Accelerate MaxClimb INT 1 000 213 720B DEFAULT 5 5 Climb MaxClimb ZERO 3 000 720B DEFAULT 5 6 Accelerate MaxClimb ZERO 1 000 250 720B DEFAULT 5 7 Climb MaxClimb ZERO 5 500 720B DEFAULT 5 8 Climb MaxClimb ZERO 7 500 720B DEFAULT 5 9 Climb MaxClimb ZERO 10 000 727100 DEFAULT 1 1 Takeoff MaxTakeoff 5 727100 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 727100 DEFAULT 1 3 Accelerate MaxTakeoff 5 1 342 160 727100 DEFAULT 1 4 Accelerate MaxTakeoff 2 1 342 190 727100 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 200 727100 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 727100 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 727100 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 727100 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 727100 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 727100 DEFAULT 2 1 Takeoff MaxTakeoff 5 727100 DEFAULT 2 2 Climb MaxTakeoff 5 1 000L 168/244 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727100 DEFAULT 2 3 Accelerate MaxTakeoff 5 1 265 160 727100 DEFAULT 2 4 Accelerate MaxTakeoff 2 1 265 190 727100 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 200 727100 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 727100 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 727100 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 727100 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 727100 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 727100 DEFAULT 3 1 Takeoff MaxTakeoff 5 727100 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 727100 DEFAULT 3 3 Accelerate MaxTakeoff 5 1 192 165 727100 DEFAULT 3 4 Accelerate MaxTakeoff 2 1 192 195 727100 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 205 727100 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 727100 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 727100 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 727100 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 727100 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 727100 DEFAULT 4 1 Takeoff MaxTakeoff 5 727100 DEFAULT 4 2 Climb MaxTakeoff 5 1 0001.7.2015 EN Official Journal of the European Union L 168/245 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727100 DEFAULT 4 3 Accelerate MaxTakeoff 5 1 115 170 727100 DEFAULT 4 4 Accelerate MaxTakeoff 2 1 115 200 727100 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 210 727100 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 727100 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 727100 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 727100 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 727100 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 727D15 DEFAULT 1 1 Takeoff MaxTakeoff 5 727D15 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 727D15 DEFAULT 1 3 Accelerate MaxTakeoff 5 1 363 170 727D15 DEFAULT 1 4 Accelerate MaxTakeoff 2 1 363 200 727D15 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 210 727D15 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 727D15 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 727D15 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 727D15 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 727D15 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 727D15 DEFAULT 2 1 Takeoff MaxTakeoff 5 727D15 DEFAULT 2 2 Climb MaxTakeoff 5 1 000L 168/246 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727D15 DEFAULT 2 3 Accelerate MaxTakeoff 5 1 281 170 727D15 DEFAULT 2 4 Accelerate MaxTakeoff 2 1 281 200 727D15 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 210 727D15 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 727D15 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 727D15 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 727D15 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 727D15 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 727D15 DEFAULT 3 1 Takeoff MaxTakeoff 5 727D15 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 727D15 DEFAULT 3 3 Accelerate MaxTakeoff 5 1 177 175 727D15 DEFAULT 3 4 Accelerate MaxTakeoff 2 1 177 205 727D15 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 215 727D15 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 727D15 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 727D15 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 727D15 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 727D15 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 727D15 DEFAULT 4 1 Takeoff MaxTakeoff 5 727D15 DEFAULT 4 2 Climb MaxTakeoff 5 1 0001.7.2015 EN Official Journal of the European Union L 168/247 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727D15 DEFAULT 4 3 Accelerate MaxTakeoff 5 1 057 180 727D15 DEFAULT 4 4 Accelerate MaxTakeoff 2 1 057 210 727D15 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 220 727D15 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 727D15 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 727D15 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 727D15 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 727D15 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 727D15 DEFAULT 5 1 Takeoff MaxTakeoff 5 727D15 DEFAULT 5 2 Climb MaxTakeoff 5 1 000 727D15 DEFAULT 5 3 Accelerate MaxTakeoff 2 941 210 727D15 DEFAULT 5 4 Accelerate MaxClimb ZERO 1 000 220 727D15 DEFAULT 5 5 Climb MaxClimb ZERO 3 000 727D15 DEFAULT 5 6 Accelerate MaxClimb ZERO 1 000 250 727D15 DEFAULT 5 7 Climb MaxClimb ZERO 5 500 727D15 DEFAULT 5 8 Climb MaxClimb ZERO 7 500 727D15 DEFAULT 5 9 Climb MaxClimb ZERO 10 000 727D17 DEFAULT 1 1 Takeoff MaxTakeoff 5 727D17 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 727D17 DEFAULT 1 3 Accelerate MaxTakeoff 5 1 465 170L 168/248 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727D17 DEFAULT 1 4 Accelerate MaxTakeoff 2 1 465 200 727D17 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 210 727D17 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 727D17 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 727D17 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 727D17 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 727D17 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 727D17 DEFAULT 2 1 Takeoff MaxTakeoff 5 727D17 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 727D17 DEFAULT 2 3 Accelerate MaxTakeoff 5 1 340 175 727D17 DEFAULT 2 4 Accelerate MaxTakeoff 2 1 340 205 727D17 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 215 727D17 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 727D17 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 727D17 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 727D17 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 727D17 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 727D17 DEFAULT 3 1 Takeoff MaxTakeoff 5 727D17 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 727D17 DEFAULT 3 3 Accelerate MaxTakeoff 5 1 236 1801.7.2015 EN Official Journal of the European Union L 168/249 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727D17 DEFAULT 3 4 Accelerate MaxTakeoff 2 1 236 210 727D17 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 220 727D17 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 727D17 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 727D17 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 727D17 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 727D17 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 727D17 DEFAULT 4 1 Takeoff MaxTakeoff 5 727D17 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 727D17 DEFAULT 4 3 Accelerate MaxTakeoff 5 1 158 180 727D17 DEFAULT 4 4 Accelerate MaxTakeoff 2 1 158 210 727D17 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 220 727D17 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 727D17 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 727D17 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 727D17 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 727D17 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 727EM1 DEFAULT 1 1 Takeoff MaxTakeoff 5 727EM1 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 727EM1 DEFAULT 1 3 Accelerate MaxTakeoff 5 1 342 160L 168/250 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727EM1 DEFAULT 1 4 Accelerate MaxTakeoff 2 1 342 190 727EM1 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 200 727EM1 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 727EM1 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 727EM1 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 727EM1 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 727EM1 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 727EM1 DEFAULT 2 1 Takeoff MaxTakeoff 5 727EM1 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 727EM1 DEFAULT 2 3 Accelerate MaxTakeoff 5 1 265 160 727EM1 DEFAULT 2 4 Accelerate MaxTakeoff 2 1 265 190 727EM1 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 200 727EM1 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 727EM1 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 727EM1 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 727EM1 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 727EM1 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 727EM1 DEFAULT 3 1 Takeoff MaxTakeoff 5 727EM1 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 727EM1 DEFAULT 3 3 Accelerate MaxTakeoff 5 1 192 1651.7.2015 EN Official Journal of the European Union L 168/251 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727EM1 DEFAULT 3 4 Accelerate MaxTakeoff 2 1 192 195 727EM1 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 205 727EM1 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 727EM1 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 727EM1 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 727EM1 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 727EM1 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 727EM1 DEFAULT 4 1 Takeoff MaxTakeoff 5 727EM1 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 727EM1 DEFAULT 4 3 Accelerate MaxTakeoff 5 1 115 170 727EM1 DEFAULT 4 4 Accelerate MaxTakeoff 2 1 115 200 727EM1 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 210 727EM1 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 727EM1 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 727EM1 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 727EM1 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 727EM1 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 727EM2 DEFAULT 1 1 Takeoff MaxTakeoff 5 727EM2 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 727EM2 DEFAULT 1 3 Accelerate MaxTakeoff 5 1 363 170L 168/252 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727EM2 DEFAULT 1 4 Accelerate MaxTakeoff 2 1 363 200 727EM2 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 210 727EM2 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 727EM2 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 727EM2 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 727EM2 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 727EM2 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 727EM2 DEFAULT 2 1 Takeoff MaxTakeoff 5 727EM2 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 727EM2 DEFAULT 2 3 Accelerate MaxTakeoff 5 1 281 170 727EM2 DEFAULT 2 4 Accelerate MaxTakeoff 2 1 281 200 727EM2 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 210 727EM2 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 727EM2 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 727EM2 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 727EM2 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 727EM2 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 727EM2 DEFAULT 3 1 Takeoff MaxTakeoff 5 727EM2 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 727EM2 DEFAULT 3 3 Accelerate MaxTakeoff 5 1 177 1751.7.2015 EN Official Journal of the European Union L 168/253 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727EM2 DEFAULT 3 4 Accelerate MaxTakeoff 2 1 177 205 727EM2 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 215 727EM2 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 727EM2 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 727EM2 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 727EM2 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 727EM2 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 727EM2 DEFAULT 4 1 Takeoff MaxTakeoff 5 727EM2 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 727EM2 DEFAULT 4 3 Accelerate MaxTakeoff 5 1 057 180 727EM2 DEFAULT 4 4 Accelerate MaxTakeoff 2 1 057 210 727EM2 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 220 727EM2 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 727EM2 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 727EM2 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 727EM2 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 727EM2 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 727EM2 DEFAULT 5 1 Takeoff MaxTakeoff 5 727EM2 DEFAULT 5 2 Climb MaxTakeoff 5 1 000 727EM2 DEFAULT 5 3 Accelerate MaxTakeoff 2 941 210L 168/254 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727EM2 DEFAULT 5 4 Accelerate MaxClimb ZERO 1 000 220 727EM2 DEFAULT 5 5 Climb MaxClimb ZERO 3 000 727EM2 DEFAULT 5 6 Accelerate MaxClimb ZERO 1 000 250 727EM2 DEFAULT 5 7 Climb MaxClimb ZERO 5 500 727EM2 DEFAULT 5 8 Climb MaxClimb ZERO 7 500 727EM2 DEFAULT 5 9 Climb MaxClimb ZERO 10 000 727Q15 DEFAULT 1 1 Takeoff MaxTakeoff 5 727Q15 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 727Q15 DEFAULT 1 3 Accelerate MaxTakeoff 5 1 363 170 727Q15 DEFAULT 1 4 Accelerate MaxTakeoff 2 1 363 200 727Q15 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 210 727Q15 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 727Q15 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 727Q15 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 727Q15 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 727Q15 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 727Q15 DEFAULT 2 1 Takeoff MaxTakeoff 5 727Q15 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 727Q15 DEFAULT 2 3 Accelerate MaxTakeoff 5 1 281 170 727Q15 DEFAULT 2 4 Accelerate MaxTakeoff 2 1 281 2001.7.2015 EN Official Journal of the European Union L 168/255 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727Q15 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 210 727Q15 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 727Q15 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 727Q15 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 727Q15 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 727Q15 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 727Q15 DEFAULT 3 1 Takeoff MaxTakeoff 5 727Q15 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 727Q15 DEFAULT 3 3 Accelerate MaxTakeoff 5 1 177 175 727Q15 DEFAULT 3 4 Accelerate MaxTakeoff 2 1 177 205 727Q15 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 215 727Q15 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 727Q15 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 727Q15 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 727Q15 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 727Q15 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 727Q15 DEFAULT 4 1 Takeoff MaxTakeoff 5 727Q15 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 727Q15 DEFAULT 4 3 Accelerate MaxTakeoff 5 1 057 180 727Q15 DEFAULT 4 4 Accelerate MaxTakeoff 2 1 057 210L 168/256 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727Q15 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 220 727Q15 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 727Q15 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 727Q15 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 727Q15 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 727Q15 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 727Q15 DEFAULT 5 1 Takeoff MaxTakeoff 5 727Q15 DEFAULT 5 2 Climb MaxTakeoff 5 1 000 727Q15 DEFAULT 5 3 Accelerate MaxTakeoff 2 941 210 727Q15 DEFAULT 5 4 Accelerate MaxClimb ZERO 1 000 220 727Q15 DEFAULT 5 5 Climb MaxClimb ZERO 3 000 727Q15 DEFAULT 5 6 Accelerate MaxClimb ZERO 1 000 250 727Q15 DEFAULT 5 7 Climb MaxClimb ZERO 5 500 727Q15 DEFAULT 5 8 Climb MaxClimb ZERO 7 500 727Q15 DEFAULT 5 9 Climb MaxClimb ZERO 10 000 727Q7 DEFAULT 1 1 Takeoff MaxTakeoff 5 727Q7 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 727Q7 DEFAULT 1 3 Accelerate MaxTakeoff 5 1 342 160 727Q7 DEFAULT 1 4 Accelerate MaxTakeoff 2 1 342 190 727Q7 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 2001.7.2015 EN Official Journal of the European Union L 168/257 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727Q7 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 727Q7 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 727Q7 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 727Q7 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 727Q7 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 727Q7 DEFAULT 2 1 Takeoff MaxTakeoff 5 727Q7 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 727Q7 DEFAULT 2 3 Accelerate MaxTakeoff 5 1 265 160 727Q7 DEFAULT 2 4 Accelerate MaxTakeoff 2 1 265 190 727Q7 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 200 727Q7 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 727Q7 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 727Q7 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 727Q7 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 727Q7 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 727Q7 DEFAULT 3 1 Takeoff MaxTakeoff 5 727Q7 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 727Q7 DEFAULT 3 3 Accelerate MaxTakeoff 5 1 192 165 727Q7 DEFAULT 3 4 Accelerate MaxTakeoff 2 1 192 195 727Q7 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 205L 168/258 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727Q7 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 727Q7 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 727Q7 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 727Q7 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 727Q7 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 727Q7 DEFAULT 4 1 Takeoff MaxTakeoff 5 727Q7 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 727Q7 DEFAULT 4 3 Accelerate MaxTakeoff 5 1 115 170 727Q7 DEFAULT 4 4 Accelerate MaxTakeoff 2 1 115 200 727Q7 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 210 727Q7 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 727Q7 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 727Q7 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 727Q7 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 727Q7 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 727Q9 DEFAULT 1 1 Takeoff MaxTakeoff 5 727Q9 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 727Q9 DEFAULT 1 3 Accelerate MaxTakeoff 5 1 539 170 727Q9 DEFAULT 1 4 Accelerate MaxTakeoff 2 1 539 200 727Q9 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 2101.7.2015 EN Official Journal of the European Union L 168/259 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727Q9 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 727Q9 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 727Q9 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 727Q9 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 727Q9 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 727Q9 DEFAULT 2 1 Takeoff MaxTakeoff 5 727Q9 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 727Q9 DEFAULT 2 3 Accelerate MaxTakeoff 5 1 390 170 727Q9 DEFAULT 2 4 Accelerate MaxTakeoff 2 1 390 200 727Q9 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 210 727Q9 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 727Q9 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 727Q9 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 727Q9 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 727Q9 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 727Q9 DEFAULT 3 1 Takeoff MaxTakeoff 5 727Q9 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 727Q9 DEFAULT 3 3 Accelerate MaxTakeoff 5 1 255 180 727Q9 DEFAULT 3 4 Accelerate MaxTakeoff 2 1 255 210 727Q9 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 220L 168/260 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727Q9 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 727Q9 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 727Q9 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 727Q9 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 727Q9 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 727Q9 DEFAULT 4 1 Takeoff MaxTakeoff 5 727Q9 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 727Q9 DEFAULT 4 3 Accelerate MaxTakeoff 2 855 210 727Q9 DEFAULT 4 4 Accelerate MaxClimb ZERO 1 000 220 727Q9 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 727Q9 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 000 250 727Q9 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 727Q9 DEFAULT 4 8 Climb MaxClimb ZERO 7 500 727Q9 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 727QF DEFAULT 1 1 Takeoff MaxTakeoff 5 727QF DEFAULT 1 2 Climb MaxTakeoff 5 1 000 727QF DEFAULT 1 3 Accelerate MaxTakeoff 5 1 000 175 727QF DEFAULT 1 4 Accelerate MaxTakeoff 2 1 000 190 727QF DEFAULT 1 5 Accelerate MaxTakeoff ZERO 1 000 200 727QF DEFAULT 1 6 Climb MaxContin­ ZERO 3 000 uous1.7.2015 EN Official Journal of the European Union L 168/261 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727QF DEFAULT 1 7 Accelerate MaxContin­ ZERO 1 000 250 uous 727QF DEFAULT 1 8 Climb MaxClimb ZERO 5 500 727QF DEFAULT 1 9 Climb MaxClimb ZERO 7 500 727QF DEFAULT 1 10 Climb MaxClimb ZERO 10 000 727QF DEFAULT 2 1 Takeoff MaxTakeoff 5 727QF DEFAULT 2 2 Climb MaxTakeoff 5 1 000 727QF DEFAULT 2 3 Accelerate MaxTakeoff 5 1 000 180 727QF DEFAULT 2 4 Accelerate MaxTakeoff 2 1 000 190 727QF DEFAULT 2 5 Accelerate MaxTakeoff ZERO 1 000 200 727QF DEFAULT 2 6 Climb MaxContin­ ZERO 3 000 uous 727QF DEFAULT 2 7 Accelerate MaxContin­ ZERO 1 000 250 uous 727QF DEFAULT 2 8 Climb MaxClimb ZERO 5 500 727QF DEFAULT 2 9 Climb MaxClimb ZERO 7 500 727QF DEFAULT 2 10 Climb MaxClimb ZERO 10 000 727QF DEFAULT 3 1 Takeoff MaxTakeoff 5 727QF DEFAULT 3 2 Climb MaxTakeoff 5 1 000 727QF DEFAULT 3 3 Accelerate MaxTakeoff 5 1 000 184 727QF DEFAULT 3 4 Accelerate MaxTakeoff 2 1 000 190 727QF DEFAULT 3 5 Accelerate MaxTakeoff ZERO 1 000 200 727QF DEFAULT 3 6 Climb MaxContin­ ZERO 3 000 uousL 168/262 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 727QF DEFAULT 3 7 Accelerate MaxContin­ ZERO 1 000 250 uous 727QF DEFAULT 3 8 Climb MaxClimb ZERO 5 500 727QF DEFAULT 3 9 Climb MaxClimb ZERO 7 500 727QF DEFAULT 3 10 Climb MaxClimb ZERO 10 000 727QF DEFAULT 4 1 Takeoff MaxTakeoff 5 727QF DEFAULT 4 2 Climb MaxTakeoff 5 1 000 727QF DEFAULT 4 3 Accelerate MaxTakeoff 5 1 000 189 727QF DEFAULT 4 4 Accelerate MaxTakeoff 2 1 000 190 727QF DEFAULT 4 5 Accelerate MaxTakeoff ZERO 1 000 200 727QF DEFAULT 4 6 Climb MaxContin­ ZERO 3 000 uous 727QF DEFAULT 4 7 Accelerate MaxContin­ ZERO 1 000 250 uous 727QF DEFAULT 4 8 Climb MaxClimb ZERO 5 500 727QF DEFAULT 4 9 Climb MaxClimb ZERO 7 500 727QF DEFAULT 4 10 Climb MaxClimb ZERO 10 000 737 DEFAULT 1 1 Takeoff MaxTakeoff 5 737 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 737 DEFAULT 1 3 Accelerate MaxTakeoff 5 2 090 146 737 DEFAULT 1 4 Accelerate MaxTakeoff INT 1 568 171 737 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 210 737 DEFAULT 1 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/263 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 737 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 737 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 737 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 737 DEFAULT 2 1 Takeoff MaxTakeoff 5 737 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 737 DEFAULT 2 3 Accelerate MaxTakeoff 5 2 014 149 737 DEFAULT 2 4 Accelerate MaxTakeoff INT 1 511 174 737 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 210 737 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 737 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 737 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 737 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 737 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 737 DEFAULT 3 1 Takeoff MaxTakeoff 5 737 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 737 DEFAULT 3 3 Accelerate MaxTakeoff 5 1 851 154 737 DEFAULT 3 4 Accelerate MaxTakeoff INT 1 388 179 737 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 210 737 DEFAULT 3 6 Climb MaxClimb ZERO 3 000L 168/264 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 737 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 737 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 737 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 737 DEFAULT 4 1 Takeoff MaxTakeoff 5 737 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 737 DEFAULT 4 3 Accelerate MaxTakeoff 5 1 685 160 737 DEFAULT 4 4 Accelerate MaxTakeoff INT 1 264 185 737 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 210 737 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 737 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 737 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 737 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 737 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 737300 DEFAULT 1 1 Takeoff MaxTakeoff 5 737300 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 737300 DEFAULT 1 3 Accelerate MaxClimb 5 1 483,4 187,9 737300 DEFAULT 1 4 Accelerate MaxClimb 1 1 684,6 205,5 737300 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 815,6 220,5 737300 DEFAULT 1 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/265 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737300 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 892,6 250 737300 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 737300 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 737300 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 737300 DEFAULT 2 1 Takeoff MaxTakeoff 5 737300 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 737300 DEFAULT 2 3 Accelerate MaxClimb 5 1 398,8 189,2 737300 DEFAULT 2 4 Accelerate MaxClimb 1 1 579,3 204,5 737300 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 700,5 220,5 737300 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 737300 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 774,1 250 737300 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 737300 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 737300 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 737300 DEFAULT 3 1 Takeoff MaxTakeoff 5 737300 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 737300 DEFAULT 3 3 Accelerate MaxClimb 5 1 311,5 190,8 737300 DEFAULT 3 4 Accelerate MaxClimb 1 1 487,2 213,2 737300 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 609,4 220,5 737300 DEFAULT 3 6 Climb MaxClimb ZERO 3 000L 168/266 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737300 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 657,6 250 737300 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 737300 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 737300 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 737300 DEFAULT 4 1 Takeoff MaxTakeoff 5 737300 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 737300 DEFAULT 4 3 Accelerate MaxClimb 5 1 154,7 194,6 737300 DEFAULT 4 4 Accelerate MaxClimb 1 1 295,8 211,5 737300 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 391,6 220,5 737300 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 737300 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 444,8 250 737300 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 737300 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 737300 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 737300 ICAO_A 1 1 Takeoff MaxTakeoff 5 737300 ICAO_A 1 2 Climb MaxTakeoff 5 1 500 737300 ICAO_A 1 3 Climb MaxClimb 5 3 000 737300 ICAO_A 1 4 Accelerate MaxClimb 5 1 413,5 184,9 737300 ICAO_A 1 5 Accelerate MaxClimb 1 1 601,4 203,9 737300 ICAO_A 1 6 Accelerate MaxClimb ZERO 1 821,6 2501.7.2015 EN Official Journal of the European Union L 168/267 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737300 ICAO_A 1 7 Climb MaxClimb ZERO 5 500 737300 ICAO_A 1 8 Climb MaxClimb ZERO 7 500 737300 ICAO_A 1 9 Climb MaxClimb ZERO 10 000 737300 ICAO_A 2 1 Takeoff MaxTakeoff 5 737300 ICAO_A 2 2 Climb MaxTakeoff 5 1 500 737300 ICAO_A 2 3 Climb MaxClimb 5 3 000 737300 ICAO_A 2 4 Accelerate MaxClimb 5 1 332,5 186,4 737300 ICAO_A 2 5 Accelerate MaxClimb 1 1 497,1 203 737300 ICAO_A 2 6 Accelerate MaxClimb ZERO 1 705,6 250 737300 ICAO_A 2 7 Climb MaxClimb ZERO 5 500 737300 ICAO_A 2 8 Climb MaxClimb ZERO 7 500 737300 ICAO_A 2 9 Climb MaxClimb ZERO 10 000 737300 ICAO_A 3 1 Takeoff MaxTakeoff 5 737300 ICAO_A 3 2 Climb MaxTakeoff 5 1 500 737300 ICAO_A 3 3 Climb MaxClimb 5 3 000 737300 ICAO_A 3 4 Accelerate MaxClimb 5 1 247,9 188,2 737300 ICAO_A 3 5 Accelerate MaxClimb 1 1 415,3 211,7 737300 ICAO_A 3 6 Accelerate MaxClimb ZERO 1 609,9 250 737300 ICAO_A 3 7 Climb MaxClimb ZERO 5 500 737300 ICAO_A 3 8 Climb MaxClimb ZERO 7 500L 168/268 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737300 ICAO_A 3 9 Climb MaxClimb ZERO 10 000 737300 ICAO_A 4 1 Takeoff MaxTakeoff 5 737300 ICAO_A 4 2 Climb MaxTakeoff 5 1 500 737300 ICAO_A 4 3 Climb MaxClimb 5 3 000 737300 ICAO_A 4 4 Accelerate MaxClimb 5 1 093,3 192,2 737300 ICAO_A 4 5 Accelerate MaxClimb 1 1 223,7 210,2 737300 ICAO_A 4 6 Accelerate MaxClimb ZERO 1 399,1 250 737300 ICAO_A 4 7 Climb MaxClimb ZERO 5 500 737300 ICAO_A 4 8 Climb MaxClimb ZERO 7 500 737300 ICAO_A 4 9 Climb MaxClimb ZERO 10 000 737300 ICAO_B 1 1 Takeoff MaxTakeoff 5 737300 ICAO_B 1 2 Climb MaxTakeoff 5 1 000 737300 ICAO_B 1 3 Accelerate MaxTakeoff 5 1 560,7 189,3 737300 ICAO_B 1 4 Accelerate MaxTakeoff 1 1 765,5 206,2 737300 ICAO_B 1 5 Accelerate MaxTakeoff ZERO 1 897 220,5 737300 ICAO_B 1 6 Climb MaxClimb ZERO 3 000 737300 ICAO_B 1 7 Accelerate MaxClimb ZERO 1 892,6 250 737300 ICAO_B 1 8 Climb MaxClimb ZERO 5 500 737300 ICAO_B 1 9 Climb MaxClimb ZERO 7 500 737300 ICAO_B 1 10 Climb MaxClimb ZERO 10 0001.7.2015 EN Official Journal of the European Union L 168/269 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737300 ICAO_B 2 1 Takeoff MaxTakeoff 5 737300 ICAO_B 2 2 Climb MaxTakeoff 5 1 000 737300 ICAO_B 2 3 Accelerate MaxTakeoff 5 1 468,7 190,5 737300 ICAO_B 2 4 Accelerate MaxTakeoff 1 1 652,2 205,8 737300 ICAO_B 2 5 Accelerate MaxTakeoff ZERO 1 773,2 220,5 737300 ICAO_B 2 6 Climb MaxClimb ZERO 3 000 737300 ICAO_B 2 7 Accelerate MaxClimb ZERO 1 773,3 250 737300 ICAO_B 2 8 Climb MaxClimb ZERO 5 500 737300 ICAO_B 2 9 Climb MaxClimb ZERO 7 500 737300 ICAO_B 2 10 Climb MaxClimb ZERO 10 000 737300 ICAO_B 3 1 Takeoff MaxTakeoff 5 737300 ICAO_B 3 2 Climb MaxTakeoff 5 1 000 737300 ICAO_B 3 3 Accelerate MaxTakeoff 5 1 380,4 192,1 737300 ICAO_B 3 4 Accelerate MaxTakeoff 1 1 557,4 213,8 737300 ICAO_B 3 5 Accelerate MaxTakeoff ZERO 1 688,1 220,5 737300 ICAO_B 3 6 Climb MaxClimb ZERO 3 000 737300 ICAO_B 3 7 Accelerate MaxClimb ZERO 1 657,6 250 737300 ICAO_B 3 8 Climb MaxClimb ZERO 5 500 737300 ICAO_B 3 9 Climb MaxClimb ZERO 7 500 737300 ICAO_B 3 10 Climb MaxClimb ZERO 10 000L 168/270 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737300 ICAO_B 4 1 Takeoff MaxTakeoff 5 737300 ICAO_B 4 2 Climb MaxTakeoff 5 1 000 737300 ICAO_B 4 3 Accelerate MaxTakeoff 5 1 217,8 195,7 737300 ICAO_B 4 4 Accelerate MaxTakeoff 1 1 361,4 212 737300 ICAO_B 4 5 Accelerate MaxTakeoff ZERO 1 457,6 220,5 737300 ICAO_B 4 6 Climb MaxClimb ZERO 3 000 737300 ICAO_B 4 7 Accelerate MaxClimb ZERO 1 444,8 250 737300 ICAO_B 4 8 Climb MaxClimb ZERO 5 500 737300 ICAO_B 4 9 Climb MaxClimb ZERO 7 500 737300 ICAO_B 4 10 Climb MaxClimb ZERO 10 000 7373B2 DEFAULT 1 1 Takeoff MaxTakeoff 5 7373B2 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 7373B2 DEFAULT 1 3 Accelerate MaxClimb T_05 1 671,2 191,9 7373B2 DEFAULT 1 4 Accelerate MaxClimb T_01 1 900 209,1 7373B2 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 7373B2 DEFAULT 1 6 Accelerate MaxClimb ZERO 2 058,2 250 7373B2 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 7373B2 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 7373B2 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 7373B2 DEFAULT 2 1 Takeoff MaxTakeoff 51.7.2015 EN Official Journal of the European Union L 168/271 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7373B2 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 7373B2 DEFAULT 2 3 Accelerate MaxClimb T_05 1 575,5 192,6 7373B2 DEFAULT 2 4 Accelerate MaxClimb T_01 1 786 208,8 7373B2 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 7373B2 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 934,6 250 7373B2 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 7373B2 DEFAULT 2 8 Climb MaxClimb ZERO 7 500 7373B2 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 7373B2 DEFAULT 3 1 Takeoff MaxTakeoff 5 7373B2 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 7373B2 DEFAULT 3 3 Accelerate MaxClimb T_05 1 483,2 194 7373B2 DEFAULT 3 4 Accelerate MaxClimb T_01 1 675,9 215,3 7373B2 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 7373B2 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 828,7 250 7373B2 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 7373B2 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 7373B2 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 7373B2 DEFAULT 4 1 Takeoff MaxTakeoff 5 7373B2 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 7373B2 DEFAULT 4 3 Accelerate MaxClimb T_05 1 314,1 197,8L 168/272 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7373B2 DEFAULT 4 4 Accelerate MaxClimb T_01 1 478,4 213,5 7373B2 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 7373B2 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 597,8 250 7373B2 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 7373B2 DEFAULT 4 8 Climb MaxClimb ZERO 7 500 7373B2 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 7373B2 DEFAULT M 1 Takeoff MaxTakeoff 5 7373B2 DEFAULT M 2 Climb MaxTakeoff 5 1 000 7373B2 DEFAULT M 3 Accelerate MaxClimb T_05 1 214,7 200,6 7373B2 DEFAULT M 4 Accelerate MaxClimb T_01 1 372,5 222,3 7373B2 DEFAULT M 5 Climb MaxClimb ZERO 3 000 7373B2 DEFAULT M 6 Accelerate MaxClimb ZERO 1 493,4 250 7373B2 DEFAULT M 7 Climb MaxClimb ZERO 5 500 7373B2 DEFAULT M 8 Climb MaxClimb ZERO 7 500 7373B2 DEFAULT M 9 Climb MaxClimb ZERO 10 000 7373B2 ICAO_A 1 1 Takeoff MaxTakeoff 5 7373B2 ICAO_A 1 2 Climb MaxTakeoff 5 1 500 7373B2 ICAO_A 1 3 Climb MaxClimb 5 3 000 7373B2 ICAO_A 1 4 Accelerate MaxClimb T_05 1 607,4 188,9 7373B2 ICAO_A 1 5 Accelerate MaxClimb T_01 1 827,6 2061.7.2015 EN Official Journal of the European Union L 168/273 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7373B2 ICAO_A 1 6 Accelerate MaxClimb ZERO 2 030,2 250 7373B2 ICAO_A 1 7 Climb MaxClimb ZERO 5 500 7373B2 ICAO_A 1 8 Climb MaxClimb ZERO 7 500 7373B2 ICAO_A 1 9 Climb MaxClimb ZERO 10 000 7373B2 ICAO_A 2 1 Takeoff MaxTakeoff 5 7373B2 ICAO_A 2 2 Climb MaxTakeoff 5 1 500 7373B2 ICAO_A 2 3 Climb MaxClimb 5 3 000 7373B2 ICAO_A 2 4 Accelerate MaxClimb T_05 1 507,4 188,9 7373B2 ICAO_A 2 5 Accelerate MaxClimb T_01 1 703,4 206 7373B2 ICAO_A 2 6 Accelerate MaxClimb ZERO 1 909,1 250 7373B2 ICAO_A 2 7 Climb MaxClimb ZERO 5 500 7373B2 ICAO_A 2 8 Climb MaxClimb ZERO 7 500 7373B2 ICAO_A 2 9 Climb MaxClimb ZERO 10 000 7373B2 ICAO_A 3 1 Takeoff MaxTakeoff 5 7373B2 ICAO_A 3 2 Climb MaxTakeoff 5 1 500 7373B2 ICAO_A 3 3 Climb MaxClimb 5 3 000 7373B2 ICAO_A 3 4 Accelerate MaxClimb T_05 1 417,2 191,3 7373B2 ICAO_A 3 5 Accelerate MaxClimb T_01 1 604,3 213,7 7373B2 ICAO_A 3 6 Accelerate MaxClimb ZERO 1 807,6 250 7373B2 ICAO_A 3 7 Climb MaxClimb ZERO 5 500L 168/274 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7373B2 ICAO_A 3 8 Climb MaxClimb ZERO 7 500 7373B2 ICAO_A 3 9 Climb MaxClimb ZERO 10 000 7373B2 ICAO_A 4 1 Takeoff MaxTakeoff 5 7373B2 ICAO_A 4 2 Climb MaxTakeoff 5 1 500 7373B2 ICAO_A 4 3 Climb MaxClimb 5 3 000 7373B2 ICAO_A 4 4 Accelerate MaxClimb T_05 1 255,2 195,4 7373B2 ICAO_A 4 5 Accelerate MaxClimb T_01 1 411,8 212,1 7373B2 ICAO_A 4 6 Accelerate MaxClimb ZERO 1 576,8 250 7373B2 ICAO_A 4 7 Climb MaxClimb ZERO 5 500 7373B2 ICAO_A 4 8 Climb MaxClimb ZERO 7 500 7373B2 ICAO_A 4 9 Climb MaxClimb ZERO 10 000 7373B2 ICAO_A M 1 Takeoff MaxTakeoff 5 7373B2 ICAO_A M 2 Climb MaxTakeoff 5 1 500 7373B2 ICAO_A M 3 Climb MaxClimb 5 3 000 7373B2 ICAO_A M 4 Accelerate MaxClimb T_05 1 163,2 198,2 7373B2 ICAO_A M 5 Accelerate MaxClimb T_01 1 309,7 220,9 7373B2 ICAO_A M 6 Accelerate MaxClimb ZERO 1 469,1 250 7373B2 ICAO_A M 7 Climb MaxClimb ZERO 5 500 7373B2 ICAO_A M 8 Climb MaxClimb ZERO 7 500 7373B2 ICAO_A M 9 Climb MaxClimb ZERO 10 0001.7.2015 EN Official Journal of the European Union L 168/275 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7373B2 ICAO_B 1 1 Takeoff MaxTakeoff 5 7373B2 ICAO_B 1 2 Climb MaxTakeoff 5 1 000 7373B2 ICAO_B 1 3 Accelerate MaxTakeoff T_05 1 881 195,6 7373B2 ICAO_B 1 4 Accelerate MaxTakeoff T_01 2 138,5 214,5 7373B2 ICAO_B 1 5 Climb MaxClimb ZERO 3 000 7373B2 ICAO_B 1 6 Accelerate MaxClimb ZERO 2 075,4 250 7373B2 ICAO_B 1 7 Climb MaxClimb ZERO 5 500 7373B2 ICAO_B 1 8 Climb MaxClimb ZERO 7 500 7373B2 ICAO_B 1 9 Climb MaxClimb ZERO 10 000 7373B2 ICAO_B 2 1 Takeoff MaxTakeoff 5 7373B2 ICAO_B 2 2 Climb MaxTakeoff 5 1 000 7373B2 ICAO_B 2 3 Accelerate MaxTakeoff T_05 1 774,2 196,2 7373B2 ICAO_B 2 4 Accelerate MaxTakeoff T_01 2 009,3 214 7373B2 ICAO_B 2 5 Climb MaxClimb ZERO 3 000 7373B2 ICAO_B 2 6 Accelerate MaxClimb ZERO 1 950,7 250 7373B2 ICAO_B 2 7 Climb MaxClimb ZERO 5 500 7373B2 ICAO_B 2 8 Climb MaxClimb ZERO 7 500 7373B2 ICAO_B 2 9 Climb MaxClimb ZERO 10 000 7373B2 ICAO_B 3 1 Takeoff MaxTakeoff 5 7373B2 ICAO_B 3 2 Climb MaxTakeoff 5 1 000L 168/276 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7373B2 ICAO_B 3 3 Accelerate MaxTakeoff T_05 1 674,8 197,4 7373B2 ICAO_B 3 4 Accelerate MaxTakeoff T_01 1 895,7 217 7373B2 ICAO_B 3 5 Climb MaxClimb ZERO 3 000 7373B2 ICAO_B 3 6 Accelerate MaxClimb ZERO 1 835,6 250 7373B2 ICAO_B 3 7 Climb MaxClimb ZERO 5 500 7373B2 ICAO_B 3 8 Climb MaxClimb ZERO 7 500 7373B2 ICAO_B 3 9 Climb MaxClimb ZERO 10 000 7373B2 ICAO_B 4 1 Takeoff MaxTakeoff 5 7373B2 ICAO_B 4 2 Climb MaxTakeoff 5 1 000 7373B2 ICAO_B 4 3 Accelerate MaxTakeoff T_05 1 494,5 200,9 7373B2 ICAO_B 4 4 Accelerate MaxTakeoff T_01 1 672,5 215,5 7373B2 ICAO_B 4 5 Climb MaxClimb ZERO 3 000 7373B2 ICAO_B 4 6 Accelerate MaxClimb ZERO 1 606,9 250 7373B2 ICAO_B 4 7 Climb MaxClimb ZERO 5 500 7373B2 ICAO_B 4 8 Climb MaxClimb ZERO 7 500 7373B2 ICAO_B 4 9 Climb MaxClimb ZERO 10 000 7373B2 ICAO_B M 1 Takeoff MaxTakeoff 5 7373B2 ICAO_B M 2 Climb MaxTakeoff 5 1 000 7373B2 ICAO_B M 3 Accelerate MaxTakeoff T_05 1 387,7 203,4 7373B2 ICAO_B M 4 Accelerate MaxTakeoff T_01 1 557,1 223,71.7.2015 EN Official Journal of the European Union L 168/277 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7373B2 ICAO_B M 5 Climb MaxClimb ZERO 3 000 7373B2 ICAO_B M 6 Accelerate MaxClimb ZERO 1 493,2 250 7373B2 ICAO_B M 7 Climb MaxClimb ZERO 5 500 7373B2 ICAO_B M 8 Climb MaxClimb ZERO 7 500 7373B2 ICAO_B M 9 Climb MaxClimb ZERO 10 000 737400 DEFAULT 1 1 Takeoff MaxTakeoff 5 737400 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 737400 DEFAULT 1 3 Accelerate MaxClimb 5 1 715,3 198,8 737400 DEFAULT 1 4 Accelerate MaxClimb 1 1 894,7 210,5 737400 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 737400 DEFAULT 1 6 Accelerate MaxClimb ZERO 2 067,4 250 737400 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 737400 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 737400 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 737400 DEFAULT 2 1 Takeoff MaxTakeoff 5 737400 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 737400 DEFAULT 2 3 Accelerate MaxClimb 5 1 616 199,8 737400 DEFAULT 2 4 Accelerate MaxClimb 1 1 786,6 210,5 737400 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 737400 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 939,1 250L 168/278 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737400 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 737400 DEFAULT 2 8 Climb MaxClimb ZERO 7 500 737400 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 737400 DEFAULT 3 1 Takeoff MaxTakeoff 5 737400 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 737400 DEFAULT 3 3 Accelerate MaxClimb 5 1 516,6 201 737400 DEFAULT 3 4 Accelerate MaxClimb 1 1 660,9 210,5 737400 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 737400 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 807,5 250 737400 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 737400 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 737400 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 737400 DEFAULT 4 1 Takeoff MaxTakeoff 5 737400 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 737400 DEFAULT 4 3 Accelerate MaxClimb 5 1 370,2 203,9 737400 DEFAULT 4 4 Accelerate MaxClimb 1 1 504,1 210,5 737400 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 737400 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 609,1 250 737400 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 737400 DEFAULT 4 8 Climb MaxClimb ZERO 7 5001.7.2015 EN Official Journal of the European Union L 168/279 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737400 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 737400 DEFAULT M 1 Takeoff MaxTakeoff 5 737400 DEFAULT M 2 Climb MaxTakeoff 5 1 000 737400 DEFAULT M 3 Accelerate MaxClimb 5 1 225,8 207,5 737400 DEFAULT M 4 Accelerate MaxClimb 1 1 312,5 210,5 737400 DEFAULT M 5 Climb MaxClimb ZERO 3 000 737400 DEFAULT M 6 Accelerate MaxClimb ZERO 1 414,3 250 737400 DEFAULT M 7 Climb MaxClimb ZERO 5 500 737400 DEFAULT M 8 Climb MaxClimb ZERO 7 500 737400 DEFAULT M 9 Climb MaxClimb ZERO 10 000 737400 ICAO_A 1 1 Takeoff MaxTakeoff 5 737400 ICAO_A 1 2 Climb MaxTakeoff 5 1 500 737400 ICAO_A 1 3 Climb MaxClimb 5 3 000 737400 ICAO_A 1 4 Accelerate MaxClimb 5 1 641,7 195,7 737400 ICAO_A 1 5 Accelerate MaxClimb 1 1 830 210,1 737400 ICAO_A 1 6 Accelerate MaxClimb ZERO 2 058,4 250 737400 ICAO_A 1 7 Climb MaxClimb ZERO 5 500 737400 ICAO_A 1 8 Climb MaxClimb ZERO 7 500 737400 ICAO_A 1 9 Climb MaxClimb ZERO 10 000 737400 ICAO_A 2 1 Takeoff MaxTakeoff 5L 168/280 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737400 ICAO_A 2 2 Climb MaxTakeoff 5 1 500 737400 ICAO_A 2 3 Climb MaxClimb 5 3 000 737400 ICAO_A 2 4 Accelerate MaxClimb 5 1 546 196,8 737400 ICAO_A 2 5 Accelerate MaxClimb 1 1 702,5 210,1 737400 ICAO_A 2 6 Accelerate MaxClimb ZERO 1 919,2 250 737400 ICAO_A 2 7 Climb MaxClimb ZERO 5 500 737400 ICAO_A 2 8 Climb MaxClimb ZERO 7 500 737400 ICAO_A 2 9 Climb MaxClimb ZERO 10 000 737400 ICAO_A 3 1 Takeoff MaxTakeoff 5 737400 ICAO_A 3 2 Climb MaxTakeoff 5 1 500 737400 ICAO_A 3 3 Climb MaxClimb 5 3 000 737400 ICAO_A 3 4 Accelerate MaxClimb 5 1 446,6 198,2 737400 ICAO_A 3 5 Accelerate MaxClimb 1 1 592,3 210,3 737400 ICAO_A 3 6 Accelerate MaxClimb ZERO 1 789,6 250 737400 ICAO_A 3 7 Climb MaxClimb ZERO 5 500 737400 ICAO_A 3 8 Climb MaxClimb ZERO 7 500 737400 ICAO_A 3 9 Climb MaxClimb ZERO 10 000 737400 ICAO_A 4 1 Takeoff MaxTakeoff 5 737400 ICAO_A 4 2 Climb MaxTakeoff 5 1 500 737400 ICAO_A 4 3 Climb MaxClimb 5 3 0001.7.2015 EN Official Journal of the European Union L 168/281 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737400 ICAO_A 4 4 Accelerate MaxClimb 5 1 303,9 201,3 737400 ICAO_A 4 5 Accelerate MaxClimb 1 1 426,1 210,3 737400 ICAO_A 4 6 Accelerate MaxClimb ZERO 1 598,5 250 737400 ICAO_A 4 7 Climb MaxClimb ZERO 5 500 737400 ICAO_A 4 8 Climb MaxClimb ZERO 7 500 737400 ICAO_A 4 9 Climb MaxClimb ZERO 10 000 737400 ICAO_A M 1 Takeoff MaxTakeoff 5 737400 ICAO_A M 2 Climb MaxTakeoff 5 1 500 737400 ICAO_A M 3 Climb MaxClimb 5 3 000 737400 ICAO_A M 4 Accelerate MaxClimb 5 1 159,5 205,1 737400 ICAO_A M 5 Accelerate MaxClimb 1 1 249,3 210,3 737400 ICAO_A M 6 Accelerate MaxClimb ZERO 1 392,2 250 737400 ICAO_A M 7 Climb MaxClimb ZERO 5 500 737400 ICAO_A M 8 Climb MaxClimb ZERO 7 500 737400 ICAO_A M 9 Climb MaxClimb ZERO 10 000 737400 ICAO_B 1 1 Takeoff MaxTakeoff 5 737400 ICAO_B 1 2 Climb MaxTakeoff 5 1 000 737400 ICAO_B 1 3 Accelerate MaxTakeoff 5 1 869,9 201,5 737400 ICAO_B 1 4 Accelerate MaxTakeoff 1 2 073,3 210,5 737400 ICAO_B 1 5 Climb MaxClimb ZERO 3 000L 168/282 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737400 ICAO_B 1 6 Accelerate MaxClimb ZERO 2 067,4 250 737400 ICAO_B 1 7 Climb MaxClimb ZERO 5 500 737400 ICAO_B 1 8 Climb MaxClimb ZERO 7 500 737400 ICAO_B 1 9 Climb MaxClimb ZERO 10 000 737400 ICAO_B 2 1 Takeoff MaxTakeoff 5 737400 ICAO_B 2 2 Climb MaxTakeoff 5 1 000 737400 ICAO_B 2 3 Accelerate MaxTakeoff 5 1 766,9 202,3 737400 ICAO_B 2 4 Accelerate MaxTakeoff 1 1 945,9 210,5 737400 ICAO_B 2 5 Climb MaxClimb ZERO 3 000 737400 ICAO_B 2 6 Accelerate MaxClimb ZERO 1 939,1 250 737400 ICAO_B 2 7 Climb MaxClimb ZERO 5 500 737400 ICAO_B 2 8 Climb MaxClimb ZERO 7 500 737400 ICAO_B 2 9 Climb MaxClimb ZERO 10 000 737400 ICAO_B 3 1 Takeoff MaxTakeoff 5 737400 ICAO_B 3 2 Climb MaxTakeoff 5 1 000 737400 ICAO_B 3 3 Accelerate MaxTakeoff 5 1 660,1 203,4 737400 ICAO_B 3 4 Accelerate MaxTakeoff 1 1 822,5 210,5 737400 ICAO_B 3 5 Climb MaxClimb ZERO 3 000 737400 ICAO_B 3 6 Accelerate MaxClimb ZERO 1 807,5 250 737400 ICAO_B 3 7 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/283 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737400 ICAO_B 3 8 Climb MaxClimb ZERO 7 500 737400 ICAO_B 3 9 Climb MaxClimb ZERO 10 000 737400 ICAO_B 4 1 Takeoff MaxTakeoff 5 737400 ICAO_B 4 2 Climb MaxTakeoff 5 1 000 737400 ICAO_B 4 3 Accelerate MaxTakeoff 5 1 502,8 206,1 737400 ICAO_B 4 4 Accelerate MaxTakeoff 1 1 644,7 210,5 737400 ICAO_B 4 5 Climb MaxClimb ZERO 3 000 737400 ICAO_B 4 6 Accelerate MaxClimb ZERO 1 610,5 250 737400 ICAO_B 4 7 Climb MaxClimb ZERO 5 500 737400 ICAO_B 4 8 Climb MaxClimb ZERO 7 500 737400 ICAO_B 4 9 Climb MaxClimb ZERO 10 000 737400 ICAO_B M 1 Takeoff MaxTakeoff 5 737400 ICAO_B M 2 Climb MaxTakeoff 5 1 000 737400 ICAO_B M 3 Accelerate MaxTakeoff 5 1 350,9 209,5 737400 ICAO_B M 4 Accelerate MaxTakeoff 1 1 428,6 210,5 737400 ICAO_B M 5 Climb MaxClimb ZERO 3 000 737400 ICAO_B M 6 Accelerate MaxClimb ZERO 1 414,7 250 737400 ICAO_B M 7 Climb MaxClimb ZERO 5 500 737400 ICAO_B M 8 Climb MaxClimb ZERO 7 500 737400 ICAO_B M 9 Climb MaxClimb ZERO 10 000L 168/284 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737500 DEFAULT 1 1 Takeoff MaxTakeoff 5 737500 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 737500 DEFAULT 1 3 Accelerate MaxClimb 5 1 579,1 187 737500 DEFAULT 1 4 Accelerate MaxClimb 1 1 800 206,6 737500 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 737500 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 961,7 250 737500 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 737500 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 737500 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 737500 DEFAULT 2 1 Takeoff MaxTakeoff 5 737500 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 737500 DEFAULT 2 3 Accelerate MaxClimb 5 1 490,8 188 737500 DEFAULT 2 4 Accelerate MaxClimb 1 1 681,3 205,6 737500 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 737500 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 834,4 250 737500 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 737500 DEFAULT 2 8 Climb MaxClimb ZERO 7 500 737500 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 737500 DEFAULT 3 1 Takeoff MaxTakeoff 5 737500 DEFAULT 3 2 Climb MaxTakeoff 5 1 0001.7.2015 EN Official Journal of the European Union L 168/285 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737500 DEFAULT 3 3 Accelerate MaxClimb 5 1 398,8 189,4 737500 DEFAULT 3 4 Accelerate MaxClimb 1 1 572,4 204,5 737500 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 737500 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 713,4 250 737500 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 737500 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 737500 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 737500 DEFAULT 4 1 Takeoff MaxTakeoff 5 737500 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 737500 DEFAULT 4 3 Accelerate MaxClimb 5 1 229,4 192,1 737500 DEFAULT 4 4 Accelerate MaxClimb 1 1 388,1 212,4 737500 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 737500 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 521,8 250 737500 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 737500 DEFAULT 4 8 Climb MaxClimb ZERO 7 500 737500 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 737500 DEFAULT 5 1 Takeoff MaxTakeoff 5 737500 DEFAULT 5 2 Climb MaxTakeoff 5 1 000 737500 DEFAULT 5 3 Accelerate MaxClimb 5 1 211,1 192,4 737500 DEFAULT 5 4 Accelerate MaxClimb 1 1 370,8 212L 168/286 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737500 DEFAULT 5 5 Climb MaxClimb ZERO 3 000 737500 DEFAULT 5 6 Accelerate MaxClimb ZERO 1 503,1 250 737500 DEFAULT 5 7 Climb MaxClimb ZERO 5 500 737500 DEFAULT 5 8 Climb MaxClimb ZERO 7 500 737500 DEFAULT 5 9 Climb MaxClimb ZERO 10 000 737500 DEFAULT M 1 Takeoff MaxTakeoff 5 737500 DEFAULT M 2 Climb MaxTakeoff 5 1 000 737500 DEFAULT M 3 Accelerate MaxClimb 5 1 192,6 192,8 737500 DEFAULT M 4 Accelerate MaxClimb 1 1 343,1 211,9 737500 DEFAULT M 5 Climb MaxClimb ZERO 3 000 737500 DEFAULT M 6 Accelerate MaxClimb ZERO 1 470,2 250 737500 DEFAULT M 7 Climb MaxClimb ZERO 5 500 737500 DEFAULT M 8 Climb MaxClimb ZERO 7 500 737500 DEFAULT M 9 Climb MaxClimb ZERO 10 000 737500 ICAO_A 1 1 Takeoff MaxTakeoff 5 737500 ICAO_A 1 2 Climb MaxTakeoff 5 1 500 737500 ICAO_A 1 3 Climb MaxClimb 5 3 000 737500 ICAO_A 1 4 Accelerate MaxClimb 5 1 509,2 184 737500 ICAO_A 1 5 Accelerate MaxClimb 1 1 725,7 204,8 737500 ICAO_A 1 6 Accelerate MaxClimb ZERO 1 934,3 2501.7.2015 EN Official Journal of the European Union L 168/287 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737500 ICAO_A 1 7 Climb MaxClimb ZERO 5 500 737500 ICAO_A 1 8 Climb MaxClimb ZERO 7 500 737500 ICAO_A 1 9 Climb MaxClimb ZERO 10 000 737500 ICAO_A 2 1 Takeoff MaxTakeoff 5 737500 ICAO_A 2 2 Climb MaxTakeoff 5 1 500 737500 ICAO_A 2 3 Climb MaxClimb 5 3 000 737500 ICAO_A 2 4 Accelerate MaxClimb 5 1 420,9 185,1 737500 ICAO_A 2 5 Accelerate MaxClimb 1 1 612,5 203,9 737500 ICAO_A 2 6 Accelerate MaxClimb ZERO 1 810,3 250 737500 ICAO_A 2 7 Climb MaxClimb ZERO 5 500 737500 ICAO_A 2 8 Climb MaxClimb ZERO 7 500 737500 ICAO_A 2 9 Climb MaxClimb ZERO 10 000 737500 ICAO_A 3 1 Takeoff MaxTakeoff 5 737500 ICAO_A 3 2 Climb MaxTakeoff 5 1 500 737500 ICAO_A 3 3 Climb MaxClimb 5 3 000 737500 ICAO_A 3 4 Accelerate MaxClimb 5 1 332,5 186,6 737500 ICAO_A 3 5 Accelerate MaxClimb 1 1 494,3 203 737500 ICAO_A 3 6 Accelerate MaxClimb ZERO 1 691,3 250 737500 ICAO_A 3 7 Climb MaxClimb ZERO 5 500 737500 ICAO_A 3 8 Climb MaxClimb ZERO 7 500L 168/288 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737500 ICAO_A 3 9 Climb MaxClimb ZERO 10 000 737500 ICAO_A 4 1 Takeoff MaxTakeoff 5 737500 ICAO_A 4 2 Climb MaxTakeoff 5 1 500 737500 ICAO_A 4 3 Climb MaxClimb 5 3 000 737500 ICAO_A 4 4 Accelerate MaxClimb 5 1 166,9 189,6 737500 ICAO_A 4 5 Accelerate MaxClimb 1 1 317 211 737500 ICAO_A 4 6 Accelerate MaxClimb ZERO 1 496,1 250 737500 ICAO_A 4 7 Climb MaxClimb ZERO 5 500 737500 ICAO_A 4 8 Climb MaxClimb ZERO 7 500 737500 ICAO_A 4 9 Climb MaxClimb ZERO 10 000 737500 ICAO_A 5 1 Takeoff MaxTakeoff 5 737500 ICAO_A 5 2 Climb MaxTakeoff 5 1 500 737500 ICAO_A 5 3 Climb MaxClimb 5 3 000 737500 ICAO_A 5 4 Accelerate MaxClimb 5 1 152,1 189,9 737500 ICAO_A 5 5 Accelerate MaxClimb 1 1 300 210,8 737500 ICAO_A 5 6 Accelerate MaxClimb ZERO 1 477,5 250 737500 ICAO_A 5 7 Climb MaxClimb ZERO 5 500 737500 ICAO_A 5 8 Climb MaxClimb ZERO 7 500 737500 ICAO_A 5 9 Climb MaxClimb ZERO 10 000 737500 ICAO_A M 1 Takeoff MaxTakeoff 51.7.2015 EN Official Journal of the European Union L 168/289 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737500 ICAO_A M 2 Climb MaxTakeoff 5 1 500 737500 ICAO_A M 3 Climb MaxClimb 5 3 000 737500 ICAO_A M 4 Accelerate MaxClimb 5 1 130,1 190,4 737500 ICAO_A M 5 Accelerate MaxClimb 1 1 267,1 210,6 737500 ICAO_A M 6 Accelerate MaxClimb ZERO 1 451,9 250 737500 ICAO_A M 7 Climb MaxClimb ZERO 5 500 737500 ICAO_A M 8 Climb MaxClimb ZERO 7 500 737500 ICAO_A M 9 Climb MaxClimb ZERO 10 000 737500 ICAO_B 1 1 Takeoff MaxTakeoff 5 737500 ICAO_B 1 2 Climb MaxTakeoff 5 1 000 737500 ICAO_B 1 3 Accelerate MaxTakeoff 5 1 715,3 189,5 737500 ICAO_B 1 4 Accelerate MaxTakeoff 1 1 944,8 207,8 737500 ICAO_B 1 5 Climb MaxClimb ZERO 3 000 737500 ICAO_B 1 6 Accelerate MaxClimb ZERO 1 966,3 250 737500 ICAO_B 1 7 Climb MaxClimb ZERO 5 500 737500 ICAO_B 1 8 Climb MaxClimb ZERO 7 500 737500 ICAO_B 1 9 Climb MaxClimb ZERO 10 000 737500 ICAO_B 2 1 Takeoff MaxTakeoff 5 737500 ICAO_B 2 2 Climb MaxTakeoff 5 1 000 737500 ICAO_B 2 3 Accelerate MaxTakeoff 5 1 619,6 190,3L 168/290 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737500 ICAO_B 2 4 Accelerate MaxTakeoff 1 1 835,3 207,1 737500 ICAO_B 2 5 Climb MaxClimb ZERO 3 000 737500 ICAO_B 2 6 Accelerate MaxClimb ZERO 1 844,6 250 737500 ICAO_B 2 7 Climb MaxClimb ZERO 5 500 737500 ICAO_B 2 8 Climb MaxClimb ZERO 7 500 737500 ICAO_B 2 9 Climb MaxClimb ZERO 10 000 737500 ICAO_B 3 1 Takeoff MaxTakeoff 5 737500 ICAO_B 3 2 Climb MaxTakeoff 5 1 000 737500 ICAO_B 3 3 Accelerate MaxTakeoff 5 1 520,2 191,6 737500 ICAO_B 3 4 Accelerate MaxTakeoff 1 1 717,5 207,1 737500 ICAO_B 3 5 Climb MaxClimb ZERO 3 000 737500 ICAO_B 3 6 Accelerate MaxClimb ZERO 1 722,6 250 737500 ICAO_B 3 7 Climb MaxClimb ZERO 5 500 737500 ICAO_B 3 8 Climb MaxClimb ZERO 7 500 737500 ICAO_B 3 9 Climb MaxClimb ZERO 10 000 737500 ICAO_B 4 1 Takeoff MaxTakeoff 5 737500 ICAO_B 4 2 Climb MaxTakeoff 5 1 000 737500 ICAO_B 4 3 Accelerate MaxTakeoff 5 1 339,9 194,1 737500 ICAO_B 4 4 Accelerate MaxTakeoff 1 1 512,8 213,4 737500 ICAO_B 4 5 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/291 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737500 ICAO_B 4 6 Accelerate MaxClimb ZERO 1 526,7 250 737500 ICAO_B 4 7 Climb MaxClimb ZERO 5 500 737500 ICAO_B 4 8 Climb MaxClimb ZERO 7 500 737500 ICAO_B 4 9 Climb MaxClimb ZERO 10 000 737500 ICAO_B 5 1 Takeoff MaxTakeoff 5 737500 ICAO_B 5 2 Climb MaxTakeoff 5 1 000 737500 ICAO_B 5 3 Accelerate MaxTakeoff 5 1 322,2 194,4 737500 ICAO_B 5 4 Accelerate MaxTakeoff 1 1 500 213,2 737500 ICAO_B 5 5 Climb MaxClimb ZERO 3 000 737500 ICAO_B 5 6 Accelerate MaxClimb ZERO 1 503,1 250 737500 ICAO_B 5 7 Climb MaxClimb ZERO 5 500 737500 ICAO_B 5 8 Climb MaxClimb ZERO 7 500 737500 ICAO_B 5 9 Climb MaxClimb ZERO 10 000 737500 ICAO_B M 1 Takeoff MaxTakeoff 5 737500 ICAO_B M 2 Climb MaxTakeoff 5 1 000 737500 ICAO_B M 3 Accelerate MaxTakeoff 5 1 303,1 194,8 737500 ICAO_B M 4 Accelerate MaxTakeoff 1 1 463,2 213 737500 ICAO_B M 5 Climb MaxClimb ZERO 3 000 737500 ICAO_B M 6 Accelerate MaxClimb ZERO 1 475,5 250 737500 ICAO_B M 7 Climb MaxClimb ZERO 5 500L 168/292 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737500 ICAO_B M 8 Climb MaxClimb ZERO 7 500 737500 ICAO_B M 9 Climb MaxClimb ZERO 10 000 737700 DEFAULT 1 1 Takeoff MaxTakeoff T_5 737700 DEFAULT 1 2 Climb MaxTakeoff T_5 1 000 737700 DEFAULT 1 3 Accelerate MaxClimb T_ZERO 1 782,4 195,1 737700 DEFAULT 1 4 Climb MaxClimb T_ZERO 3 000 737700 DEFAULT 1 5 Accelerate MaxClimb T_ZERO 2 159,3 250 737700 DEFAULT 1 6 Climb MaxClimb T_ZERO 5 500 737700 DEFAULT 1 7 Climb MaxClimb T_00H 7 500 737700 DEFAULT 1 8 Climb MaxClimb T_00H 10 000 737700 DEFAULT 2 1 Takeoff MaxTakeoff T_5 737700 DEFAULT 2 2 Climb MaxTakeoff T_5 1 000 737700 DEFAULT 2 3 Accelerate MaxClimb T_ZERO 1 710,1 197,7 737700 DEFAULT 2 4 Climb MaxClimb T_ZERO 3 000 737700 DEFAULT 2 5 Accelerate MaxClimb T_ZERO 2 056,7 250 737700 DEFAULT 2 6 Climb MaxClimb T_ZERO 5 500 737700 DEFAULT 2 7 Climb MaxClimb T_00H 7 500 737700 DEFAULT 2 8 Climb MaxClimb T_00H 10 000 737700 DEFAULT 3 1 Takeoff MaxTakeoff T_5 737700 DEFAULT 3 2 Climb MaxTakeoff T_5 1 0001.7.2015 EN Official Journal of the European Union L 168/293 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737700 DEFAULT 3 3 Accelerate MaxClimb T_ZERO 1 635,7 200,3 737700 DEFAULT 3 4 Climb MaxClimb T_ZERO 3 000 737700 DEFAULT 3 5 Accelerate MaxClimb T_ZERO 1 957 250 737700 DEFAULT 3 6 Climb MaxClimb T_ZERO 5 500 737700 DEFAULT 3 7 Climb MaxClimb T_ZERO 7 500 737700 DEFAULT 3 8 Climb MaxClimb T_00H 10 000 737700 DEFAULT 4 1 Takeoff MaxTakeoff T_5 737700 DEFAULT 4 2 Climb MaxTakeoff T_5 1 000 737700 DEFAULT 4 3 Accelerate MaxClimb T_ZERO 1 498,3 205,8 737700 DEFAULT 4 4 Climb MaxClimb T_ZERO 3 000 737700 DEFAULT 4 5 Accelerate MaxClimb T_ZERO 1 774,4 250 737700 DEFAULT 4 6 Climb MaxClimb T_ZERO 5 500 737700 DEFAULT 4 7 Climb MaxClimb T_ZERO 7 500 737700 DEFAULT 4 8 Climb MaxClimb T_ZERO 10 000 737700 DEFAULT 5 1 Takeoff MaxTakeoff T_5 737700 DEFAULT 5 2 Climb MaxTakeoff T_5 1 000 737700 DEFAULT 5 3 Accelerate MaxClimb T_ZERO 1 348,5 211,6 737700 DEFAULT 5 4 Climb MaxClimb T_ZERO 3 000 737700 DEFAULT 5 5 Accelerate MaxClimb T_ZERO 1 581,2 250 737700 DEFAULT 5 6 Climb MaxClimb T_ZERO 5 500L 168/294 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737700 DEFAULT 5 7 Climb MaxClimb T_ZERO 7 500 737700 DEFAULT 5 8 Climb MaxClimb T_ZERO 10 000 737700 DEFAULT 6 1 Takeoff MaxTakeoff T_5 737700 DEFAULT 6 2 Climb MaxTakeoff T_5 1 000 737700 DEFAULT 6 3 Accelerate MaxClimb T_ZERO 1 347,1 211,6 737700 DEFAULT 6 4 Climb MaxClimb T_ZERO 3 000 737700 DEFAULT 6 5 Accelerate MaxClimb T_ZERO 1 579,1 250 737700 DEFAULT 6 6 Climb MaxClimb T_ZERO 5 500 737700 DEFAULT 6 7 Climb MaxClimb T_ZERO 7 500 737700 DEFAULT 6 8 Climb MaxClimb T_ZERO 10 000 737700 ICAO_A 1 1 Takeoff MaxTakeoff T_5 737700 ICAO_A 1 2 Climb MaxTakeoff T_5 1 500 737700 ICAO_A 1 3 Climb MaxClimb T_5 3 000 737700 ICAO_A 1 4 Accelerate MaxClimb T_ZERO 1 747,6 194,9 737700 ICAO_A 1 5 Accelerate MaxClimb T_ZERO 2 128,3 250 737700 ICAO_A 1 6 Climb MaxClimb T_ZERO 5 500 737700 ICAO_A 1 7 Climb MaxClimb T_00H 7 500 737700 ICAO_A 1 8 Climb MaxClimb T_00H 10 000 737700 ICAO_A 2 1 Takeoff MaxTakeoff T_5 737700 ICAO_A 2 2 Climb MaxTakeoff T_5 1 5001.7.2015 EN Official Journal of the European Union L 168/295 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737700 ICAO_A 2 3 Climb MaxClimb T_5 3 000 737700 ICAO_A 2 4 Accelerate MaxClimb T_ZERO 1 673,6 197,4 737700 ICAO_A 2 5 Accelerate MaxClimb T_ZERO 2 028,3 250 737700 ICAO_A 2 6 Climb MaxClimb T_ZERO 5 500 737700 ICAO_A 2 7 Climb MaxClimb T_ZERO 7 500 737700 ICAO_A 2 8 Climb MaxClimb T_00H 10 000 737700 ICAO_A 3 1 Takeoff MaxTakeoff T_5 737700 ICAO_A 3 2 Climb MaxTakeoff T_5 1 500 737700 ICAO_A 3 3 Climb MaxClimb T_5 3 000 737700 ICAO_A 3 4 Accelerate MaxClimb T_ZERO 1 600,5 200,2 737700 ICAO_A 3 5 Accelerate MaxClimb T_ZERO 1 931,7 250 737700 ICAO_A 3 6 Climb MaxClimb T_ZERO 5 500 737700 ICAO_A 3 7 Climb MaxClimb T_ZERO 7 500 737700 ICAO_A 3 8 Climb MaxClimb T_00H 10 000 737700 ICAO_A 4 1 Takeoff MaxTakeoff T_5 737700 ICAO_A 4 2 Climb MaxTakeoff T_5 1 500 737700 ICAO_A 4 3 Climb MaxClimb T_5 3 000 737700 ICAO_A 4 4 Accelerate MaxClimb T_ZERO 1 462,2 205,6 737700 ICAO_A 4 5 Accelerate MaxClimb T_ZERO 1 753,8 250 737700 ICAO_A 4 6 Climb MaxClimb T_ZERO 5 500L 168/296 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737700 ICAO_A 4 7 Climb MaxClimb T_ZERO 7 500 737700 ICAO_A 4 8 Climb MaxClimb T_00H 10 000 737700 ICAO_A 5 1 Takeoff MaxTakeoff T_5 737700 ICAO_A 5 2 Climb MaxTakeoff T_5 1 500 737700 ICAO_A 5 3 Climb MaxClimb T_5 3 000 737700 ICAO_A 5 4 Accelerate MaxClimb T_ZERO 1 430 250 737700 ICAO_A 5 5 Climb MaxClimb T_ZERO 5 500 737700 ICAO_A 5 6 Climb MaxClimb T_ZERO 7 500 737700 ICAO_A 5 7 Climb MaxClimb T_ZERO 10 000 737700 ICAO_A 6 1 Takeoff MaxTakeoff T_5 737700 ICAO_A 6 2 Climb MaxTakeoff T_5 1 500 737700 ICAO_A 6 3 Climb MaxClimb T_5 3 000 737700 ICAO_A 6 4 Accelerate MaxClimb T_ZERO 1 430,1 250 737700 ICAO_A 6 5 Climb MaxClimb T_ZERO 5 500 737700 ICAO_A 6 6 Climb MaxClimb T_ZERO 7 500 737700 ICAO_A 6 7 Climb MaxClimb T_ZERO 10 000 737700 ICAO_B 1 1 Takeoff MaxTakeoff T_5 737700 ICAO_B 1 2 Climb MaxTakeoff T_5 1 000 737700 ICAO_B 1 3 Accelerate MaxTakeoff T_01 1 888,7 195,1 737700 ICAO_B 1 4 Climb MaxClimb T_ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/297 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737700 ICAO_B 1 5 Accelerate MaxClimb T_ZERO 2 159,3 250 737700 ICAO_B 1 6 Climb MaxClimb T_00H 5 500 737700 ICAO_B 1 7 Climb MaxClimb T_00H 7 500 737700 ICAO_B 1 8 Climb MaxClimb T_ZERO 10 000 737700 ICAO_B 2 1 Takeoff MaxTakeoff T_5 737700 ICAO_B 2 2 Climb MaxTakeoff T_5 1 000 737700 ICAO_B 2 3 Accelerate MaxTakeoff T_01 1 814,3 197,7 737700 ICAO_B 2 4 Climb MaxClimb T_ZERO 3 000 737700 ICAO_B 2 5 Accelerate MaxClimb T_ZERO 2 058,1 250 737700 ICAO_B 2 6 Climb MaxClimb T_ZERO 5 500 737700 ICAO_B 2 7 Climb MaxClimb T_ZERO 7 500 737700 ICAO_B 2 8 Climb MaxClimb T_00H 10 000 737700 ICAO_B 3 1 Takeoff MaxTakeoff T_5 737700 ICAO_B 3 2 Climb MaxTakeoff T_5 1 000 737700 ICAO_B 3 3 Accelerate MaxTakeoff T_5 1 619 175,6 737700 ICAO_B 3 4 Accelerate MaxTakeoff T_01 1 840,6 200,4 737700 ICAO_B 3 5 Climb MaxClimb T_ZERO 3 000 737700 ICAO_B 3 6 Accelerate MaxClimb T_ZERO 1 958,4 250 737700 ICAO_B 3 7 Climb MaxClimb T_ZERO 5 500 737700 ICAO_B 3 8 Climb MaxClimb T_ZERO 7 500L 168/298 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737700 ICAO_B 3 9 Climb MaxClimb T_ZERO 10 000 737700 ICAO_B 4 1 Takeoff MaxTakeoff T_5 737700 ICAO_B 4 2 Climb MaxTakeoff T_5 1 000 737700 ICAO_B 4 3 Accelerate MaxTakeoff T_01 1 594,1 205,8 737700 ICAO_B 4 4 Climb MaxClimb T_ZERO 3 000 737700 ICAO_B 4 5 Accelerate MaxClimb T_ZERO 1 774,4 250 737700 ICAO_B 4 6 Climb MaxClimb T_ZERO 5 500 737700 ICAO_B 4 7 Climb MaxClimb T_ZERO 7 500 737700 ICAO_B 4 8 Climb MaxClimb T_ZERO 10 000 737700 ICAO_B 5 1 Takeoff MaxTakeoff T_5 737700 ICAO_B 5 2 Climb MaxTakeoff T_5 1 000 737700 ICAO_B 5 3 Accelerate MaxTakeoff T_01 1 438,9 211,5 737700 ICAO_B 5 4 Climb MaxClimb T_ZERO 3 000 737700 ICAO_B 5 5 Accelerate MaxClimb T_ZERO 1 579,6 250 737700 ICAO_B 5 6 Climb MaxClimb T_ZERO 5 500 737700 ICAO_B 5 7 Climb MaxClimb T_ZERO 7 500 737700 ICAO_B 5 8 Climb MaxClimb T_ZERO 10 000 737700 ICAO_B 6 1 Takeoff MaxTakeoff T_5 737700 ICAO_B 6 2 Climb MaxTakeoff T_5 1 000 737700 ICAO_B 6 3 Accelerate MaxTakeoff T_01 1 437,2 211,51.7.2015 EN Official Journal of the European Union L 168/299 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737700 ICAO_B 6 4 Climb MaxClimb T_ZERO 3 000 737700 ICAO_B 6 5 Accelerate MaxClimb T_ZERO 1 579,1 250 737700 ICAO_B 6 6 Climb MaxClimb T_ZERO 5 500 737700 ICAO_B 6 7 Climb MaxClimb T_ZERO 7 500 737700 ICAO_B 6 8 Climb MaxClimb T_ZERO 10 000 737800 DEFAULT 1 1 Takeoff MaxTakeoff T_05 737800 DEFAULT 1 2 Climb MaxTakeoff T_05 1 000 737800 DEFAULT 1 3 Accelerate MaxTakeoff T_05 1 885,7 181,7 737800 DEFAULT 1 4 Accelerate MaxTakeoff T_01 2 112 204,8 737800 DEFAULT 1 5 Climb MaxTakeoff T_00 2 040 737800 DEFAULT 1 6 Climb MaxClimb T_00 3 000 737800 DEFAULT 1 7 Accelerate MaxClimb T_00 1 891,3 250 737800 DEFAULT 1 8 Climb MaxClimb T_00 5 500 737800 DEFAULT 1 9 Climb MaxClimb T_00 7 500 737800 DEFAULT 1 10 Climb MaxClimb T_00 10 000 737800 DEFAULT 2 1 Takeoff MaxTakeoff T_05 737800 DEFAULT 2 2 Climb MaxTakeoff T_05 1 000 737800 DEFAULT 2 3 Accelerate MaxTakeoff T_05 1 786,4 183,9 737800 DEFAULT 2 4 Accelerate MaxTakeoff T_01 2 016,2 208 737800 DEFAULT 2 5 Climb MaxTakeoff T_00 2 000L 168/300 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737800 DEFAULT 2 6 Climb MaxClimb T_00 3 000 737800 DEFAULT 2 7 Accelerate MaxClimb T_00 1 793,4 250 737800 DEFAULT 2 8 Climb MaxClimb T_00 5 500 737800 DEFAULT 2 9 Climb MaxClimb T_00 7 500 737800 DEFAULT 2 10 Climb MaxClimb T_00 10 000 737800 DEFAULT 3 1 Takeoff MaxTakeoff T_05 737800 DEFAULT 3 2 Climb MaxTakeoff T_05 1 000 737800 DEFAULT 3 3 Accelerate MaxTakeoff T_05 1 707,7 186,2 737800 DEFAULT 3 4 Accelerate MaxTakeoff T_05 1 922 211,2 737800 DEFAULT 3 5 Climb MaxTakeoff T_00 1 960 737800 DEFAULT 3 6 Climb MaxClimb T_00 3 000 737800 DEFAULT 3 7 Accelerate MaxClimb T_00 1 705,3 250 737800 DEFAULT 3 8 Climb MaxClimb T_00 5 500 737800 DEFAULT 3 9 Climb MaxClimb T_00 7 500 737800 DEFAULT 3 10 Climb MaxClimb T_00 10 000 737800 DEFAULT 4 1 Takeoff MaxTakeoff T_05 737800 DEFAULT 4 2 Climb MaxTakeoff T_05 1 000 737800 DEFAULT 4 3 Accelerate MaxTakeoff T_05 1 576,6 189,6 737800 DEFAULT 4 4 Accelerate MaxTakeoff T_01 1 766,9 216,2 737800 DEFAULT 4 5 Climb MaxTakeoff T_00 1 8801.7.2015 EN Official Journal of the European Union L 168/301 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737800 DEFAULT 4 6 Climb MaxClimb T_00 3 000 737800 DEFAULT 4 7 Accelerate MaxClimb T_00 1 546,5 250 737800 DEFAULT 4 8 Climb MaxClimb T_00 5 500 737800 DEFAULT 4 9 Climb MaxClimb T_00 7 500 737800 DEFAULT 4 10 Climb MaxClimb T_00 10 000 737800 DEFAULT 5 1 Takeoff MaxTakeoff T_05 737800 DEFAULT 5 2 Climb MaxTakeoff T_05 1 000 737800 DEFAULT 5 3 Accelerate MaxTakeoff T_05 1 444,9 192,9 737800 DEFAULT 5 4 Accelerate MaxTakeoff T_01 1 628,6 220,7 737800 DEFAULT 5 5 Climb MaxTakeoff T_00 1 811 737800 DEFAULT 5 6 Climb MaxClimb T_00 3 000 737800 DEFAULT 5 7 Accelerate MaxClimb T_00 1 412,2 250 737800 DEFAULT 5 8 Climb MaxClimb T_00 5 500 737800 DEFAULT 5 9 Climb MaxClimb T_00 7 500 737800 DEFAULT 5 10 Climb MaxClimb T_00 10 000 737800 DEFAULT 6 1 Takeoff MaxTakeoff T_05 737800 DEFAULT 6 2 Climb MaxTakeoff T_05 1 000 737800 DEFAULT 6 3 Accelerate MaxTakeoff T_05 1 400 194,4 737800 DEFAULT 6 4 Accelerate MaxTakeoff T_01 1 575,4 222,7 737800 DEFAULT 6 5 Climb MaxTakeoff T_00 1 785L 168/302 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737800 DEFAULT 6 6 Climb MaxClimb T_00 3 000 737800 DEFAULT 6 7 Accelerate MaxClimb T_00 1 357,5 250 737800 DEFAULT 6 8 Climb MaxClimb T_00 5 500 737800 DEFAULT 6 9 Climb MaxClimb T_00 7 500 737800 DEFAULT 6 10 Climb MaxClimb T_00 10 000 737800 ICAO_A 1 1 Takeoff MaxTakeoff T_05 737800 ICAO_A 1 2 Climb MaxTakeoff T_05 1 500 737800 ICAO_A 1 3 Climb MaxClimb T_05 3 000 737800 ICAO_A 1 4 Accelerate MaxClimb T_05 1 449,4 177,2 737800 ICAO_A 1 5 Accelerate MaxClimb T_01 1 663,3 204,6 737800 ICAO_A 1 6 Climb MaxClimb T_00 3 807 737800 ICAO_A 1 7 Accelerate MaxClimb T_00 1 896,8 250 737800 ICAO_A 1 8 Climb MaxClimb T_00 5 500 737800 ICAO_A 1 9 Climb MaxClimb T_00 7 500 737800 ICAO_A 1 10 Climb MaxClimb T_00 10 000 737800 ICAO_A 2 1 Takeoff MaxTakeoff T_05 737800 ICAO_A 2 2 Climb MaxTakeoff T_05 1 500 737800 ICAO_A 2 3 Climb MaxClimb T_05 3 000 737800 ICAO_A 2 4 Accelerate MaxClimb T_05 1 372,3 179,6 737800 ICAO_A 2 5 Accelerate MaxClimb T_01 1 579,3 207,81.7.2015 EN Official Journal of the European Union L 168/303 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737800 ICAO_A 2 6 Climb MaxClimb T_00 3 772 737800 ICAO_A 2 7 Accelerate MaxClimb T_00 1 804,3 250 737800 ICAO_A 2 8 Climb MaxClimb T_00 5 500 737800 ICAO_A 2 9 Climb MaxClimb T_00 7 500 737800 ICAO_A 2 10 Climb MaxClimb T_00 10 000 737800 ICAO_A 3 1 Takeoff MaxTakeoff T_05 737800 ICAO_A 3 2 Climb MaxTakeoff T_05 1 500 737800 ICAO_A 3 3 Climb MaxClimb T_05 3 000 737800 ICAO_A 3 4 Accelerate MaxClimb T_05 1 297 182,1 737800 ICAO_A 3 5 Accelerate MaxClimb T_01 1 496,9 211 737800 ICAO_A 3 6 Climb MaxClimb T_00 3 737 737800 ICAO_A 3 7 Accelerate MaxClimb T_00 1 701,8 250 737800 ICAO_A 3 8 Climb MaxClimb T_00 5 500 737800 ICAO_A 3 9 Climb MaxClimb T_00 7 500 737800 ICAO_A 3 10 Climb MaxClimb T_00 10 000 737800 ICAO_A 4 1 Takeoff MaxTakeoff T_05 737800 ICAO_A 4 2 Climb MaxTakeoff T_05 1 500 737800 ICAO_A 4 3 Climb MaxClimb T_05 3 000 737800 ICAO_A 4 4 Accelerate MaxClimb T_05 1 194,2 185,8 737800 ICAO_A 4 5 Accelerate MaxClimb T_01 1 352,1 214,8L 168/304 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737800 ICAO_A 4 6 Accelerate MaxClimb T_00 1 548,2 250 737800 ICAO_A 4 7 Climb MaxClimb T_00 5 500 737800 ICAO_A 4 8 Climb MaxClimb T_00 7 500 737800 ICAO_A 4 9 Climb MaxClimb T_00 10 000 737800 ICAO_A 5 1 Takeoff MaxTakeoff T_05 737800 ICAO_A 5 2 Climb MaxTakeoff T_05 1 500 737800 ICAO_A 5 3 Climb MaxClimb T_05 3 000 737800 ICAO_A 5 4 Accelerate MaxClimb T_05 1 078,9 189,4 737800 ICAO_A 5 5 Accelerate MaxClimb T_01 1 233,3 217,4 737800 ICAO_A 5 6 Accelerate MaxClimb T_00 1 403,6 250 737800 ICAO_A 5 7 Climb MaxClimb T_00 5 500 737800 ICAO_A 5 8 Climb MaxClimb T_00 7 500 737800 ICAO_A 5 9 Climb MaxClimb T_00 10 000 737800 ICAO_A 6 1 Takeoff MaxTakeoff T_05 737800 ICAO_A 6 2 Climb MaxTakeoff T_05 1 500 737800 ICAO_A 6 3 Climb MaxClimb T_05 3 000 737800 ICAO_A 6 4 Accelerate MaxClimb T_05 1 037,8 190,9 737800 ICAO_A 6 5 Accelerate MaxClimb T_01 1 182,7 218,6 737800 ICAO_A 6 6 Accelerate MaxClimb T_00 1 349,5 250 737800 ICAO_A 6 7 Climb MaxClimb T_00 5 5001.7.2015 EN Official Journal of the European Union L 168/305 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737800 ICAO_A 6 8 Climb MaxClimb T_00 7 500 737800 ICAO_A 6 9 Climb MaxClimb T_00 10 000 737800 ICAO_B 1 1 Takeoff MaxTakeoff T_05 737800 ICAO_B 1 2 Climb MaxTakeoff T_05 1 000 737800 ICAO_B 1 3 Accelerate MaxTakeoff T_05 1 885,7 181,7 737800 ICAO_B 1 4 Accelerate MaxTakeoff T_01 2 112 204,8 737800 ICAO_B 1 5 Climb MaxTakeoff T_00 2 040 737800 ICAO_B 1 6 Climb MaxClimb T_00 3 000 737800 ICAO_B 1 7 Accelerate MaxClimb T_00 1 891,3 250 737800 ICAO_B 1 8 Climb MaxClimb T_00 5 500 737800 ICAO_B 1 9 Climb MaxClimb T_00 7 500 737800 ICAO_B 1 10 Climb MaxClimb T_00 10 000 737800 ICAO_B 2 1 Takeoff MaxTakeoff T_05 737800 ICAO_B 2 2 Climb MaxTakeoff T_05 1 000 737800 ICAO_B 2 3 Accelerate MaxTakeoff T_05 1 786,4 183,9 737800 ICAO_B 2 4 Accelerate MaxTakeoff T_01 2 016,2 208 737800 ICAO_B 2 5 Climb MaxTakeoff T_00 2 000 737800 ICAO_B 2 6 Climb MaxClimb T_00 3 000 737800 ICAO_B 2 7 Accelerate MaxClimb T_00 1 793,4 250 737800 ICAO_B 2 8 Climb MaxClimb T_00 5 500L 168/306 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737800 ICAO_B 2 9 Climb MaxClimb T_00 7 500 737800 ICAO_B 2 10 Climb MaxClimb T_00 10 000 737800 ICAO_B 3 1 Takeoff MaxTakeoff T_05 737800 ICAO_B 3 2 Climb MaxTakeoff T_05 1 000 737800 ICAO_B 3 3 Accelerate MaxTakeoff T_05 1 707,7 186,2 737800 ICAO_B 3 4 Accelerate MaxTakeoff T_05 1 922 211,2 737800 ICAO_B 3 5 Climb MaxTakeoff T_00 1 960 737800 ICAO_B 3 6 Climb MaxClimb T_00 3 000 737800 ICAO_B 3 7 Accelerate MaxClimb T_00 1 705,3 250 737800 ICAO_B 3 8 Climb MaxClimb T_00 5 500 737800 ICAO_B 3 9 Climb MaxClimb T_00 7 500 737800 ICAO_B 3 10 Climb MaxClimb T_00 10 000 737800 ICAO_B 4 1 Takeoff MaxTakeoff T_05 737800 ICAO_B 4 2 Climb MaxTakeoff T_05 1 000 737800 ICAO_B 4 3 Accelerate MaxTakeoff T_05 1 576,6 189,6 737800 ICAO_B 4 4 Accelerate MaxTakeoff T_01 1 766,9 216,2 737800 ICAO_B 4 5 Climb MaxTakeoff T_00 1 880 737800 ICAO_B 4 6 Climb MaxClimb T_00 3 000 737800 ICAO_B 4 7 Accelerate MaxClimb T_00 1 546,5 250 737800 ICAO_B 4 8 Climb MaxClimb T_00 5 5001.7.2015 EN Official Journal of the European Union L 168/307 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737800 ICAO_B 4 9 Climb MaxClimb T_00 7 500 737800 ICAO_B 4 10 Climb MaxClimb T_00 10 000 737800 ICAO_B 5 1 Takeoff MaxTakeoff T_05 737800 ICAO_B 5 2 Climb MaxTakeoff T_05 1 000 737800 ICAO_B 5 3 Accelerate MaxTakeoff T_05 1 444,9 192,9 737800 ICAO_B 5 4 Accelerate MaxTakeoff T_01 1 628,6 220,7 737800 ICAO_B 5 5 Climb MaxTakeoff T_00 1 811 737800 ICAO_B 5 6 Climb MaxClimb T_00 3 000 737800 ICAO_B 5 7 Accelerate MaxClimb T_00 1 412,2 250 737800 ICAO_B 5 8 Climb MaxClimb T_00 5 500 737800 ICAO_B 5 9 Climb MaxClimb T_00 7 500 737800 ICAO_B 5 10 Climb MaxClimb T_00 10 000 737800 ICAO_B 6 1 Takeoff MaxTakeoff T_05 737800 ICAO_B 6 2 Climb MaxTakeoff T_05 1 000 737800 ICAO_B 6 3 Accelerate MaxTakeoff T_05 1 400 194,4 737800 ICAO_B 6 4 Accelerate MaxTakeoff T_01 1 575,4 222,7 737800 ICAO_B 6 5 Climb MaxTakeoff T_00 1 785 737800 ICAO_B 6 6 Climb MaxClimb T_00 3 000 737800 ICAO_B 6 7 Accelerate MaxClimb T_00 1 357,5 250 737800 ICAO_B 6 8 Climb MaxClimb T_00 5 500L 168/308 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737800 ICAO_B 6 9 Climb MaxClimb T_00 7 500 737800 ICAO_B 6 10 Climb MaxClimb T_00 10 000 737D17 DEFAULT 1 1 Takeoff MaxTakeoff 5 737D17 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 737D17 DEFAULT 1 3 Accelerate MaxTakeoff 5 2 279 152 737D17 DEFAULT 1 4 Accelerate MaxTakeoff INT 1 709 177 737D17 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 210 737D17 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 737D17 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 737D17 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 737D17 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 737D17 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 737D17 DEFAULT 2 1 Takeoff MaxTakeoff 5 737D17 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 737D17 DEFAULT 2 3 Accelerate MaxTakeoff 5 2 155 156 737D17 DEFAULT 2 4 Accelerate MaxTakeoff INT 1 616 181 737D17 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 210 737D17 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 737D17 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 737D17 DEFAULT 2 8 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/309 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737D17 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 737D17 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 737D17 DEFAULT 3 1 Takeoff MaxTakeoff 5 737D17 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 737D17 DEFAULT 3 3 Accelerate MaxTakeoff 5 2 041 160 737D17 DEFAULT 3 4 Accelerate MaxTakeoff INT 1 531 185 737D17 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 210 737D17 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 737D17 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 737D17 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 737D17 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 737D17 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 737D17 DEFAULT 4 1 Takeoff MaxTakeoff 5 737D17 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 737D17 DEFAULT 4 3 Accelerate MaxTakeoff 5 1 935 163 737D17 DEFAULT 4 4 Accelerate MaxTakeoff INT 1 452 188 737D17 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 210 737D17 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 737D17 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 737D17 DEFAULT 4 8 Climb MaxClimb ZERO 5 500L 168/310 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737D17 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 737D17 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 737N17 DEFAULT 1 1 Takeoff MaxTakeoff 5 737N17 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 737N17 DEFAULT 1 3 Accelerate MaxTakeoff 5 2 279 152 737N17 DEFAULT 1 4 Accelerate MaxTakeoff INT 1 709 177 737N17 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 210 737N17 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 737N17 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 737N17 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 737N17 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 737N17 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 737N17 DEFAULT 2 1 Takeoff MaxTakeoff 5 737N17 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 737N17 DEFAULT 2 3 Accelerate MaxTakeoff 5 2 155 156 737N17 DEFAULT 2 4 Accelerate MaxTakeoff INT 1 616 181 737N17 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 210 737N17 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 737N17 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 737N17 DEFAULT 2 8 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/311 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737N17 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 737N17 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 737N17 DEFAULT 3 1 Takeoff MaxTakeoff 5 737N17 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 737N17 DEFAULT 3 3 Accelerate MaxTakeoff 5 2 041 160 737N17 DEFAULT 3 4 Accelerate MaxTakeoff INT 1 531 185 737N17 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 210 737N17 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 737N17 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 737N17 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 737N17 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 737N17 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 737N17 DEFAULT 4 1 Takeoff MaxTakeoff 5 737N17 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 737N17 DEFAULT 4 3 Accelerate MaxTakeoff 5 1 935 163 737N17 DEFAULT 4 4 Accelerate MaxTakeoff INT 1 452 188 737N17 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 210 737N17 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 737N17 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 737N17 DEFAULT 4 8 Climb MaxClimb ZERO 5 500L 168/312 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737N17 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 737N17 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 737N9 DEFAULT 1 1 Takeoff MaxTakeoff 5 737N9 DEFAULT 1 2 Climb MaxTakeoff 5 1 000 737N9 DEFAULT 1 3 Accelerate MaxTakeoff 5 2 090 146 737N9 DEFAULT 1 4 Accelerate MaxTakeoff INT 1 568 171 737N9 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 210 737N9 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 737N9 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 737N9 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 737N9 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 737N9 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 737N9 DEFAULT 2 1 Takeoff MaxTakeoff 5 737N9 DEFAULT 2 2 Climb MaxTakeoff 5 1 000 737N9 DEFAULT 2 3 Accelerate MaxTakeoff 5 2 014 149 737N9 DEFAULT 2 4 Accelerate MaxTakeoff INT 1 511 174 737N9 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 210 737N9 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 737N9 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 737N9 DEFAULT 2 8 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/313 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737N9 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 737N9 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 737N9 DEFAULT 3 1 Takeoff MaxTakeoff 5 737N9 DEFAULT 3 2 Climb MaxTakeoff 5 1 000 737N9 DEFAULT 3 3 Accelerate MaxTakeoff 5 1 851 154 737N9 DEFAULT 3 4 Accelerate MaxTakeoff INT 1 388 179 737N9 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 210 737N9 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 737N9 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 737N9 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 737N9 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 737N9 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 737N9 DEFAULT 4 1 Takeoff MaxTakeoff 5 737N9 DEFAULT 4 2 Climb MaxTakeoff 5 1 000 737N9 DEFAULT 4 3 Accelerate MaxTakeoff 5 1 685 160 737N9 DEFAULT 4 4 Accelerate MaxTakeoff INT 1 264 185 737N9 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 210 737N9 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 737N9 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 737N9 DEFAULT 4 8 Climb MaxClimb ZERO 5 500L 168/314 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737N9 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 737N9 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 737QN DEFAULT 1 1 Takeoff MaxTakeoff 5 737QN DEFAULT 1 2 Climb MaxTakeoff 5 1 000 737QN DEFAULT 1 3 Accelerate MaxTakeoff 5 2 090 146 737QN DEFAULT 1 4 Accelerate MaxTakeoff INT 1 568 171 737QN DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 210 737QN DEFAULT 1 6 Climb MaxClimb ZERO 3 000 737QN DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 737QN DEFAULT 1 8 Climb MaxClimb ZERO 5 500 737QN DEFAULT 1 9 Climb MaxClimb ZERO 7 500 737QN DEFAULT 1 10 Climb MaxClimb ZERO 10 000 737QN DEFAULT 2 1 Takeoff MaxTakeoff 5 737QN DEFAULT 2 2 Climb MaxTakeoff 5 1 000 737QN DEFAULT 2 3 Accelerate MaxTakeoff 5 2 014 149 737QN DEFAULT 2 4 Accelerate MaxTakeoff INT 1 511 174 737QN DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 210 737QN DEFAULT 2 6 Climb MaxClimb ZERO 3 000 737QN DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 737QN DEFAULT 2 8 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/315 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737QN DEFAULT 2 9 Climb MaxClimb ZERO 7 500 737QN DEFAULT 2 10 Climb MaxClimb ZERO 10 000 737QN DEFAULT 3 1 Takeoff MaxTakeoff 5 737QN DEFAULT 3 2 Climb MaxTakeoff 5 1 000 737QN DEFAULT 3 3 Accelerate MaxTakeoff 5 1 851 154 737QN DEFAULT 3 4 Accelerate MaxTakeoff INT 1 388 179 737QN DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 210 737QN DEFAULT 3 6 Climb MaxClimb ZERO 3 000 737QN DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 737QN DEFAULT 3 8 Climb MaxClimb ZERO 5 500 737QN DEFAULT 3 9 Climb MaxClimb ZERO 7 500 737QN DEFAULT 3 10 Climb MaxClimb ZERO 10 000 737QN DEFAULT 4 1 Takeoff MaxTakeoff 5 737QN DEFAULT 4 2 Climb MaxTakeoff 5 1 000 737QN DEFAULT 4 3 Accelerate MaxTakeoff 5 1 685 160 737QN DEFAULT 4 4 Accelerate MaxTakeoff INT 1 264 185 737QN DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 210 737QN DEFAULT 4 6 Climb MaxClimb ZERO 3 000 737QN DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 737QN DEFAULT 4 8 Climb MaxClimb ZERO 5 500L 168/316 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 737QN DEFAULT 4 9 Climb MaxClimb ZERO 7 500 737QN DEFAULT 4 10 Climb MaxClimb ZERO 10 000 74710Q DEFAULT 1 1 Takeoff MaxTakeoff 10 74710Q DEFAULT 1 2 Climb MaxTakeoff 10 1 000 74710Q DEFAULT 1 3 Accelerate MaxTakeoff 10 2 071 176 74710Q DEFAULT 1 4 Accelerate MaxClimb 5 1 000 216 74710Q DEFAULT 1 5 Climb MaxClimb ZERO 3 000 74710Q DEFAULT 1 6 Accelerate MaxClimb ZERO 1 000 250 74710Q DEFAULT 1 7 Climb MaxClimb ZERO 5 500 74710Q DEFAULT 1 8 Climb MaxClimb ZERO 7 500 74710Q DEFAULT 1 9 Climb MaxClimb ZERO 10 000 74710Q DEFAULT 2 1 Takeoff MaxTakeoff 10 74710Q DEFAULT 2 2 Climb MaxTakeoff 10 1 000 74710Q DEFAULT 2 3 Accelerate MaxTakeoff 10 1 972 179 74710Q DEFAULT 2 4 Accelerate MaxClimb 5 1 000 219 74710Q DEFAULT 2 5 Climb MaxClimb ZERO 3 000 74710Q DEFAULT 2 6 Accelerate MaxClimb ZERO 1 000 250 74710Q DEFAULT 2 7 Climb MaxClimb ZERO 5 500 74710Q DEFAULT 2 8 Climb MaxClimb ZERO 7 500 74710Q DEFAULT 2 9 Climb MaxClimb ZERO 10 0001.7.2015 EN Official Journal of the European Union L 168/317 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 74710Q DEFAULT 3 1 Takeoff MaxTakeoff 10 74710Q DEFAULT 3 2 Climb MaxTakeoff 10 1 000 74710Q DEFAULT 3 3 Accelerate MaxTakeoff 10 1 856 183 74710Q DEFAULT 3 4 Accelerate MaxClimb 5 1 000 223 74710Q DEFAULT 3 5 Climb MaxClimb ZERO 3 000 74710Q DEFAULT 3 6 Accelerate MaxClimb ZERO 1 000 250 74710Q DEFAULT 3 7 Climb MaxClimb ZERO 5 500 74710Q DEFAULT 3 8 Climb MaxClimb ZERO 7 500 74710Q DEFAULT 3 9 Climb MaxClimb ZERO 10 000 74710Q DEFAULT 4 1 Takeoff MaxTakeoff 10 74710Q DEFAULT 4 2 Climb MaxTakeoff 10 1 000 74710Q DEFAULT 4 3 Accelerate MaxTakeoff 10 1 727 187 74710Q DEFAULT 4 4 Accelerate MaxClimb 5 1 000 227 74710Q DEFAULT 4 5 Climb MaxClimb ZERO 3 000 74710Q DEFAULT 4 6 Accelerate MaxClimb ZERO 1 000 250 74710Q DEFAULT 4 7 Climb MaxClimb ZERO 5 500 74710Q DEFAULT 4 8 Climb MaxClimb ZERO 7 500 74710Q DEFAULT 4 9 Climb MaxClimb ZERO 10 000 74710Q DEFAULT 5 1 Takeoff MaxTakeoff 10 74710Q DEFAULT 5 2 Climb MaxTakeoff 10 1 000L 168/318 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 74710Q DEFAULT 5 3 Accelerate MaxTakeoff 10 1 445 198 74710Q DEFAULT 5 4 Accelerate MaxClimb 5 750 238 74710Q DEFAULT 5 5 Climb MaxClimb ZERO 3 000 74710Q DEFAULT 5 6 Accelerate MaxClimb ZERO 750 258 74710Q DEFAULT 5 7 Climb MaxClimb ZERO 5 500 74710Q DEFAULT 5 8 Climb MaxClimb ZERO 7 500 74710Q DEFAULT 5 9 Climb MaxClimb ZERO 10 000 74710Q DEFAULT 6 1 Takeoff MaxTakeoff 10 74710Q DEFAULT 6 2 Climb MaxTakeoff 10 1 000 74710Q DEFAULT 6 3 Accelerate MaxTakeoff 10 1 411 199 74710Q DEFAULT 6 4 Accelerate MaxClimb 5 750 239 74710Q DEFAULT 6 5 Climb MaxClimb ZERO 3 000 74710Q DEFAULT 6 6 Accelerate MaxClimb ZERO 750 259 74710Q DEFAULT 6 7 Climb MaxClimb ZERO 5 500 74710Q DEFAULT 6 8 Climb MaxClimb ZERO 7 500 74710Q DEFAULT 6 9 Climb MaxClimb ZERO 10 000 747200 DEFAULT 1 1 Takeoff MaxTakeoff 10 747200 DEFAULT 1 2 Climb MaxTakeoff 10 1 000 747200 DEFAULT 1 3 Accelerate MaxTakeoff 10 1 842 183 747200 DEFAULT 1 4 Accelerate MaxClimb 5 1 000 2231.7.2015 EN Official Journal of the European Union L 168/319 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747200 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 747200 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 000 250 747200 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 747200 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 747200 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 747200 DEFAULT 2 1 Takeoff MaxTakeoff 10 747200 DEFAULT 2 2 Climb MaxTakeoff 10 1 000 747200 DEFAULT 2 3 Accelerate MaxTakeoff 10 1 757 186 747200 DEFAULT 2 4 Accelerate MaxClimb 5 1 000 226 747200 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 747200 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 000 250 747200 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 747200 DEFAULT 2 8 Climb MaxClimb ZERO 7 500 747200 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 747200 DEFAULT 3 1 Takeoff MaxTakeoff 10 747200 DEFAULT 3 2 Climb MaxTakeoff 10 1 000 747200 DEFAULT 3 3 Accelerate MaxTakeoff 10 1 676 189 747200 DEFAULT 3 4 Accelerate MaxClimb 5 1 000 229 747200 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 747200 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 000 250L 168/320 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747200 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 747200 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 747200 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 747200 DEFAULT 4 1 Takeoff MaxTakeoff 10 747200 DEFAULT 4 2 Climb MaxTakeoff 10 1 000 747200 DEFAULT 4 3 Accelerate MaxTakeoff 10 1 508 195 747200 DEFAULT 4 4 Accelerate MaxClimb 5 750 235 747200 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 747200 DEFAULT 4 6 Accelerate MaxClimb ZERO 750 255 747200 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 747200 DEFAULT 4 8 Climb MaxClimb ZERO 7 500 747200 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 747200 DEFAULT 5 1 Takeoff MaxTakeoff 10 747200 DEFAULT 5 2 Climb MaxTakeoff 10 1 000 747200 DEFAULT 5 3 Accelerate MaxTakeoff 10 1 325 203 747200 DEFAULT 5 4 Accelerate MaxClimb 5 750 243 747200 DEFAULT 5 5 Climb MaxClimb ZERO 3 000 747200 DEFAULT 5 6 Accelerate MaxClimb ZERO 750 263 747200 DEFAULT 5 7 Climb MaxClimb ZERO 5 500 747200 DEFAULT 5 8 Climb MaxClimb ZERO 7 5001.7.2015 EN Official Journal of the European Union L 168/321 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747200 DEFAULT 5 9 Climb MaxClimb ZERO 10 000 747200 DEFAULT 6 1 Takeoff MaxTakeoff 10 747200 DEFAULT 6 2 Climb MaxTakeoff 10 1 000 747200 DEFAULT 6 3 Accelerate MaxTakeoff 10 1 146 210 747200 DEFAULT 6 4 Accelerate MaxClimb 5 500 250 747200 DEFAULT 6 5 Climb MaxClimb ZERO 3 000 747200 DEFAULT 6 6 Accelerate MaxClimb ZERO 500 270 747200 DEFAULT 6 7 Climb MaxClimb ZERO 5 500 747200 DEFAULT 6 8 Climb MaxClimb ZERO 7 500 747200 DEFAULT 6 9 Climb MaxClimb ZERO 10 000 747200 DEFAULT 7 1 Takeoff MaxTakeoff 10 747200 DEFAULT 7 2 Climb MaxTakeoff 10 1 000 747200 DEFAULT 7 3 Accelerate MaxTakeoff 10 1 012 216 747200 DEFAULT 7 4 Accelerate MaxClimb 5 500 256 747200 DEFAULT 7 5 Accelerate MaxClimb ZERO 500 276 747200 DEFAULT 7 6 Climb MaxClimb ZERO 5 500 747200 DEFAULT 7 7 Climb MaxClimb ZERO 7 500 747200 DEFAULT 7 8 Climb MaxClimb ZERO 10 000 74720A DEFAULT 1 1 Takeoff MaxTakeoff 10 74720A DEFAULT 1 2 Climb MaxTakeoff 10 1 000L 168/322 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 74720A DEFAULT 1 3 Accelerate MaxTakeoff 10 2 068 176 74720A DEFAULT 1 4 Accelerate MaxClimb 5 1 000 239 74720A DEFAULT 1 5 Climb MaxClimb ZERO 3 000 74720A DEFAULT 1 6 Accelerate MaxClimb ZERO 1 000 259 74720A DEFAULT 1 7 Climb MaxClimb ZERO 5 500 74720A DEFAULT 1 8 Climb MaxClimb ZERO 7 500 74720A DEFAULT 1 9 Climb MaxClimb ZERO 10 000 74720A DEFAULT 2 1 Takeoff MaxTakeoff 10 74720A DEFAULT 2 2 Climb MaxTakeoff 10 1 000 74720A DEFAULT 2 3 Accelerate MaxTakeoff 10 1 950 179 74720A DEFAULT 2 4 Accelerate MaxClimb 5 1 000 242 74720A DEFAULT 2 5 Climb MaxClimb ZERO 3 000 74720A DEFAULT 2 6 Accelerate MaxClimb ZERO 1 000 262 74720A DEFAULT 2 7 Climb MaxClimb ZERO 5 500 74720A DEFAULT 2 8 Climb MaxClimb ZERO 7 500 74720A DEFAULT 2 9 Climb MaxClimb ZERO 10 000 74720A DEFAULT 3 1 Takeoff MaxTakeoff 10 74720A DEFAULT 3 2 Climb MaxTakeoff 10 1 000 74720A DEFAULT 3 3 Accelerate MaxTakeoff 10 1 862 182 74720A DEFAULT 3 4 Accelerate MaxClimb 5 1 000 2441.7.2015 EN Official Journal of the European Union L 168/323 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 74720A DEFAULT 3 5 Climb MaxClimb ZERO 3 000 74720A DEFAULT 3 6 Accelerate MaxClimb ZERO 1 000 264 74720A DEFAULT 3 7 Climb MaxClimb ZERO 5 500 74720A DEFAULT 3 8 Climb MaxClimb ZERO 7 500 74720A DEFAULT 3 9 Climb MaxClimb ZERO 10 000 74720A DEFAULT 4 1 Takeoff MaxTakeoff 10 74720A DEFAULT 4 2 Climb MaxTakeoff 10 1 000 74720A DEFAULT 4 3 Accelerate MaxTakeoff 10 1 700 188 74720A DEFAULT 4 4 Accelerate MaxClimb 5 750 248 74720A DEFAULT 4 5 Climb MaxClimb ZERO 3 000 74720A DEFAULT 4 6 Accelerate MaxClimb ZERO 750 268 74720A DEFAULT 4 7 Climb MaxClimb ZERO 5 500 74720A DEFAULT 4 8 Climb MaxClimb ZERO 7 500 74720A DEFAULT 4 9 Climb MaxClimb ZERO 10 000 74720A DEFAULT 5 1 Takeoff MaxTakeoff 10 74720A DEFAULT 5 2 Climb MaxTakeoff 10 1 000 74720A DEFAULT 5 3 Accelerate MaxTakeoff 10 1 520 195 74720A DEFAULT 5 4 Accelerate MaxClimb 5 750 254 74720A DEFAULT 5 5 Climb MaxClimb ZERO 3 000 74720A DEFAULT 5 6 Accelerate MaxClimb ZERO 750 274L 168/324 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 74720A DEFAULT 5 7 Climb MaxClimb ZERO 5 500 74720A DEFAULT 5 8 Climb MaxClimb ZERO 7 500 74720A DEFAULT 5 9 Climb MaxClimb ZERO 10 000 74720A DEFAULT 6 1 Takeoff MaxTakeoff 10 74720A DEFAULT 6 2 Climb MaxTakeoff 10 1 000 74720A DEFAULT 6 3 Accelerate MaxTakeoff 10 1 313 204 74720A DEFAULT 6 4 Accelerate MaxClimb 5 750 264 74720A DEFAULT 6 5 Accelerate MaxClimb ZERO 750 284 74720A DEFAULT 6 6 Climb MaxClimb ZERO 5 500 74720A DEFAULT 6 7 Climb MaxClimb ZERO 7 500 74720A DEFAULT 6 8 Climb MaxClimb ZERO 10 000 74720A DEFAULT 7 1 Takeoff MaxTakeoff 10 74720A DEFAULT 7 2 Climb MaxTakeoff 10 1 000 74720A DEFAULT 7 3 Accelerate MaxTakeoff 10 1 172 210 74720A DEFAULT 7 4 Accelerate MaxClimb 5 750 272 74720A DEFAULT 7 5 Accelerate MaxClimb ZERO 750 292 74720A DEFAULT 7 6 Climb MaxClimb ZERO 5 500 74720A DEFAULT 7 7 Climb MaxClimb ZERO 7 500 74720A DEFAULT 7 8 Climb MaxClimb ZERO 10 000 74720B DEFAULT 1 1 Takeoff MaxTakeoff 101.7.2015 EN Official Journal of the European Union L 168/325 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 74720B DEFAULT 1 2 Climb MaxTakeoff 10 1 000 74720B DEFAULT 1 3 Accelerate MaxTakeoff 10 2 497 184 74720B DEFAULT 1 4 Accelerate MaxClimb 5 1 000 244 74720B DEFAULT 1 5 Climb MaxClimb ZERO 3 000 74720B DEFAULT 1 6 Accelerate MaxClimb ZERO 1 000 264 74720B DEFAULT 1 7 Climb MaxClimb ZERO 5 500 74720B DEFAULT 1 8 Climb MaxClimb ZERO 7 500 74720B DEFAULT 1 9 Climb MaxClimb ZERO 10 000 74720B DEFAULT 2 1 Takeoff MaxTakeoff 10 74720B DEFAULT 2 2 Climb MaxTakeoff 10 1 000 74720B DEFAULT 2 3 Accelerate MaxTakeoff 10 2 397 187 74720B DEFAULT 2 4 Accelerate MaxClimb 5 1 000 246 74720B DEFAULT 2 5 Climb MaxClimb ZERO 3 000 74720B DEFAULT 2 6 Accelerate MaxClimb ZERO 1 000 266 74720B DEFAULT 2 7 Climb MaxClimb ZERO 5 500 74720B DEFAULT 2 8 Climb MaxClimb ZERO 7 500 74720B DEFAULT 2 9 Climb MaxClimb ZERO 10 000 74720B DEFAULT 3 1 Takeoff MaxTakeoff 10 74720B DEFAULT 3 2 Climb MaxTakeoff 10 1 000 74720B DEFAULT 3 3 Accelerate MaxTakeoff 10 2 303 190L 168/326 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 74720B DEFAULT 3 4 Accelerate MaxClimb 5 750 249 74720B DEFAULT 3 5 Climb MaxClimb ZERO 3 000 74720B DEFAULT 3 6 Accelerate MaxClimb ZERO 750 269 74720B DEFAULT 3 7 Climb MaxClimb ZERO 5 500 74720B DEFAULT 3 8 Climb MaxClimb ZERO 7 500 74720B DEFAULT 3 9 Climb MaxClimb ZERO 10 000 74720B DEFAULT 4 1 Takeoff MaxTakeoff 10 74720B DEFAULT 4 2 Climb MaxTakeoff 10 1 000 74720B DEFAULT 4 3 Accelerate MaxTakeoff 10 2 109 196 74720B DEFAULT 4 4 Accelerate MaxClimb 5 750 254 74720B DEFAULT 4 5 Climb MaxClimb ZERO 3 000 74720B DEFAULT 4 6 Accelerate MaxClimb ZERO 750 274 74720B DEFAULT 4 7 Climb MaxClimb ZERO 5 500 74720B DEFAULT 4 8 Climb MaxClimb ZERO 7 500 74720B DEFAULT 4 9 Climb MaxClimb ZERO 10 000 74720B DEFAULT 5 1 Takeoff MaxTakeoff 10 74720B DEFAULT 5 2 Climb MaxTakeoff 10 1 000 74720B DEFAULT 5 3 Accelerate MaxTakeoff 10 1 900 204 74720B DEFAULT 5 4 Accelerate MaxClimb 5 750 263 74720B DEFAULT 5 5 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/327 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 74720B DEFAULT 5 6 Accelerate MaxClimb ZERO 750 283 74720B DEFAULT 5 7 Climb MaxClimb ZERO 5 500 74720B DEFAULT 5 8 Climb MaxClimb ZERO 7 500 74720B DEFAULT 5 9 Climb MaxClimb ZERO 10 000 74720B DEFAULT 6 1 Takeoff MaxTakeoff 10 74720B DEFAULT 6 2 Climb MaxTakeoff 10 1 000 74720B DEFAULT 6 3 Accelerate MaxTakeoff 10 1 699 211 74720B DEFAULT 6 4 Accelerate MaxClimb 5 750 272 74720B DEFAULT 6 5 Climb MaxClimb ZERO 3 000 74720B DEFAULT 6 6 Accelerate MaxClimb ZERO 750 292 74720B DEFAULT 6 7 Climb MaxClimb ZERO 5 500 74720B DEFAULT 6 8 Climb MaxClimb ZERO 7 500 74720B DEFAULT 6 9 Climb MaxClimb ZERO 10 000 74720B DEFAULT 7 1 Takeoff MaxTakeoff 10 74720B DEFAULT 7 2 Climb MaxTakeoff 10 1 000 74720B DEFAULT 7 3 Accelerate MaxTakeoff 10 1 547 218 74720B DEFAULT 7 4 Accelerate MaxClimb 5 750 279 74720B DEFAULT 7 5 Accelerate MaxClimb ZERO 750 299 74720B DEFAULT 7 6 Climb MaxClimb ZERO 5 500 74720B DEFAULT 7 7 Climb MaxClimb ZERO 7 500L 168/328 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 74720B DEFAULT 7 8 Climb MaxClimb ZERO 10 000 747400 DEFAULT 1 1 Takeoff MaxTakeoff 10 747400 DEFAULT 1 2 Climb MaxTakeoff T_10 1 000 747400 DEFAULT 1 3 Accelerate MaxClimb 10 1 533,3 190,8 747400 DEFAULT 1 4 Accelerate MaxClimb T_05 1 798,9 242 747400 DEFAULT 1 5 Climb MaxClimb 5 3 869 747400 DEFAULT 1 6 Accelerate MaxClimb ZERO 2 198,9 269 747400 DEFAULT 1 7 Climb MaxClimb T_00H 5 500 747400 DEFAULT 1 8 Climb MaxClimb T_00H 7 500 747400 DEFAULT 1 9 Climb MaxClimb T_00H 10 000 747400 DEFAULT 2 1 Takeoff MaxTakeoff 10 747400 DEFAULT 2 2 Climb MaxTakeoff T_10 1 000 747400 DEFAULT 2 3 Accelerate MaxClimb 10 1 507,6 192,9 747400 DEFAULT 2 4 Accelerate MaxClimb T_05 1 718,8 244,6 747400 DEFAULT 2 5 Climb MaxClimb T_01 3 756 747400 DEFAULT 2 6 Accelerate MaxClimb T_00H 2 111,9 269 747400 DEFAULT 2 7 Climb MaxClimb T_00H 5 500 747400 DEFAULT 2 8 Climb MaxClimb T_00H 7 500 747400 DEFAULT 2 9 Climb MaxClimb T_00H 10 000 747400 DEFAULT 3 1 Takeoff MaxTakeoff 101.7.2015 EN Official Journal of the European Union L 168/329 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 DEFAULT 3 2 Climb MaxTakeoff T_10 1 000 747400 DEFAULT 3 3 Accelerate MaxClimb 10 1 412,1 195,1 747400 DEFAULT 3 4 Accelerate MaxClimb T_05 1 660,4 247,2 747400 DEFAULT 3 5 Climb MaxClimb T_01 3 637 747400 DEFAULT 3 6 Accelerate MaxClimb ZERO 2 033,6 269 747400 DEFAULT 3 7 Climb MaxClimb T_00H 5 500 747400 DEFAULT 3 8 Climb MaxClimb T_00H 7 500 747400 DEFAULT 3 9 Climb MaxClimb T_00H 10 000 747400 DEFAULT 4 1 Takeoff MaxTakeoff 10 747400 DEFAULT 4 2 Climb MaxTakeoff T_10 1 000 747400 DEFAULT 4 3 Accelerate MaxClimb 10 1 310,5 199,4 747400 DEFAULT 4 4 Accelerate MaxClimb T_05 1 531,8 252,3 747400 DEFAULT 4 5 Climb MaxClimb T_01 3 435 747400 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 882,8 269 747400 DEFAULT 4 7 Climb MaxClimb T_00H 5 500 747400 DEFAULT 4 8 Climb MaxClimb T_00H 7 500 747400 DEFAULT 4 9 Climb MaxClimb T_00H 10 000 747400 DEFAULT 5 1 Takeoff MaxTakeoff 10 747400 DEFAULT 5 2 Climb MaxTakeoff T_10 1 000 747400 DEFAULT 5 3 Accelerate MaxClimb 10 1 182,2 204,8L 168/330 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 DEFAULT 5 4 Accelerate MaxClimb T_05 1 402,6 258,4 747400 DEFAULT 5 5 Climb MaxClimb T_01 3 199 747400 DEFAULT 5 6 Accelerate MaxClimb ZERO 1 724,1 269 747400 DEFAULT 5 7 Climb MaxClimb T_00H 5 500 747400 DEFAULT 5 8 Climb MaxClimb T_00H 7 500 747400 DEFAULT 5 9 Climb MaxClimb ZERO 10 000 747400 DEFAULT 6 1 Takeoff MaxTakeoff 10 747400 DEFAULT 6 2 Climb MaxTakeoff T_10 1 000 747400 DEFAULT 6 3 Accelerate MaxClimb 5 1 088,1 210,4 747400 DEFAULT 6 4 Accelerate MaxClimb 5 1 372 259,5 747400 DEFAULT 6 5 Accelerate MaxClimb T_01 1 432,4 264,7 747400 DEFAULT 6 6 Climb MaxClimb T_01 3 004 747400 DEFAULT 6 7 Accelerate MaxClimb ZERO 1 560 269 747400 DEFAULT 6 8 Climb MaxClimb T_00H 5 500 747400 DEFAULT 6 9 Climb MaxClimb T_00H 7 500 747400 DEFAULT 6 10 Climb MaxClimb T_00H 10 000 747400 DEFAULT 7 1 Takeoff MaxTakeoff 10 747400 DEFAULT 7 2 Climb MaxTakeoff T_10H 1 000 747400 DEFAULT 7 3 Accelerate MaxClimb 10 963,6 216,4 747400 DEFAULT 7 4 Accelerate MaxClimb 5 1 114,2 259,61.7.2015 EN Official Journal of the European Union L 168/331 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 DEFAULT 7 5 Climb MaxClimb T_01 2 544 747400 DEFAULT 7 6 Accelerate MaxClimb T_05 1 329,4 270 747400 DEFAULT 7 7 Climb MaxClimb T_00H 5 500 747400 DEFAULT 7 8 Climb MaxClimb T_00H 7 500 747400 DEFAULT 7 9 Climb MaxClimb T_00H 10 000 747400 DEFAULT 8 1 Takeoff MaxTakeoff 10 747400 DEFAULT 8 2 Climb MaxTakeoff T_10H 1 000 747400 DEFAULT 8 3 Accelerate MaxClimb 10 855,6 222,8 747400 DEFAULT 8 4 Accelerate MaxClimb 5 968,9 259,6 747400 DEFAULT 8 5 Climb MaxClimb T_01 2 561 747400 DEFAULT 8 6 Accelerate MaxClimb T_01 1 173,1 270 747400 DEFAULT 8 7 Accelerate MaxClimb T_00H 1 260 278 747400 DEFAULT 8 8 Climb MaxClimb T_00H 5 500 747400 DEFAULT 8 9 Climb MaxClimb T_00H 7 500 747400 DEFAULT 8 10 Climb MaxClimb T_00H 10 000 747400 DEFAULT 9 1 Takeoff MaxTakeoff 10 747400 DEFAULT 9 2 Climb MaxTakeoff T_10H 1 000 747400 DEFAULT 9 3 Accelerate MaxClimb 10 783,8 226,8 747400 DEFAULT 9 4 Accelerate MaxClimb 5 884,5 259,6 747400 DEFAULT 9 5 Climb MaxClimb T_01 2 600L 168/332 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 DEFAULT 9 6 Accelerate MaxClimb T_01 1 078,7 271,8 747400 DEFAULT 9 7 Accelerate MaxClimb T_00H 1 182,6 282,7 747400 DEFAULT 9 8 Climb MaxClimb T_00H 5 500 747400 DEFAULT 9 9 Climb MaxClimb T_00H 7 500 747400 DEFAULT 9 10 Climb MaxClimb T_00H 10 000 747400 ICAO_A 1 1 Takeoff MaxTakeoff 10 747400 ICAO_A 1 2 Climb MaxTakeoff T_10 1 500 747400 ICAO_A 1 3 Climb MaxClimb 10 3 000 747400 ICAO_A 1 4 Accelerate MaxClimb 10 1 472,8 190 747400 ICAO_A 1 5 Accelerate MaxClimb 5 1 753,3 241,7 747400 ICAO_A 1 6 Climb MaxClimb T_01 5 796 747400 ICAO_A 1 7 Accelerate MaxClimb ZERO 2 158,4 268,4 747400 ICAO_A 1 8 Climb MaxClimb ZERO 7 500 747400 ICAO_A 1 9 Climb MaxClimb ZERO 10 000 747400 ICAO_A 2 1 Takeoff MaxTakeoff 10 747400 ICAO_A 2 2 Climb MaxTakeoff T_10 1 500 747400 ICAO_A 2 3 Climb MaxClimb 10 3 000 747400 ICAO_A 2 4 Accelerate MaxClimb 10 1 412,8 192,2 747400 ICAO_A 2 5 Accelerate MaxClimb 5 1 689,5 244,3 747400 ICAO_A 2 6 Climb MaxClimb T_01 5 6851.7.2015 EN Official Journal of the European Union L 168/333 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 ICAO_A 2 7 Accelerate MaxClimb ZERO 2 078,8 268,4 747400 ICAO_A 2 8 Climb MaxClimb ZERO 7 500 747400 ICAO_A 2 9 Climb MaxClimb ZERO 10 000 747400 ICAO_A 3 1 Takeoff MaxTakeoff 10 747400 ICAO_A 3 2 Climb MaxTakeoff T_10 1 500 747400 ICAO_A 3 3 Climb MaxClimb 10 3 000 747400 ICAO_A 3 4 Accelerate MaxClimb 10 1 353,5 194,4 747400 ICAO_A 3 5 Accelerate MaxClimb 5 1 618,4 246,8 747400 ICAO_A 3 6 Climb MaxClimb T_01 5 579 747400 ICAO_A 3 7 Accelerate MaxClimb ZERO 1 995 268,4 747400 ICAO_A 3 8 Climb MaxClimb ZERO 7 500 747400 ICAO_A 3 9 Climb MaxClimb ZERO 10 000 747400 ICAO_A 4 1 Takeoff MaxTakeoff 10 747400 ICAO_A 4 2 Climb MaxTakeoff T_10 1 500 747400 ICAO_A 4 3 Climb MaxClimb 10 3 000 747400 ICAO_A 4 4 Accelerate MaxClimb 10 1 249,3 198,7 747400 ICAO_A 4 5 Accelerate MaxClimb 5 1 500,4 251,9 747400 ICAO_A 4 6 Climb MaxClimb T_01 5 372 747400 ICAO_A 4 7 Accelerate MaxClimb ZERO 1 847,9 268,4 747400 ICAO_A 4 8 Climb MaxClimb ZERO 7 500L 168/334 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 ICAO_A 4 9 Climb MaxClimb ZERO 10 000 747400 ICAO_A 5 1 Takeoff MaxTakeoff 10 747400 ICAO_A 5 2 Climb MaxTakeoff T_10 1 500 747400 ICAO_A 5 3 Climb MaxClimb 10 3 000 747400 ICAO_A 5 4 Accelerate MaxClimb 10 1 131,2 204,1 747400 ICAO_A 5 5 Accelerate MaxClimb 5 1 367,5 257,8 747400 ICAO_A 5 6 Climb MaxClimb T_01 5 145 747400 ICAO_A 5 7 Accelerate MaxClimb ZERO 1 686,7 268,4 747400 ICAO_A 5 8 Climb MaxClimb ZERO 7 500 747400 ICAO_A 5 9 Climb MaxClimb ZERO 10 000 747400 ICAO_A 6 1 Takeoff MaxTakeoff 10 747400 ICAO_A 6 2 Climb MaxTakeoff T_10H 1 500 747400 ICAO_A 6 3 Climb MaxClimb 10 3 000 747400 ICAO_A 6 4 Accelerate MaxClimb 10 1 017,7 209,8 747400 ICAO_A 6 5 Accelerate MaxClimb 5 1 223,8 259,1 747400 ICAO_A 6 6 Climb MaxClimb T_01 4 508 747400 ICAO_A 6 7 Accelerate MaxClimb T_01 1 416 264,3 747400 ICAO_A 6 8 Climb MaxClimb ZERO 4 921 747400 ICAO_A 6 9 Accelerate MaxClimb ZERO 1 531 269 747400 ICAO_A 6 10 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/335 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 ICAO_A 6 11 Climb MaxClimb ZERO 7 500 747400 ICAO_A 6 12 Climb MaxClimb ZERO 10 000 747400 ICAO_A 7 1 Takeoff MaxTakeoff 10 747400 ICAO_A 7 2 Climb MaxTakeoff T_10H 1 500 747400 ICAO_A 7 3 Climb MaxClimb 10 3 000 747400 ICAO_A 7 4 Accelerate MaxClimb 10 908,3 215,8 747400 ICAO_A 7 5 Accelerate MaxClimb 5 1 082,4 259,1 747400 ICAO_A 7 6 Climb MaxClimb T_01 4 509 747400 ICAO_A 7 7 Accelerate MaxClimb T_01 1 308,4 269,1 747400 ICAO_A 7 8 Accelerate MaxClimb ZERO 1 365,5 271 747400 ICAO_A 7 9 Climb MaxClimb ZERO 5 500 747400 ICAO_A 7 10 Climb MaxClimb ZERO 7 500 747400 ICAO_A 7 11 Climb MaxClimb T_00H 10 000 747400 ICAO_A 8 1 Takeoff MaxTakeoff 10 747400 ICAO_A 8 2 Climb MaxTakeoff T_10H 1 500 747400 ICAO_A 8 3 Climb MaxClimb 10 3 000 747400 ICAO_A 8 4 Accelerate MaxClimb 10 801,1 222,2 747400 ICAO_A 8 5 Accelerate MaxClimb 5 942,7 259,1 747400 ICAO_A 8 6 Climb MaxClimb T_01 4 540 747400 ICAO_A 8 7 Accelerate MaxClimb T_01 1 146,3 267,9L 168/336 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 ICAO_A 8 8 Accelerate MaxClimb ZERO 1 230 277,7 747400 ICAO_A 8 9 Climb MaxClimb ZERO 5 500 747400 ICAO_A 8 10 Climb MaxClimb T_00H 7 500 747400 ICAO_A 8 11 Climb MaxClimb T_00H 10 000 747400 ICAO_A 9 1 Takeoff MaxTakeoff 10 747400 ICAO_A 9 2 Climb MaxTakeoff T_10H 1 500 747400 ICAO_A 9 3 Climb MaxClimb 10 3 000 747400 ICAO_A 9 4 Accelerate MaxClimb 10 734,4 226,3 747400 ICAO_A 9 5 Accelerate MaxClimb 5 858,9 259,1 747400 ICAO_A 9 6 Climb MaxClimb T_01 4 590 747400 ICAO_A 9 7 Accelerate MaxClimb T_01 1 051,2 270,6 747400 ICAO_A 9 8 Accelerate MaxClimb T_00H 1 143 282,2 747400 ICAO_A 9 9 Climb MaxClimb T_00H 5 500 747400 ICAO_A 9 10 Climb MaxClimb T_00H 7 500 747400 ICAO_A 9 11 Climb MaxClimb T_00H 10 000 747400 ICAO_B 1 1 Takeoff MaxTakeoff 10 747400 ICAO_B 1 2 Climb MaxTakeoff T_10 1 000 747400 ICAO_B 1 3 Accelerate MaxTakeoff 10 1 890,2 182,3 747400 ICAO_B 1 4 Climb MaxTakeoff 10 1 646 747400 ICAO_B 1 5 Accelerate MaxClimb T_05 1 788,2 2421.7.2015 EN Official Journal of the European Union L 168/337 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 ICAO_B 1 6 Climb MaxClimb T_05 4 194 747400 ICAO_B 1 7 Accelerate MaxClimb ZERO 2 170,6 259 747400 ICAO_B 1 8 Climb MaxClimb ZERO 5 500 747400 ICAO_B 1 9 Climb MaxClimb ZERO 7 500 747400 ICAO_B 1 10 Climb MaxClimb ZERO 10 000 747400 ICAO_B 2 1 Takeoff MaxTakeoff 10 747400 ICAO_B 2 2 Climb MaxTakeoff T_10 1 000 747400 ICAO_B 2 3 Accelerate MaxTakeoff 10 1 836,7 184,9 747400 ICAO_B 2 4 Climb MaxTakeoff 10 1 640 747400 ICAO_B 2 5 Accelerate MaxClimb T_05 1 727,1 244,6 747400 ICAO_B 2 6 Climb MaxClimb T_05 4 067 747400 ICAO_B 2 7 Accelerate MaxClimb ZERO 2 088,1 259,2 747400 ICAO_B 2 8 Climb MaxClimb ZERO 5 500 747400 ICAO_B 2 9 Climb MaxClimb ZERO 7 500 747400 ICAO_B 2 10 Climb MaxClimb ZERO 10 000 747400 ICAO_B 3 1 Takeoff MaxTakeoff 10 747400 ICAO_B 3 2 Climb MaxTakeoff T_10 1 000 747400 ICAO_B 3 3 Accelerate MaxTakeoff 10 1 777,6 187,5 747400 ICAO_B 3 4 Climb MaxTakeoff 10 1 637 747400 ICAO_B 3 5 Accelerate MaxClimb T_05 1 653,3 247,2L 168/338 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 ICAO_B 3 6 Climb MaxClimb T_05C 3 942 747400 ICAO_B 3 7 Accelerate MaxClimb ZERO 2 009,7 259,2 747400 ICAO_B 3 8 Climb MaxClimb ZERO 5 500 747400 ICAO_B 3 9 Climb MaxClimb ZERO 7 500 747400 ICAO_B 3 10 Climb MaxClimb ZERO 10 000 747400 ICAO_B 4 1 Takeoff MaxTakeoff 10 747400 ICAO_B 4 2 Climb MaxTakeoff T_10 1 000 747400 ICAO_B 4 3 Accelerate MaxTakeoff 10 1 653,5 192,6 747400 ICAO_B 4 4 Climb MaxTakeoff 10 1 633 747400 ICAO_B 4 5 Accelerate MaxClimb T_05 1 535,2 252,2 747400 ICAO_B 4 6 Climb MaxClimb T_05C 3 718 747400 ICAO_B 4 7 Accelerate MaxClimb ZERO 1 858,5 259,2 747400 ICAO_B 4 8 Climb MaxClimb ZERO 5 500 747400 ICAO_B 4 9 Climb MaxClimb ZERO 7 500 747400 ICAO_B 4 10 Climb MaxClimb ZERO 10 000 747400 ICAO_B 5 1 Takeoff MaxTakeoff 10 747400 ICAO_B 5 2 Climb MaxTakeoff T_10 1 000 747400 ICAO_B 5 3 Accelerate MaxTakeoff 10 1 518,3 198,7 747400 ICAO_B 5 4 Climb MaxTakeoff 10 1 619 747400 ICAO_B 5 5 Accelerate MaxClimb T_05 1 397,6 258,31.7.2015 EN Official Journal of the European Union L 168/339 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 ICAO_B 5 6 Climb MaxClimb T_05C 3 459 747400 ICAO_B 5 7 Accelerate MaxClimb ZERO 1 685,4 259,4 747400 ICAO_B 5 8 Climb MaxClimb ZERO 5 500 747400 ICAO_B 5 9 Climb MaxClimb ZERO 7 500 747400 ICAO_B 5 10 Climb MaxClimb ZERO 10 000 747400 ICAO_B 6 1 Takeoff MaxTakeoff 10 747400 ICAO_B 6 2 Climb MaxTakeoff T_10 1 000 747400 ICAO_B 6 3 Accelerate MaxTakeoff 10 1 394,6 205,1 747400 ICAO_B 6 4 Climb MaxTakeoff T_05C 1 606 747400 ICAO_B 6 5 Accelerate MaxClimb T_05 1 346,5 264,7 747400 ICAO_B 6 6 Climb MaxClimb T_05C 3 217 747400 ICAO_B 6 7 Accelerate MaxClimb ZERO 1 560 269,2 747400 ICAO_B 6 8 Climb MaxClimb ZERO 5 500 747400 ICAO_B 6 9 Climb MaxClimb ZERO 7 500 747400 ICAO_B 6 10 Climb MaxClimb ZERO 10 000 747400 ICAO_B 7 1 Takeoff MaxTakeoff 10 747400 ICAO_B 7 2 Climb MaxTakeoff T_10H 1 000 747400 ICAO_B 7 3 Accelerate MaxTakeoff 10 1 271 211,9 747400 ICAO_B 7 4 Climb MaxTakeoff T_05 1 597 747400 ICAO_B 7 5 Accelerate MaxClimb T_05 1 112,4 259,4L 168/340 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 ICAO_B 7 6 Climb MaxClimb T_05C 2 759 747400 ICAO_B 7 7 Accelerate MaxClimb T_01 1 323,5 271,4 747400 ICAO_B 7 8 Climb MaxClimb ZERO 5 500 747400 ICAO_B 7 9 Climb MaxClimb T_00H 7 500 747400 ICAO_B 7 10 Climb MaxClimb T_00H 10 000 747400 ICAO_B 8 1 Takeoff MaxTakeoff 10 747400 ICAO_B 8 2 Climb MaxTakeoff T_10H 1 000 747400 ICAO_B 8 3 Accelerate MaxTakeoff 10 1 147 218,9 747400 ICAO_B 8 4 Climb MaxTakeoff T_05 1 592 747400 ICAO_B 8 5 Accelerate MaxClimb T_05 975,2 259,6 747400 ICAO_B 8 6 Climb MaxClimb T_05C 2 755 747400 ICAO_B 8 7 Accelerate MaxClimb T_01 1 209,5 278,4 747400 ICAO_B 8 8 Climb MaxClimb T_00H 5 500 747400 ICAO_B 8 9 Climb MaxClimb T_00H 7 500 747400 ICAO_B 8 10 Climb MaxClimb T_00H 10 000 747400 ICAO_B 9 1 Takeoff MaxTakeoff 10 747400 ICAO_B 9 2 Climb MaxTakeoff T_10H 1 000 747400 ICAO_B 9 3 Accelerate MaxTakeoff 10 1 070,9 223,3 747400 ICAO_B 9 4 Climb MaxTakeoff 10 1 611 747400 ICAO_B 9 5 Accelerate MaxClimb T_05 893,7 259,51.7.2015 EN Official Journal of the European Union L 168/341 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747400 ICAO_B 9 6 Climb MaxClimb T_01 2 782 747400 ICAO_B 9 7 Accelerate MaxClimb T_01 1 119,3 282,7 747400 ICAO_B 9 8 Climb MaxClimb T_00H 5 500 747400 ICAO_B 9 9 Climb MaxClimb T_00H 7 500 747400 ICAO_B 9 10 Climb MaxClimb T_00H 10 000 7478 DEFAULT 1 1 Takeoff MaxTakeoff F_10 7478 DEFAULT 1 2 Climb MaxTakeoff F_10 1 000 7478 DEFAULT 1 3 Accelerate_ MaxClimb F_10 215 55 Percent 7478 DEFAULT 1 4 Accelerate_ MaxClimb F_5 250 55 Percent 7478 DEFAULT 1 5 Accelerate_ MaxClimb F_1 260 55 Percent 7478 DEFAULT 1 6 Climb MaxClimb F_0 3 000 7478 DEFAULT 1 7 Accelerate_ MaxClimb F_0 295 50 Percent 7478 DEFAULT 1 8 Climb MaxClimb F_0 10 000 7478 DEFAULT 2 1 Takeoff MaxTakeoff F_10 7478 DEFAULT 2 2 Climb MaxTakeoff F_10 1 000 7478 DEFAULT 2 3 Accelerate_ MaxClimb F_10 215 55 Percent 7478 DEFAULT 2 4 Accelerate_ MaxClimb F_5 250 55 Percent 7478 DEFAULT 2 5 Accelerate_ MaxClimb F_1 260 55 Percent 7478 DEFAULT 2 6 Climb MaxClimb F_0 3 000 7478 DEFAULT 2 7 Accelerate_ MaxClimb F_0 295 50 PercentL 168/342 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7478 DEFAULT 2 8 Climb MaxClimb F_0 10 000 7478 DEFAULT 3 1 Takeoff MaxTakeoff F_10 7478 DEFAULT 3 2 Climb MaxTakeoff F_10 1 000 7478 DEFAULT 3 3 Accelerate_ MaxClimb F_10 215 55 Percent 7478 DEFAULT 3 4 Accelerate_ MaxClimb F_5 250 55 Percent 7478 DEFAULT 3 5 Accelerate_ MaxClimb F_1 260 55 Percent 7478 DEFAULT 3 6 Climb MaxClimb F_0 3 000 7478 DEFAULT 3 7 Accelerate_ MaxClimb F_0 295 50 Percent 7478 DEFAULT 3 8 Climb MaxClimb F_0 10 000 7478 DEFAULT 4 1 Takeoff MaxTakeoff F_10 7478 DEFAULT 4 2 Climb MaxTakeoff F_10 1 000 7478 DEFAULT 4 3 Accelerate_ MaxClimb F_10 220 55 Percent 7478 DEFAULT 4 4 Accelerate_ MaxClimb F_5 250 55 Percent 7478 DEFAULT 4 5 Accelerate_ MaxClimb F_1 268 55 Percent 7478 DEFAULT 4 6 Climb MaxClimb F_0 3 000 7478 DEFAULT 4 7 Accelerate_ MaxClimb F_0 295 50 Percent 7478 DEFAULT 4 8 Climb MaxClimb F_0 10 000 7478 DEFAULT 5 1 Takeoff MaxTakeoff F_10 7478 DEFAULT 5 2 Climb MaxTakeoff F_10 1 000 7478 DEFAULT 5 3 Accelerate_ MaxClimb F_10 220 55 Percent1.7.2015 EN Official Journal of the European Union L 168/343 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7478 DEFAULT 5 4 Accelerate_ MaxClimb F_5 250 55 Percent 7478 DEFAULT 5 5 Accelerate_ MaxClimb F_1 270 55 Percent 7478 DEFAULT 5 6 Climb MaxClimb F_0 3 000 7478 DEFAULT 5 7 Accelerate_ MaxClimb F_0 295 50 Percent 7478 DEFAULT 5 8 Climb MaxClimb F_0 10 000 7478 DEFAULT 6 1 Takeoff MaxTakeoff F_10 7478 DEFAULT 6 2 Climb MaxTakeoff F_10 1 000 7478 DEFAULT 6 3 Accelerate_ MaxClimb F_10 227 55 Percent 7478 DEFAULT 6 4 Accelerate_ MaxClimb F_5 258 55 Percent 7478 DEFAULT 6 5 Accelerate_ MaxClimb F_1 270 55 Percent 7478 DEFAULT 6 6 Climb MaxClimb F_0 3 000 7478 DEFAULT 6 7 Accelerate_ MaxClimb F_0 295 50 Percent 7478 DEFAULT 6 8 Climb MaxClimb F_0 10 000 7478 DEFAULT 7 1 Takeoff MaxTakeoff F_10 7478 DEFAULT 7 2 Climb MaxTakeoff F_10 1 000 7478 DEFAULT 7 3 Accelerate_ MaxClimb F_10 230 55 Percent 7478 DEFAULT 7 4 Accelerate_ MaxClimb F_5 260 55 Percent 7478 DEFAULT 7 5 Accelerate_ MaxClimb F_1 275 55 Percent 7478 DEFAULT 7 6 Climb MaxClimb F_0 3 000 7478 DEFAULT 7 7 Accelerate_ MaxClimb F_0 295 50 PercentL 168/344 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7478 DEFAULT 7 8 Climb MaxClimb F_0 10 000 7478 DEFAULT 8 1 Takeoff MaxTakeoff F_10 7478 DEFAULT 8 2 Climb MaxTakeoff F_10 1 000 7478 DEFAULT 8 3 Accelerate_ MaxClimb F_10 235 55 Percent 7478 DEFAULT 8 4 Accelerate_ MaxClimb F_5 265 55 Percent 7478 DEFAULT 8 5 Accelerate_ MaxClimb F_1 280 55 Percent 7478 DEFAULT 8 6 Climb MaxClimb F_0 3 000 7478 DEFAULT 8 7 Accelerate_ MaxClimb F_0 295 50 Percent 7478 DEFAULT 8 8 Climb MaxClimb F_0 10 000 7478 DEFAULT 9 1 Takeoff MaxTakeoff F_10 7478 DEFAULT 9 2 Climb MaxTakeoff F_10 1 000 7478 DEFAULT 9 3 Accelerate_ MaxClimb F_10 235 55 Percent 7478 DEFAULT 9 4 Accelerate_ MaxClimb F_5 265 55 Percent 7478 DEFAULT 9 5 Accelerate_ MaxClimb F_1 280 55 Percent 7478 DEFAULT 9 6 Climb MaxClimb F_0 3 000 7478 DEFAULT 9 7 Accelerate_ MaxClimb F_0 295 50 Percent 7478 DEFAULT 9 8 Climb MaxClimb F_0 10 000 7478 ICAO_A 1 1 Takeoff MaxTakeoff F_10 7478 ICAO_A 1 2 Climb MaxTakeoff F_10 1 500 7478 ICAO_A 1 3 Climb MaxClimb F_10 3 0001.7.2015 EN Official Journal of the European Union L 168/345 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7478 ICAO_A 1 4 Accelerate_ MaxClimb F_10 220 55 Percent 7478 ICAO_A 1 5 Accelerate_ MaxClimb F_5 250 55 Percent 7478 ICAO_A 1 6 Climb MaxClimb F_1 4 700 7478 ICAO_A 1 7 Accelerate_ MaxClimb F_0 276 50 Percent 7478 ICAO_A 1 8 Climb MaxClimb F_0 10 000 7478 ICAO_A 2 1 Takeoff MaxTakeoff F_10 7478 ICAO_A 2 2 Climb MaxTakeoff F_10 1 500 7478 ICAO_A 2 3 Climb MaxClimb F_10 3 000 7478 ICAO_A 2 4 Accelerate_ MaxClimb F_10 220 55 Percent 7478 ICAO_A 2 5 Accelerate_ MaxClimb F_1 254 55 Percent 7478 ICAO_A 2 6 Climb MaxClimb F_1 4 800 7478 ICAO_A 2 7 Accelerate_ MaxClimb F_0 275 50 Percent 7478 ICAO_A 2 8 Climb MaxClimb F_0 10 000 7478 ICAO_A 3 1 Takeoff MaxTakeoff F_10 7478 ICAO_A 3 2 Climb MaxTakeoff F_10 1 500 7478 ICAO_A 3 3 Climb MaxClimb F_10 3 000 7478 ICAO_A 3 4 Accelerate_ MaxClimb F_5 220 55 Percent 7478 ICAO_A 3 5 Accelerate_ MaxClimb F_1 255 55 Percent 7478 ICAO_A 3 6 Climb MaxClimb F_1 4 500 7478 ICAO_A 3 7 Accelerate_ MaxClimb F_0 275 50 PercentL 168/346 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7478 ICAO_A 3 8 Climb MaxClimb F_0 10 000 7478 ICAO_A 4 1 Takeoff MaxTakeoff F_10 7478 ICAO_A 4 2 Climb MaxTakeoff F_10 1 500 7478 ICAO_A 4 3 Climb MaxClimb F_10 3 000 7478 ICAO_A 4 4 Accelerate_ MaxClimb F_10 220 55 Percent 7478 ICAO_A 4 5 Accelerate_ MaxClimb F_5 255 55 Percent 7478 ICAO_A 4 6 Accelerate_ MaxClimb F_1 275 55 Percent 7478 ICAO_A 4 7 Climb MaxClimb F_0 10 000 7478 ICAO_A 5 1 Takeoff MaxTakeoff F_10 7478 ICAO_A 5 2 Climb MaxTakeoff F_10 1 500 7478 ICAO_A 5 3 Climb MaxClimb F_10 3 000 7478 ICAO_A 5 4 Accelerate_ MaxClimb F_5 220 55 Percent 7478 ICAO_A 5 5 Accelerate_ MaxClimb F_1 255 55 Percent 7478 ICAO_A 5 6 Accelerate_ MaxClimb F_0 275 50 Percent 7478 ICAO_A 5 7 Climb MaxClimb F_0 10 000 7478 ICAO_A 6 1 Takeoff MaxTakeoff F_10 7478 ICAO_A 6 2 Climb MaxTakeoff F_10 1 500 7478 ICAO_A 6 3 Climb MaxClimb F_10 3 000 7478 ICAO_A 6 4 Accelerate_ MaxClimb F_5 225 55 Percent 7478 ICAO_A 6 5 Accelerate_ MaxClimb F_1 255 55 Percent1.7.2015 EN Official Journal of the European Union L 168/347 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7478 ICAO_A 6 6 Accelerate_ MaxClimb F_0 278 50 Percent 7478 ICAO_A 6 7 Climb MaxClimb F_0 10 000 7478 ICAO_A 7 1 Takeoff MaxTakeoff F_10 7478 ICAO_A 7 2 Climb MaxTakeoff F_10 1 500 7478 ICAO_A 7 3 Climb MaxClimb F_10 3 000 7478 ICAO_A 7 4 Accelerate_ MaxClimb F_5 225 55 Percent 7478 ICAO_A 7 5 Accelerate_ MaxClimb F_1 255 55 Percent 7478 ICAO_A 7 6 Accelerate_ MaxClimb F_0 278 50 Percent 7478 ICAO_A 7 7 Climb MaxClimb F_0 10 000 7478 ICAO_A 8 1 Takeoff MaxTakeoff F_10 7478 ICAO_A 8 2 Climb MaxTakeoff F_10 1 500 7478 ICAO_A 8 3 Climb MaxClimb F_10 3 000 7478 ICAO_A 8 4 Accelerate_ MaxClimb F_5 230 55 Percent 7478 ICAO_A 8 5 Accelerate_ MaxClimb F_1 265 55 Percent 7478 ICAO_A 8 6 Accelerate_ MaxClimb F_0 280 50 Percent 7478 ICAO_A 8 7 Climb MaxClimb F_0 10 000 7478 ICAO_A 9 1 Takeoff MaxTakeoff F_10 7478 ICAO_A 9 2 Climb MaxTakeoff F_10 1 500 7478 ICAO_A 9 3 Climb MaxClimb F_10 3 000 7478 ICAO_A 9 4 Accelerate_ MaxClimb F_5 230 55 PercentL 168/348 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7478 ICAO_A 9 5 Accelerate_ MaxClimb F_1 265 55 Percent 7478 ICAO_A 9 6 Accelerate_ MaxClimb F_0 280 50 Percent 7478 ICAO_A 9 7 Climb MaxClimb F_0 10 000 7478 ICAO_B 1 1 Takeoff MaxTakeoff F_10 7478 ICAO_B 1 2 Climb MaxTakeoff F_10 1 000 7478 ICAO_B 1 3 Accelerate_ MaxTakeoff F_10 210 55 Percent 7478 ICAO_B 1 4 Accelerate_ MaxTakeoff F_5 250 55 Percent 7478 ICAO_B 1 5 Climb MaxTakeoff F_1 3 480 7478 ICAO_B 1 6 Accelerate_ MaxClimb F_0 280 50 Percent 7478 ICAO_B 1 7 Climb MaxClimb F_0 10 000 7478 ICAO_B 2 1 Takeoff MaxTakeoff F_10 7478 ICAO_B 2 2 Climb MaxTakeoff F_10 1 000 7478 ICAO_B 2 3 Accelerate_ MaxTakeoff F_10 223 55 Percent 7478 ICAO_B 2 4 Accelerate_ MaxTakeoff F_5 250 55 Percent 7478 ICAO_B 2 5 Climb MaxTakeoff F_1 3 350 7478 ICAO_B 2 6 Accelerate_ MaxClimb F_0 280 50 Percent 7478 ICAO_B 2 7 Climb MaxClimb F_0 10 000 7478 ICAO_B 3 1 Takeoff MaxTakeoff F_10 7478 ICAO_B 3 2 Climb MaxTakeoff F_10 1 000 7478 ICAO_B 3 3 Accelerate_ MaxTakeoff F_10 223 55 Percent1.7.2015 EN Official Journal of the European Union L 168/349 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7478 ICAO_B 3 4 Accelerate_ MaxTakeoff F_5 263 55 Percent 7478 ICAO_B 3 5 Climb MaxTakeoff F_1 3 350 7478 ICAO_B 3 6 Accelerate_ MaxClimb F_0 300 50 Percent 7478 ICAO_B 3 7 Climb MaxClimb F_0 10 000 7478 ICAO_B 4 1 Takeoff MaxTakeoff F_10 7478 ICAO_B 4 2 Climb MaxTakeoff F_10 1 000 7478 ICAO_B 4 3 Accelerate_ MaxTakeoff F_10 210 55 Percent 7478 ICAO_B 4 4 Accelerate_ MaxTakeoff F_5 260 55 Percent 7478 ICAO_B 4 5 Climb MaxTakeoff F_1 3 480 7478 ICAO_B 4 6 Accelerate_ MaxClimb F_0 270 50 Percent 7478 ICAO_B 4 7 Climb MaxClimb F_0 10 000 7478 ICAO_B 5 1 Takeoff MaxTakeoff F_10 7478 ICAO_B 5 2 Climb MaxTakeoff F_10 1 000 7478 ICAO_B 5 3 Accelerate_ MaxTakeoff F_10 228 55 Percent 7478 ICAO_B 5 4 Accelerate_ MaxTakeoff F_5 262 55 Percent 7478 ICAO_B 5 5 Climb MaxTakeoff F_1 2 760 7478 ICAO_B 5 6 Accelerate_ MaxClimb F_0 270 50 Percent 7478 ICAO_B 5 7 Climb MaxClimb F_0 10 000 7478 ICAO_B 6 1 Takeoff MaxTakeoff F_10 7478 ICAO_B 6 2 Climb MaxTakeoff F_10 1 000L 168/350 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7478 ICAO_B 6 3 Accelerate_ MaxTakeoff F_10 231 55 Percent 7478 ICAO_B 6 4 Accelerate_ MaxTakeoff F_5 264 55 Percent 7478 ICAO_B 6 5 Climb MaxTakeoff F_1 2 610 7478 ICAO_B 6 6 Accelerate_ MaxClimb F_0 300 50 Percent 7478 ICAO_B 6 7 Climb MaxClimb F_0 10 000 7478 ICAO_B 7 1 Takeoff MaxTakeoff F_10 7478 ICAO_B 7 2 Climb MaxTakeoff F_10 1 000 7478 ICAO_B 7 3 Accelerate_ MaxTakeoff F_10 231 55 Percent 7478 ICAO_B 7 4 Accelerate_ MaxTakeoff F_5 270 55 Percent 7478 ICAO_B 7 5 Climb MaxTakeoff F_1 2 610 7478 ICAO_B 7 6 Accelerate_ MaxClimb F_0 300 50 Percent 7478 ICAO_B 7 7 Climb MaxClimb F_0 10 000 7478 ICAO_B 8 1 Takeoff MaxTakeoff F_10 7478 ICAO_B 8 2 Climb MaxTakeoff F_10 1 000 7478 ICAO_B 8 3 Accelerate_ MaxTakeoff F_10 235 55 Percent 7478 ICAO_B 8 4 Accelerate_ MaxTakeoff F_5 265 55 Percent 7478 ICAO_B 8 5 Accelerate_ MaxTakeoff F_1 275 55 Percent 7478 ICAO_B 8 6 Climb MaxClimb F_0 10 000 7478 ICAO_B 9 1 Takeoff MaxTakeoff F_10 7478 ICAO_B 9 2 Climb MaxTakeoff F_10 1 0001.7.2015 EN Official Journal of the European Union L 168/351 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7478 ICAO_B 9 3 Accelerate_ MaxTakeoff F_10 240 55 Percent 7478 ICAO_B 9 4 Accelerate_ MaxTakeoff F_5 270 55 Percent 7478 ICAO_B 9 5 Accelerate_ MaxTakeoff F_1 280 55 Percent 7478 ICAO_B 9 6 Climb MaxClimb F_0 10 000 747SP DEFAULT 1 1 Takeoff MaxTakeoff 10 747SP DEFAULT 1 2 Climb MaxTakeoff 10 1 000 747SP DEFAULT 1 3 Accelerate MaxTakeoff 10 2 469 163 747SP DEFAULT 1 4 Accelerate MaxClimb 5 1 000 203 747SP DEFAULT 1 5 Climb MaxClimb ZERO 3 000 747SP DEFAULT 1 6 Accelerate MaxClimb ZERO 1 000 250 747SP DEFAULT 1 7 Climb MaxClimb ZERO 5 500 747SP DEFAULT 1 8 Climb MaxClimb ZERO 7 500 747SP DEFAULT 1 9 Climb MaxClimb ZERO 10 000 747SP DEFAULT 2 1 Takeoff MaxTakeoff 10 747SP DEFAULT 2 2 Climb MaxTakeoff 10 1 000 747SP DEFAULT 2 3 Accelerate MaxTakeoff 10 2 326 167 747SP DEFAULT 2 4 Accelerate MaxClimb 5 1 000 207 747SP DEFAULT 2 5 Climb MaxClimb ZERO 3 000 747SP DEFAULT 2 6 Accelerate MaxClimb ZERO 1 000 250 747SP DEFAULT 2 7 Climb MaxClimb ZERO 5 500L 168/352 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747SP DEFAULT 2 8 Climb MaxClimb ZERO 7 500 747SP DEFAULT 2 9 Climb MaxClimb ZERO 10 000 747SP DEFAULT 3 1 Takeoff MaxTakeoff 10 747SP DEFAULT 3 2 Climb MaxTakeoff 10 1 000 747SP DEFAULT 3 3 Accelerate MaxTakeoff 10 2 201 170 747SP DEFAULT 3 4 Accelerate MaxClimb 5 1 000 210 747SP DEFAULT 3 5 Climb MaxClimb ZERO 3 000 747SP DEFAULT 3 6 Accelerate MaxClimb ZERO 1 000 250 747SP DEFAULT 3 7 Climb MaxClimb ZERO 5 500 747SP DEFAULT 3 8 Climb MaxClimb ZERO 7 500 747SP DEFAULT 3 9 Climb MaxClimb ZERO 10 000 747SP DEFAULT 4 1 Takeoff MaxTakeoff 10 747SP DEFAULT 4 2 Climb MaxTakeoff 10 1 000 747SP DEFAULT 4 3 Accelerate MaxTakeoff 10 2 027 175 747SP DEFAULT 4 4 Accelerate MaxClimb 5 1 000 215 747SP DEFAULT 4 5 Climb MaxClimb ZERO 3 000 747SP DEFAULT 4 6 Accelerate MaxClimb ZERO 1 000 250 747SP DEFAULT 4 7 Climb MaxClimb ZERO 5 500 747SP DEFAULT 4 8 Climb MaxClimb ZERO 7 500 747SP DEFAULT 4 9 Climb MaxClimb ZERO 10 0001.7.2015 EN Official Journal of the European Union L 168/353 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747SP DEFAULT 5 1 Takeoff MaxTakeoff 10 747SP DEFAULT 5 2 Climb MaxTakeoff 10 1 000 747SP DEFAULT 5 3 Accelerate MaxTakeoff 10 1 821 182 747SP DEFAULT 5 4 Accelerate MaxClimb 5 1 000 222 747SP DEFAULT 5 5 Climb MaxClimb ZERO 3 000 747SP DEFAULT 5 6 Accelerate MaxClimb ZERO 1 000 250 747SP DEFAULT 5 7 Climb MaxClimb ZERO 5 500 747SP DEFAULT 5 8 Climb MaxClimb ZERO 7 500 747SP DEFAULT 5 9 Climb MaxClimb ZERO 10 000 747SP DEFAULT 6 1 Takeoff MaxTakeoff 10 747SP DEFAULT 6 2 Climb MaxTakeoff 10 1 000 747SP DEFAULT 6 3 Accelerate MaxTakeoff 10 1 643 188 747SP DEFAULT 6 4 Accelerate MaxClimb 5 1 000 228 747SP DEFAULT 6 5 Climb MaxClimb ZERO 3 000 747SP DEFAULT 6 6 Accelerate MaxClimb ZERO 1 000 250 747SP DEFAULT 6 7 Climb MaxClimb ZERO 5 500 747SP DEFAULT 6 8 Climb MaxClimb ZERO 7 500 747SP DEFAULT 6 9 Climb MaxClimb ZERO 10 000L 168/354 EN Official Journal of the European Union 1.7.2015 Table I-4 (part 2) Default departures procedural steps Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 747SP DEFAULT 7 1 Takeoff MaxTakeoff 10 747SP DEFAULT 7 2 Climb MaxTakeoff 10 1 000 747SP DEFAULT 7 3 Accelerate MaxTakeoff 10 1 403 196 747SP DEFAULT 7 4 Accelerate MaxClimb 5 1 000 236 747SP DEFAULT 7 5 Accelerate MaxClimb ZERO 1 000 250 747SP DEFAULT 7 6 Climb MaxClimb ZERO 5 500 747SP DEFAULT 7 7 Climb MaxClimb ZERO 7 500 747SP DEFAULT 7 8 Climb MaxClimb ZERO 10 000 757300 DEFAULT 1 1 Takeoff MaxTakeoff T_05 757300 DEFAULT 1 2 Climb MaxTakeoff T_05 1 097 757300 DEFAULT 1 3 Accelerate MaxTakeoff T_05 2 252,1 211,8 757300 DEFAULT 1 4 Accelerate MaxTakeoff T_01 2 480 215,4 757300 DEFAULT 1 5 Climb MaxTakeoff T_00 2 569 757300 DEFAULT 1 6 Climb MaxClimb T_00 3 000 757300 DEFAULT 1 7 Accelerate MaxClimb T_00 1 701,7 250 757300 DEFAULT 1 8 Climb MaxClimb T_00 5 500 757300 DEFAULT 1 9 Climb MaxClimb T_00 7 500 757300 DEFAULT 1 10 Climb MaxClimb T_00 10 0001.7.2015 EN Official Journal of the European Union L 168/355 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757300 DEFAULT 2 1 Takeoff MaxTakeoff T_05 757300 DEFAULT 2 2 Climb MaxTakeoff T_05 1 041 757300 DEFAULT 2 3 Accelerate MaxTakeoff T_05 2 154,9 213 757300 DEFAULT 2 4 Accelerate MaxTakeoff T_01 2 352 218,6 757300 DEFAULT 2 5 Climb MaxTakeoff T_00 2 412 757300 DEFAULT 2 6 Climb MaxClimb T_00 3 000 757300 DEFAULT 2 7 Accelerate MaxClimb T_00 1 607,8 250 757300 DEFAULT 2 8 Climb MaxClimb T_00 5 500 757300 DEFAULT 2 9 Climb MaxClimb T_00 7 500 757300 DEFAULT 2 10 Climb MaxClimb T_00 10 000 757300 DEFAULT 3 1 Takeoff MaxTakeoff T_05 757300 DEFAULT 3 2 Climb MaxTakeoff T_05 1 000 757300 DEFAULT 3 3 Accelerate MaxTakeoff T_05 2 062 214,5 757300 DEFAULT 3 4 Accelerate MaxTakeoff T_01 2 223,5 221,8 757300 DEFAULT 3 5 Climb MaxTakeoff T_00 2 275 757300 DEFAULT 3 6 Climb MaxClimb T_00 3 000 757300 DEFAULT 3 7 Accelerate MaxClimb T_00 1 521,8 250 757300 DEFAULT 3 8 Climb MaxClimb T_00 5 500 757300 DEFAULT 3 9 Climb MaxClimb T_00 7 500L 168/356 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757300 DEFAULT 3 10 Climb MaxClimb T_00 10 000 757300 DEFAULT 4 1 Takeoff MaxTakeoff T_05 757300 DEFAULT 4 2 Climb MaxTakeoff T_05 1 000 757300 DEFAULT 4 3 Accelerate MaxTakeoff T_05 1 901,4 217,4 757300 DEFAULT 4 4 Accelerate MaxTakeoff T_01 2 061,8 228 757300 DEFAULT 4 5 Climb MaxTakeoff T_00 2 099 757300 DEFAULT 4 6 Climb MaxClimb T_00 3 000 757300 DEFAULT 4 7 Accelerate MaxClimb T_00 1 374,1 250 757300 DEFAULT 4 8 Climb MaxClimb T_00 5 500 757300 DEFAULT 4 9 Climb MaxClimb T_00 7 500 757300 DEFAULT 4 10 Climb MaxClimb T_00 10 000 757300 DEFAULT 5 1 Takeoff MaxTakeoff T_05 757300 DEFAULT 5 2 Climb MaxTakeoff T_05 1 000 757300 DEFAULT 5 3 Accelerate MaxTakeoff T_05 1 729,2 221,7 757300 DEFAULT 5 4 Accelerate MaxTakeoff T_01 1 881,8 236,7 757300 DEFAULT 5 5 Climb MaxTakeoff T_00 1 891 757300 DEFAULT 5 6 Climb MaxClimb T_00 3 000 757300 DEFAULT 5 7 Accelerate MaxClimb T_00 1 227,3 250 757300 DEFAULT 5 8 Climb MaxClimb T_00 5 500 757300 DEFAULT 5 9 Climb MaxClimb T_00 7 5001.7.2015 EN Official Journal of the European Union L 168/357 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757300 DEFAULT 5 10 Climb MaxClimb T_00 10 000 757300 DEFAULT 6 1 Takeoff MaxTakeoff T_05 757300 DEFAULT 6 2 Climb MaxTakeoff T_05 1 000 757300 DEFAULT 6 3 Accelerate MaxTakeoff T_05 1 655 224 757300 DEFAULT 6 4 Accelerate MaxTakeoff T_01 1 836,4 240,1 757300 DEFAULT 6 5 Climb MaxTakeoff T_00 1 829 757300 DEFAULT 6 6 Climb MaxClimb T_00 3 000 757300 DEFAULT 6 7 Accelerate MaxClimb T_00 1 159,2 250 757300 DEFAULT 6 8 Climb MaxClimb T_00 5 500 757300 DEFAULT 6 9 Climb MaxClimb T_00 7 500 757300 DEFAULT 6 10 Climb MaxClimb T_00 10 000 757300 ICAO_A 1 1 Takeoff MaxTakeoff T_05 757300 ICAO_A 1 2 Climb MaxTakeoff T_05 1 500 757300 ICAO_A 1 3 Climb MaxClimb T_05 3 000 757300 ICAO_A 1 4 Accelerate MaxClimb T_05 1 388,6 198 757300 ICAO_A 1 5 Accelerate MaxClimb T_01 1 528,2 215 757300 ICAO_A 1 6 Accelerate MaxClimb T_00 1 693,5 250 757300 ICAO_A 1 7 Climb MaxClimb T_00 5 500 757300 ICAO_A 1 8 Climb MaxClimb T_00 7 500 757300 ICAO_A 1 9 Climb MaxClimb T_00 10 000L 168/358 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757300 ICAO_A 2 1 Takeoff MaxTakeoff T_05 757300 ICAO_A 2 2 Climb MaxTakeoff T_05 1 500 757300 ICAO_A 2 3 Climb MaxClimb T_05 3 000 757300 ICAO_A 2 4 Accelerate MaxClimb T_05 1 304,9 199,6 757300 ICAO_A 2 5 Accelerate MaxClimb T_01 1 441 215,6 757300 ICAO_A 2 6 Accelerate MaxClimb T_00 1 597,7 250 757300 ICAO_A 2 7 Climb MaxClimb T_00 5 500 757300 ICAO_A 2 8 Climb MaxClimb T_00 7 500 757300 ICAO_A 2 9 Climb MaxClimb T_00 10 000 757300 ICAO_A 3 1 Takeoff MaxTakeoff T_05 757300 ICAO_A 3 2 Climb MaxTakeoff T_05 1 500 757300 ICAO_A 3 3 Climb MaxClimb T_05 3 000 757300 ICAO_A 3 4 Accelerate MaxClimb T_05 1 242,3 201,6 757300 ICAO_A 3 5 Accelerate MaxClimb T_01 1 357,6 216,7 757300 ICAO_A 3 6 Accelerate MaxClimb T_00 1 500 250 757300 ICAO_A 3 7 Climb MaxClimb T_00 5 500 757300 ICAO_A 3 8 Climb MaxClimb T_00 7 500 757300 ICAO_A 3 9 Climb MaxClimb T_00 10 000 757300 ICAO_A 4 1 Takeoff MaxTakeoff T_05 757300 ICAO_A 4 2 Climb MaxTakeoff T_05 1 5001.7.2015 EN Official Journal of the European Union L 168/359 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757300 ICAO_A 4 3 Climb MaxClimb T_05 3 000 757300 ICAO_A 4 4 Accelerate MaxClimb T_05 1 127,1 205,3 757300 ICAO_A 4 5 Accelerate MaxClimb T_01 1 221,4 221,1 757300 ICAO_A 4 6 Accelerate MaxClimb T_00 1 359,4 250 757300 ICAO_A 4 7 Climb MaxClimb T_00 5 500 757300 ICAO_A 4 8 Climb MaxClimb T_00 7 500 757300 ICAO_A 4 9 Climb MaxClimb T_00 10 000 757300 ICAO_A 5 1 Takeoff MaxTakeoff T_05 757300 ICAO_A 5 2 Climb MaxTakeoff T_05 1 500 757300 ICAO_A 5 3 Climb MaxClimb T_05 3 000 757300 ICAO_A 5 4 Accelerate MaxClimb T_05 997,2 210,6 757300 ICAO_A 5 5 Accelerate MaxClimb T_01 1 076 227,9 757300 ICAO_A 5 6 Accelerate MaxClimb T_00 1 192 250 757300 ICAO_A 5 7 Climb MaxClimb T_00 5 500 757300 ICAO_A 5 8 Climb MaxClimb T_00 7 500 757300 ICAO_A 5 9 Climb MaxClimb T_00 10 000 757300 ICAO_A 6 1 Takeoff MaxTakeoff T_05 757300 ICAO_A 6 2 Climb MaxTakeoff T_05 1 500 757300 ICAO_A 6 3 Climb MaxClimb T_05 3 000 757300 ICAO_A 6 4 Accelerate MaxClimb T_05 945,1 213,2L 168/360 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757300 ICAO_A 6 5 Accelerate MaxClimb T_01 1 031,2 230,6 757300 ICAO_A 6 6 Accelerate MaxClimb T_00 1 127,9 250 757300 ICAO_A 6 7 Climb MaxClimb T_00 5 500 757300 ICAO_A 6 8 Climb MaxClimb T_00 7 500 757300 ICAO_A 6 9 Climb MaxClimb T_00 10 000 757300 ICAO_B 1 1 Takeoff MaxTakeoff T_05 757300 ICAO_B 1 2 Climb MaxTakeoff T_05 1 097 757300 ICAO_B 1 3 Accelerate MaxTakeoff T_05 2 252,1 211,8 757300 ICAO_B 1 4 Accelerate MaxTakeoff T_01 2 480 215,4 757300 ICAO_B 1 5 Climb MaxTakeoff T_00 2 569 757300 ICAO_B 1 6 Climb MaxClimb T_00 3 000 757300 ICAO_B 1 7 Accelerate MaxClimb T_00 1 701,7 250 757300 ICAO_B 1 8 Climb MaxClimb T_00 5 500 757300 ICAO_B 1 9 Climb MaxClimb T_00 7 500 757300 ICAO_B 1 10 Climb MaxClimb T_00 10 000 757300 ICAO_B 2 1 Takeoff MaxTakeoff T_05 757300 ICAO_B 2 2 Climb MaxTakeoff T_05 1 041 757300 ICAO_B 2 3 Accelerate MaxTakeoff T_05 2 154,9 213 757300 ICAO_B 2 4 Accelerate MaxTakeoff T_01 2 352 218,6 757300 ICAO_B 2 5 Climb MaxTakeoff T_00 2 4121.7.2015 EN Official Journal of the European Union L 168/361 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757300 ICAO_B 2 6 Climb MaxClimb T_00 3 000 757300 ICAO_B 2 7 Accelerate MaxClimb T_00 1 607,8 250 757300 ICAO_B 2 8 Climb MaxClimb T_00 5 500 757300 ICAO_B 2 9 Climb MaxClimb T_00 7 500 757300 ICAO_B 2 10 Climb MaxClimb T_00 10 000 757300 ICAO_B 3 1 Takeoff MaxTakeoff T_05 757300 ICAO_B 3 2 Climb MaxTakeoff T_05 1 000 757300 ICAO_B 3 3 Accelerate MaxTakeoff T_05 2 062 214,5 757300 ICAO_B 3 4 Accelerate MaxTakeoff T_01 2 223,5 221,8 757300 ICAO_B 3 5 Climb MaxTakeoff T_00 2 275 757300 ICAO_B 3 6 Climb MaxClimb T_00 3 000 757300 ICAO_B 3 7 Accelerate MaxClimb T_00 1 521,8 250 757300 ICAO_B 3 8 Climb MaxClimb T_00 5 500 757300 ICAO_B 3 9 Climb MaxClimb T_00 7 500 757300 ICAO_B 3 10 Climb MaxClimb T_00 10 000 757300 ICAO_B 4 1 Takeoff MaxTakeoff T_05 757300 ICAO_B 4 2 Climb MaxTakeoff T_05 1 000 757300 ICAO_B 4 3 Accelerate MaxTakeoff T_05 1 901,4 217,4 757300 ICAO_B 4 4 Accelerate MaxTakeoff T_01 2 061,8 228 757300 ICAO_B 4 5 Climb MaxTakeoff T_00 2 099L 168/362 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757300 ICAO_B 4 6 Climb MaxClimb T_00 3 000 757300 ICAO_B 4 7 Accelerate MaxClimb T_00 1 374,1 250 757300 ICAO_B 4 8 Climb MaxClimb T_00 5 500 757300 ICAO_B 4 9 Climb MaxClimb T_00 7 500 757300 ICAO_B 4 10 Climb MaxClimb T_00 10 000 757300 ICAO_B 5 1 Takeoff MaxTakeoff T_05 757300 ICAO_B 5 2 Climb MaxTakeoff T_05 1 000 757300 ICAO_B 5 3 Accelerate MaxTakeoff T_05 1 729,2 221,7 757300 ICAO_B 5 4 Accelerate MaxTakeoff T_01 1 881,8 236,7 757300 ICAO_B 5 5 Climb MaxTakeoff T_00 1 891 757300 ICAO_B 5 6 Climb MaxClimb T_00 3 000 757300 ICAO_B 5 7 Accelerate MaxClimb T_00 1 227,3 250 757300 ICAO_B 5 8 Climb MaxClimb T_00 5 500 757300 ICAO_B 5 9 Climb MaxClimb T_00 7 500 757300 ICAO_B 5 10 Climb MaxClimb T_00 10 000 757300 ICAO_B 6 1 Takeoff MaxTakeoff T_05 757300 ICAO_B 6 2 Climb MaxTakeoff T_05 1 000 757300 ICAO_B 6 3 Accelerate MaxTakeoff T_05 1 655 224 757300 ICAO_B 6 4 Accelerate MaxTakeoff T_01 1 836,4 240,1 757300 ICAO_B 6 5 Climb MaxTakeoff T_00 1 8291.7.2015 EN Official Journal of the European Union L 168/363 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757300 ICAO_B 6 6 Climb MaxClimb T_00 3 000 757300 ICAO_B 6 7 Accelerate MaxClimb T_00 1 159,2 250 757300 ICAO_B 6 8 Climb MaxClimb T_00 5 500 757300 ICAO_B 6 9 Climb MaxClimb T_00 7 500 757300 ICAO_B 6 10 Climb MaxClimb T_00 10 000 757PW DEFAULT 1 1 Takeoff MaxTakeoff 5 757PW DEFAULT 1 2 Climb MaxTakeoff 5 1 000 757PW DEFAULT 1 3 Accelerate MaxClimb T_05 1 471 190,1 757PW DEFAULT 1 4 Accelerate MaxClimb T_01 1 636,4 206 757PW DEFAULT 1 5 Climb MaxClimb T_00 3 000 757PW DEFAULT 1 6 Accelerate MaxClimb T_00 1 822,2 250 757PW DEFAULT 1 7 Climb MaxClimb ZERO 5 500 757PW DEFAULT 1 8 Climb MaxClimb ZERO 7 500 757PW DEFAULT 1 9 Climb MaxClimb ZERO 10 000 757PW DEFAULT 2 1 Takeoff MaxTakeoff 5 757PW DEFAULT 2 2 Climb MaxTakeoff 5 1 000 757PW DEFAULT 2 3 Accelerate MaxClimb T_05 1 403,6 191,4 757PW DEFAULT 2 4 Accelerate MaxClimb T_01 1 568,2 208,7 757PW DEFAULT 2 5 Climb MaxClimb T_00 3 000 757PW DEFAULT 2 6 Accelerate MaxClimb T_00 1 742,7 250L 168/364 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757PW DEFAULT 2 7 Climb MaxClimb ZERO 5 500 757PW DEFAULT 2 8 Climb MaxClimb ZERO 7 500 757PW DEFAULT 2 9 Climb MaxClimb ZERO 10 000 757PW DEFAULT 3 1 Takeoff MaxTakeoff 5 757PW DEFAULT 3 2 Climb MaxTakeoff 5 1 000 757PW DEFAULT 3 3 Accelerate MaxClimb T_05 1 339,2 193 757PW DEFAULT 3 4 Accelerate MaxClimb T_01 1 495,9 211,1 757PW DEFAULT 3 5 Accelerate MaxClimb T_00 1 666,7 211,6 757PW DEFAULT 3 6 Climb MaxClimb T_00 3 000 757PW DEFAULT 3 7 Accelerate MaxClimb T_00 1 661 250 757PW DEFAULT 3 8 Climb MaxClimb ZERO 5 500 757PW DEFAULT 3 9 Climb MaxClimb ZERO 7 500 757PW DEFAULT 3 10 Climb MaxClimb ZERO 10 000 757PW DEFAULT 4 1 Takeoff MaxTakeoff 5 757PW DEFAULT 4 2 Climb MaxTakeoff 5 1 000 757PW DEFAULT 4 3 Accelerate MaxClimb T_05 1 213,5 196,4 757PW DEFAULT 4 4 Accelerate MaxClimb T_01 1 353,6 213,7 757PW DEFAULT 4 5 Accelerate MaxClimb T_00 1 460,3 217,4 757PW DEFAULT 4 6 Climb MaxClimb T_00 3 000 757PW DEFAULT 4 7 Accelerate MaxClimb T_00 1 510,6 2501.7.2015 EN Official Journal of the European Union L 168/365 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757PW DEFAULT 4 8 Climb MaxClimb ZERO 5 500 757PW DEFAULT 4 9 Climb MaxClimb ZERO 7 500 757PW DEFAULT 4 10 Climb MaxClimb ZERO 10 000 757PW DEFAULT 5 1 Takeoff MaxTakeoff 5 757PW DEFAULT 5 2 Climb MaxTakeoff 5 1 000 757PW DEFAULT 5 3 Accelerate MaxClimb T_05 1 082,9 200,8 757PW DEFAULT 5 4 Accelerate MaxClimb T_01 1 212 218,5 757PW DEFAULT 5 5 Accelerate MaxClimb T_00 1 291,1 224,3 757PW DEFAULT 5 6 Climb MaxClimb T_00 3 000 757PW DEFAULT 5 7 Accelerate MaxClimb T_00 1 352,4 250 757PW DEFAULT 5 8 Climb MaxClimb ZERO 5 500 757PW DEFAULT 5 9 Climb MaxClimb ZERO 7 500 757PW DEFAULT 5 10 Climb MaxClimb ZERO 10 000 757PW DEFAULT 6 1 Takeoff MaxTakeoff 5 757PW DEFAULT 6 2 Climb MaxTakeoff 5 1 000 757PW DEFAULT 6 3 Accelerate MaxClimb T_05 1 005,7 203,9 757PW DEFAULT 6 4 Accelerate MaxClimb T_01 1 124,3 221,9 757PW DEFAULT 6 5 Accelerate MaxClimb T_00 1 220 228,7 757PW DEFAULT 6 6 Climb MaxClimb T_00 3 000 757PW DEFAULT 6 7 Accelerate MaxClimb T_00 1 259,5 250L 168/366 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757PW DEFAULT 6 8 Climb MaxClimb ZERO 5 500 757PW DEFAULT 6 9 Climb MaxClimb ZERO 7 500 757PW DEFAULT 6 10 Climb MaxClimb ZERO 10 000 757PW DEFAULT 7 1 Takeoff MaxTakeoff 5 757PW DEFAULT 7 2 Climb MaxTakeoff 5 1 000 757PW DEFAULT 7 3 Accelerate MaxClimb T_05 938,1 207 757PW DEFAULT 7 4 Accelerate MaxClimb T_01 1 052,4 225,2 757PW DEFAULT 7 5 Accelerate MaxClimb T_00 1 134,5 233,3 757PW DEFAULT 7 6 Climb MaxClimb T_00 3 000 757PW DEFAULT 7 7 Accelerate MaxClimb T_00 1 172,9 250 757PW DEFAULT 7 8 Climb MaxClimb ZERO 5 500 757PW DEFAULT 7 9 Climb MaxClimb ZERO 7 500 757PW DEFAULT 7 10 Climb MaxClimb ZERO 10 000 757PW ICAO_A 1 1 Takeoff MaxTakeoff 5 757PW ICAO_A 1 2 Climb MaxTakeoff 5 1 500 757PW ICAO_A 1 3 Climb MaxClimb T_05 3 000 757PW ICAO_A 1 4 Accelerate MaxClimb T_05 1 399,5 188 757PW ICAO_A 1 5 Accelerate MaxClimb T_01 1 605,4 205,8 757PW ICAO_A 1 6 Accelerate MaxClimb ZERO 1 804,8 250 757PW ICAO_A 1 7 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/367 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757PW ICAO_A 1 8 Climb MaxClimb ZERO 7 500 757PW ICAO_A 1 9 Climb MaxClimb ZERO 10 000 757PW ICAO_A 2 1 Takeoff MaxTakeoff 5 757PW ICAO_A 2 2 Climb MaxTakeoff 5 1 500 757PW ICAO_A 2 3 Climb MaxClimb T_05 3 000 757PW ICAO_A 2 4 Accelerate MaxClimb T_05 1 337,7 189,5 757PW ICAO_A 2 5 Accelerate MaxClimb T_01 1 522,3 207,2 757PW ICAO_A 2 6 Accelerate MaxClimb ZERO 1 725,5 250 757PW ICAO_A 2 7 Climb MaxClimb ZERO 5 500 757PW ICAO_A 2 8 Climb MaxClimb ZERO 7 500 757PW ICAO_A 2 9 Climb MaxClimb ZERO 10 000 757PW ICAO_A 3 1 Takeoff MaxTakeoff 5 757PW ICAO_A 3 2 Climb MaxTakeoff 5 1 500 757PW ICAO_A 3 3 Climb MaxClimb 5 3 000 757PW ICAO_A 3 4 Accelerate MaxClimb T_05 1 271,9 191,1 757PW ICAO_A 3 5 Accelerate MaxClimb T_01 1 451,8 208,2 757PW ICAO_A 3 6 Accelerate MaxClimb ZERO 1 638 250 757PW ICAO_A 3 7 Climb MaxClimb ZERO 5 500 757PW ICAO_A 3 8 Climb MaxClimb ZERO 7 500 757PW ICAO_A 3 9 Climb MaxClimb ZERO 10 000L 168/368 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757PW ICAO_A 4 1 Takeoff MaxTakeoff 5 757PW ICAO_A 4 2 Climb MaxTakeoff 5 1 500 757PW ICAO_A 4 3 Climb MaxClimb 5 3 000 757PW ICAO_A 4 4 Accelerate MaxClimb T_05 1 153,8 194,7 757PW ICAO_A 4 5 Accelerate MaxClimb T_01 1 312,6 212,2 757PW ICAO_A 4 6 Accelerate MaxClimb ZERO 1 486 250 757PW ICAO_A 4 7 Climb MaxClimb ZERO 5 500 757PW ICAO_A 4 8 Climb MaxClimb ZERO 7 500 757PW ICAO_A 4 9 Climb MaxClimb ZERO 10 000 757PW ICAO_A 5 1 Takeoff MaxTakeoff 5 757PW ICAO_A 5 2 Climb MaxTakeoff 5 1 500 757PW ICAO_A 5 3 Climb MaxClimb 5 3 000 757PW ICAO_A 5 4 Accelerate MaxClimb T_05 1 028,8 199,2 757PW ICAO_A 5 5 Accelerate MaxClimb T_01 1 171,1 217,2 757PW ICAO_A 5 6 Accelerate MaxClimb ZERO 1 325,6 250 757PW ICAO_A 5 7 Climb MaxClimb ZERO 5 500 757PW ICAO_A 5 8 Climb MaxClimb ZERO 7 500 757PW ICAO_A 5 9 Climb MaxClimb ZERO 10 000 757PW ICAO_A 6 1 Takeoff MaxTakeoff 5 757PW ICAO_A 6 2 Climb MaxTakeoff 5 1 5001.7.2015 EN Official Journal of the European Union L 168/369 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757PW ICAO_A 6 3 Climb MaxClimb 5 3 000 757PW ICAO_A 6 4 Accelerate MaxClimb T_05 953,4 202,5 757PW ICAO_A 6 5 Accelerate MaxClimb T_01 1 087,8 220,6 757PW ICAO_A 6 6 Accelerate MaxClimb ZERO 1 225,5 250 757PW ICAO_A 6 7 Climb MaxClimb ZERO 5 500 757PW ICAO_A 6 8 Climb MaxClimb ZERO 7 500 757PW ICAO_A 6 9 Climb MaxClimb ZERO 10 000 757PW ICAO_A 7 1 Takeoff MaxTakeoff 5 757PW ICAO_A 7 2 Climb MaxTakeoff 5 1 500 757PW ICAO_A 7 3 Climb MaxClimb 5 3 000 757PW ICAO_A 7 4 Accelerate MaxClimb T_05 886,5 205,7 757PW ICAO_A 7 5 Accelerate MaxClimb T_01 1 012,8 224 757PW ICAO_A 7 6 Accelerate MaxClimb ZERO 1 140,1 250 757PW ICAO_A 7 7 Climb MaxClimb ZERO 5 500 757PW ICAO_A 7 8 Climb MaxClimb ZERO 7 500 757PW ICAO_A 7 9 Climb MaxClimb ZERO 10 000 757PW ICAO_B 1 1 Takeoff MaxTakeoff 5 757PW ICAO_B 1 2 Climb MaxTakeoff 5 1 000 757PW ICAO_B 1 3 Accelerate MaxTakeoff 5 1 970,1 206 757PW ICAO_B 1 4 Climb MaxClimb ZERO 3 000L 168/370 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757PW ICAO_B 1 5 Accelerate MaxClimb ZERO 1 821,5 250 757PW ICAO_B 1 6 Climb MaxClimb ZERO 5 500 757PW ICAO_B 1 7 Climb MaxClimb ZERO 7 500 757PW ICAO_B 1 8 Climb MaxClimb ZERO 10 000 757PW ICAO_B 2 1 Takeoff MaxTakeoff 5 757PW ICAO_B 2 2 Climb MaxTakeoff 5 1 000 757PW ICAO_B 2 3 Accelerate MaxTakeoff 5 1 899,2 208,7 757PW ICAO_B 2 4 Climb MaxClimb ZERO 3 000 757PW ICAO_B 2 5 Accelerate MaxClimb ZERO 1 743,3 250 757PW ICAO_B 2 6 Climb MaxClimb ZERO 5 500 757PW ICAO_B 2 7 Climb MaxClimb ZERO 7 500 757PW ICAO_B 2 8 Climb MaxClimb ZERO 10 000 757PW ICAO_B 3 1 Takeoff MaxTakeoff 5 757PW ICAO_B 3 2 Climb MaxTakeoff 5 1 000 757PW ICAO_B 3 3 Accelerate MaxTakeoff 5 1 825,8 211,6 757PW ICAO_B 3 4 Climb MaxClimb ZERO 3 000 757PW ICAO_B 3 5 Accelerate MaxClimb ZERO 1 659,4 250 757PW ICAO_B 3 6 Climb MaxClimb ZERO 5 500 757PW ICAO_B 3 7 Climb MaxClimb ZERO 7 500 757PW ICAO_B 3 8 Climb MaxClimb ZERO 10 0001.7.2015 EN Official Journal of the European Union L 168/371 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757PW ICAO_B 4 1 Takeoff MaxTakeoff 5 757PW ICAO_B 4 2 Climb MaxTakeoff 5 1 000 757PW ICAO_B 4 3 Accelerate MaxTakeoff 5 1 690,7 217,4 757PW ICAO_B 4 4 Climb MaxClimb ZERO 3 000 757PW ICAO_B 4 5 Accelerate MaxClimb ZERO 1 512,3 250 757PW ICAO_B 4 6 Climb MaxClimb ZERO 5 500 757PW ICAO_B 4 7 Climb MaxClimb ZERO 7 500 757PW ICAO_B 4 8 Climb MaxClimb ZERO 10 000 757PW ICAO_B 5 1 Takeoff MaxTakeoff 5 757PW ICAO_B 5 2 Climb MaxTakeoff 5 1 000 757PW ICAO_B 5 3 Accelerate MaxTakeoff 5 1 543,6 224,1 757PW ICAO_B 5 4 Climb MaxClimb ZERO 3 000 757PW ICAO_B 5 5 Accelerate MaxClimb ZERO 1 351,8 250 757PW ICAO_B 5 6 Climb MaxClimb ZERO 5 500 757PW ICAO_B 5 7 Climb MaxClimb ZERO 7 500 757PW ICAO_B 5 8 Climb MaxClimb ZERO 10 000 757PW ICAO_B 6 1 Takeoff MaxTakeoff 5 757PW ICAO_B 6 2 Climb MaxTakeoff 5 1 000 757PW ICAO_B 6 3 Accelerate MaxTakeoff 5 1 458,3 228,7 757PW ICAO_B 6 4 Climb MaxClimb ZERO 3 000L 168/372 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757PW ICAO_B 6 5 Accelerate MaxClimb ZERO 1 257,5 250 757PW ICAO_B 6 6 Climb MaxClimb ZERO 5 500 757PW ICAO_B 6 7 Climb MaxClimb ZERO 7 500 757PW ICAO_B 6 8 Climb MaxClimb ZERO 10 000 757PW ICAO_B 7 1 Takeoff MaxTakeoff 5 757PW ICAO_B 7 2 Climb MaxTakeoff 5 1 000 757PW ICAO_B 7 3 Accelerate MaxTakeoff 5 1 380,6 233,3 757PW ICAO_B 7 4 Climb MaxClimb ZERO 3 000 757PW ICAO_B 7 5 Accelerate MaxClimb ZERO 1 173,6 250 757PW ICAO_B 7 6 Climb MaxClimb ZERO 5 500 757PW ICAO_B 7 7 Climb MaxClimb ZERO 7 500 757PW ICAO_B 7 8 Climb MaxClimb ZERO 10 000 757RR DEFAULT 1 1 Takeoff MaxTakeoff 5 757RR DEFAULT 1 2 Climb MaxTakeoff 5 1 000 757RR DEFAULT 1 3 Accelerate MaxClimb T_05 1 613,9 192,4 757RR DEFAULT 1 4 Accelerate MaxClimb T_01 1 779,7 206,3 757RR DEFAULT 1 5 Climb MaxClimb ZERO 3 000 757RR DEFAULT 1 6 Accelerate MaxClimb ZERO 1 966,1 250 757RR DEFAULT 1 7 Climb MaxClimb ZERO 5 500 757RR DEFAULT 1 8 Climb MaxClimb ZERO 7 5001.7.2015 EN Official Journal of the European Union L 168/373 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757RR DEFAULT 1 9 Climb MaxClimb ZERO 10 000 757RR DEFAULT 2 1 Takeoff MaxTakeoff 5 757RR DEFAULT 2 2 Climb MaxTakeoff 5 1 000 757RR DEFAULT 2 3 Accelerate MaxClimb T_05 1 544,6 193,9 757RR DEFAULT 2 4 Accelerate MaxClimb T_01 1 703,3 209,2 757RR DEFAULT 2 5 Climb MaxClimb ZERO 3 000 757RR DEFAULT 2 6 Accelerate MaxClimb ZERO 1 879,3 250 757RR DEFAULT 2 7 Climb MaxClimb ZERO 5 500 757RR DEFAULT 2 8 Climb MaxClimb ZERO 7 500 757RR DEFAULT 2 9 Climb MaxClimb ZERO 10 000 757RR DEFAULT 3 1 Takeoff MaxTakeoff 5 757RR DEFAULT 3 2 Climb MaxTakeoff 5 1 000 757RR DEFAULT 3 3 Accelerate MaxClimb T_05 1 474,6 195,5 757RR DEFAULT 3 4 Accelerate MaxClimb T_01 1 627,6 212,2 757RR DEFAULT 3 5 Climb MaxClimb ZERO 3 000 757RR DEFAULT 3 6 Accelerate MaxClimb ZERO 1 787,2 250 757RR DEFAULT 3 7 Climb MaxClimb ZERO 5 500 757RR DEFAULT 3 8 Climb MaxClimb ZERO 7 500 757RR DEFAULT 3 9 Climb MaxClimb ZERO 10 000 757RR DEFAULT 4 1 Takeoff MaxTakeoff 5L 168/374 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757RR DEFAULT 4 2 Climb MaxTakeoff 5 1 000 757RR DEFAULT 4 3 Accelerate MaxClimb T_05 1 338 199 757RR DEFAULT 4 4 Accelerate MaxClimb T_01 1 484,6 216,4 757RR DEFAULT 4 5 Accelerate MaxClimb ZERO 1 560 218,3 757RR DEFAULT 4 6 Climb MaxClimb ZERO 3 000 757RR DEFAULT 4 7 Accelerate MaxClimb ZERO 1 623,1 250 757RR DEFAULT 4 8 Climb MaxClimb T_00 5 500 757RR DEFAULT 4 9 Climb MaxClimb T_00 7 500 757RR DEFAULT 4 10 Climb MaxClimb T_00 10 000 757RR DEFAULT 5 1 Takeoff MaxTakeoff 5 757RR DEFAULT 5 2 Climb MaxTakeoff 5 1 000 757RR DEFAULT 5 3 Accelerate MaxClimb T_05 1 196,6 203,7 757RR DEFAULT 5 4 Accelerate MaxClimb T_01 1 325,3 221,1 757RR DEFAULT 5 5 Accelerate MaxClimb T_00 1 400 225,7 757RR DEFAULT 5 6 Climb MaxClimb ZERO 3 000 757RR DEFAULT 5 7 Accelerate MaxClimb ZERO 1 447,1 250 757RR DEFAULT 5 8 Climb MaxClimb T_00 5 500 757RR DEFAULT 5 9 Climb MaxClimb T_00 7 500 757RR DEFAULT 5 10 Climb MaxClimb ZERO 10 000 757RR DEFAULT 6 1 Takeoff MaxTakeoff 51.7.2015 EN Official Journal of the European Union L 168/375 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757RR DEFAULT 6 2 Climb MaxTakeoff 5 1 000 757RR DEFAULT 6 3 Accelerate MaxClimb T_05 1 142,2 205,8 757RR DEFAULT 6 4 Accelerate MaxClimb T_01 1 258 223,4 757RR DEFAULT 6 5 Accelerate MaxClimb T_00 1 329,6 228,9 757RR DEFAULT 6 6 Climb MaxClimb ZERO 3 000 757RR DEFAULT 6 7 Accelerate MaxClimb ZERO 1 377,4 250 757RR DEFAULT 6 8 Climb MaxClimb T_00 5 500 757RR DEFAULT 6 9 Climb MaxClimb T_00 7 500 757RR DEFAULT 6 10 Climb MaxClimb ZERO 10 000 757RR DEFAULT 7 1 Takeoff MaxTakeoff 5 757RR DEFAULT 7 2 Climb MaxTakeoff 5 1 000 757RR DEFAULT 7 3 Accelerate MaxClimb T_05 1 071,3 208,8 757RR DEFAULT 7 4 Accelerate MaxClimb T_01 1 181,5 226,7 757RR DEFAULT 7 5 Accelerate MaxClimb T_00 1 265,9 233,3 757RR DEFAULT 7 6 Climb MaxClimb ZERO 3 000 757RR DEFAULT 7 7 Accelerate MaxClimb ZERO 1 287,6 250 757RR DEFAULT 7 8 Climb MaxClimb T_00 5 500 757RR DEFAULT 7 9 Climb MaxClimb ZERO 7 500 757RR DEFAULT 7 10 Climb MaxClimb ZERO 10 000 757RR ICAO_A 1 1 Takeoff MaxTakeoff 5L 168/376 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757RR ICAO_A 1 2 Climb MaxTakeoff 5 1 500 757RR ICAO_A 1 3 Climb MaxClimb 5 3 000 757RR ICAO_A 1 4 Accelerate MaxClimb T_05 1 543,3 190,3 757RR ICAO_A 1 5 Accelerate MaxClimb T_01 1 735,6 206,1 757RR ICAO_A 1 6 Accelerate MaxClimb T_00 1 959,8 250 757RR ICAO_A 1 7 Climb MaxClimb ZERO 5 500 757RR ICAO_A 1 8 Climb MaxClimb ZERO 7 500 757RR ICAO_A 1 9 Climb MaxClimb ZERO 10 000 757RR ICAO_A 2 1 Takeoff MaxTakeoff 5 757RR ICAO_A 2 2 Climb MaxTakeoff 5 1 500 757RR ICAO_A 2 3 Climb MaxClimb 5 3 000 757RR ICAO_A 2 4 Accelerate MaxClimb T_05 1 472,7 191,9 757RR ICAO_A 2 5 Accelerate MaxClimb T_01 1 660,2 208,9 757RR ICAO_A 2 6 Accelerate MaxClimb T_00 1 876 250 757RR ICAO_A 2 7 Climb MaxClimb ZERO 5 500 757RR ICAO_A 2 8 Climb MaxClimb ZERO 7 500 757RR ICAO_A 2 9 Climb MaxClimb ZERO 10 000 757RR ICAO_A 3 1 Takeoff MaxTakeoff 5 757RR ICAO_A 3 2 Climb MaxTakeoff 5 1 500 757RR ICAO_A 3 3 Climb MaxClimb 5 3 0001.7.2015 EN Official Journal of the European Union L 168/377 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757RR ICAO_A 3 4 Accelerate MaxClimb T_05 1 401 193,6 757RR ICAO_A 3 5 Accelerate MaxClimb T_01 1 590,6 211,5 757RR ICAO_A 3 6 Accelerate MaxClimb T_00 1 769,2 250 757RR ICAO_A 3 7 Climb MaxClimb ZERO 5 500 757RR ICAO_A 3 8 Climb MaxClimb ZERO 7 500 757RR ICAO_A 3 9 Climb MaxClimb ZERO 10 000 757RR ICAO_A 4 1 Takeoff MaxTakeoff 5 757RR ICAO_A 4 2 Climb MaxTakeoff 5 1 500 757RR ICAO_A 4 3 Climb MaxClimb 5 3 000 757RR ICAO_A 4 4 Accelerate MaxClimb T_05 1 271,5 197,3 757RR ICAO_A 4 5 Accelerate MaxClimb T_01 1 436 214,5 757RR ICAO_A 4 6 Accelerate MaxClimb T_00 1 593,3 250 757RR ICAO_A 4 7 Climb MaxClimb ZERO 5 500 757RR ICAO_A 4 8 Climb MaxClimb ZERO 7 500 757RR ICAO_A 4 9 Climb MaxClimb T_00 10 000 757RR ICAO_A 5 1 Takeoff MaxTakeoff 5 757RR ICAO_A 5 2 Climb MaxTakeoff 5 1 500 757RR ICAO_A 5 3 Climb MaxClimb 5 3 000 757RR ICAO_A 5 4 Accelerate MaxClimb T_05 1 134,7 202,1 757RR ICAO_A 5 5 Accelerate MaxClimb T_01 1 278,3 219,8L 168/378 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757RR ICAO_A 5 6 Accelerate MaxClimb T_00 1 416,8 250 757RR ICAO_A 5 7 Climb MaxClimb ZERO 5 500 757RR ICAO_A 5 8 Climb MaxClimb ZERO 7 500 757RR ICAO_A 5 9 Climb MaxClimb ZERO 10 000 757RR ICAO_A 6 1 Takeoff MaxTakeoff 5 757RR ICAO_A 6 2 Climb MaxTakeoff 5 1 500 757RR ICAO_A 6 3 Climb MaxClimb 5 3 000 757RR ICAO_A 6 4 Accelerate MaxClimb T_05 1 083,2 204,3 757RR ICAO_A 6 5 Accelerate MaxClimb T_01 1 218,6 222,1 757RR ICAO_A 6 6 Accelerate MaxClimb T_00 1 348,5 250 757RR ICAO_A 6 7 Climb MaxClimb ZERO 5 500 757RR ICAO_A 6 8 Climb MaxClimb ZERO 7 500 757RR ICAO_A 6 9 Climb MaxClimb ZERO 10 000 757RR ICAO_A 7 1 Takeoff MaxTakeoff 5 757RR ICAO_A 7 2 Climb MaxTakeoff 5 1 500 757RR ICAO_A 7 3 Climb MaxClimb 5 3 000 757RR ICAO_A 7 4 Accelerate MaxClimb T_05 1 013,1 207,4 757RR ICAO_A 7 5 Accelerate MaxClimb T_01 1 137,3 225,4 757RR ICAO_A 7 6 Accelerate MaxClimb ZERO 1 256,7 250 757RR ICAO_A 7 7 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/379 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757RR ICAO_A 7 8 Climb MaxClimb ZERO 7 500 757RR ICAO_A 7 9 Climb MaxClimb ZERO 10 000 757RR ICAO_B 1 1 Takeoff MaxTakeoff 5 757RR ICAO_B 1 2 Climb MaxTakeoff 5 1 000 757RR ICAO_B 1 3 Accelerate MaxTakeoff T_05 2 227,2 201,9 757RR ICAO_B 1 4 Accelerate MaxTakeoff T_01 2 474,2 206,3 757RR ICAO_B 1 5 Climb MaxClimb ZERO 3 000 757RR ICAO_B 1 6 Accelerate MaxClimb ZERO 1 965,3 250 757RR ICAO_B 1 7 Climb MaxClimb ZERO 5 500 757RR ICAO_B 1 8 Climb MaxClimb ZERO 7 500 757RR ICAO_B 1 9 Climb MaxClimb ZERO 10 000 757RR ICAO_B 2 1 Takeoff MaxTakeoff 5 757RR ICAO_B 2 2 Climb MaxTakeoff 5 1 000 757RR ICAO_B 2 3 Accelerate MaxTakeoff T_05 2 139,9 203 757RR ICAO_B 2 4 Accelerate MaxTakeoff T_01 2 400 209,2 757RR ICAO_B 2 5 Climb MaxClimb ZERO 3 000 757RR ICAO_B 2 6 Accelerate MaxClimb T_00 1 876,9 250 757RR ICAO_B 2 7 Climb MaxClimb T_00 5 500 757RR ICAO_B 2 8 Climb MaxClimb ZERO 7 500 757RR ICAO_B 2 9 Climb MaxClimb ZERO 10 000L 168/380 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757RR ICAO_B 3 1 Takeoff MaxTakeoff 5 757RR ICAO_B 3 2 Climb MaxTakeoff 5 1 000 757RR ICAO_B 3 3 Accelerate MaxTakeoff T_05 2 051,2 204,3 757RR ICAO_B 3 4 Accelerate MaxTakeoff T_01 2 300 212,1 757RR ICAO_B 3 5 Climb MaxClimb ZERO 3 000 757RR ICAO_B 3 6 Accelerate MaxClimb T_00 1 788 250 757RR ICAO_B 3 7 Climb MaxClimb T_00 5 500 757RR ICAO_B 3 8 Climb MaxClimb T_00 7 500 757RR ICAO_B 3 9 Climb MaxClimb ZERO 10 000 757RR ICAO_B 4 1 Takeoff MaxTakeoff 5 757RR ICAO_B 4 2 Climb MaxTakeoff 5 1 000 757RR ICAO_B 4 3 Accelerate MaxTakeoff T_05 1 884,9 207,3 757RR ICAO_B 4 4 Accelerate MaxTakeoff T_01 2 135,6 218,4 757RR ICAO_B 4 5 Climb MaxClimb T_00 3 000 757RR ICAO_B 4 6 Accelerate MaxClimb T_00 1 621,6 250 757RR ICAO_B 4 7 Climb MaxClimb T_00 5 500 757RR ICAO_B 4 8 Climb MaxClimb T_00 7 500 757RR ICAO_B 4 9 Climb MaxClimb T_00 10 000 757RR ICAO_B 5 1 Takeoff MaxTakeoff 5 757RR ICAO_B 5 2 Climb MaxTakeoff 5 1 0001.7.2015 EN Official Journal of the European Union L 168/381 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757RR ICAO_B 5 3 Accelerate MaxTakeoff T_05 1 713,8 211,3 757RR ICAO_B 5 4 Accelerate MaxTakeoff T_01 1 935,5 225,8 757RR ICAO_B 5 5 Climb MaxClimb ZERO 3 000 757RR ICAO_B 5 6 Accelerate MaxClimb T_00 1 447,1 250 757RR ICAO_B 5 7 Climb MaxClimb T_00 5 500 757RR ICAO_B 5 8 Climb MaxClimb T_00 7 500 757RR ICAO_B 5 9 Climb MaxClimb T_00 10 000 757RR ICAO_B 6 1 Takeoff MaxTakeoff 5 757RR ICAO_B 6 2 Climb MaxTakeoff 5 1 000 757RR ICAO_B 6 3 Accelerate MaxTakeoff T_05 1 646,9 213,1 757RR ICAO_B 6 4 Accelerate MaxTakeoff T_01 1 872,3 228,9 757RR ICAO_B 6 5 Climb MaxClimb ZERO 3 000 757RR ICAO_B 6 6 Accelerate MaxClimb T_00 1 379,1 250 757RR ICAO_B 6 7 Climb MaxClimb T_00 5 500 757RR ICAO_B 6 8 Climb MaxClimb T_00 7 500 757RR ICAO_B 6 9 Climb MaxClimb T_00 10 000 757RR ICAO_B 7 1 Takeoff MaxTakeoff 5 757RR ICAO_B 7 2 Climb MaxTakeoff 5 1 000 757RR ICAO_B 7 3 Accelerate MaxTakeoff T_05 1 562,1 215,8 757RR ICAO_B 7 4 Accelerate MaxTakeoff T_01 1 781,3 233,3L 168/382 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 757RR ICAO_B 7 5 Climb MaxClimb ZERO 3 000 757RR ICAO_B 7 6 Accelerate MaxClimb T_00 1 287,6 250 757RR ICAO_B 7 7 Climb MaxClimb T_00 5 500 757RR ICAO_B 7 8 Climb MaxClimb T_00 7 500 757RR ICAO_B 7 9 Climb MaxClimb T_00 10 000 767300 DEFAULT 1 1 Takeoff MaxTakeoff 15 767300 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 767300 DEFAULT 1 3 Accelerate MaxTakeoff 15 2 198 152 767300 DEFAULT 1 4 Accelerate MaxTakeoff 5 2 198 172 767300 DEFAULT 1 5 Accelerate MaxClimb INT 1 000 215 767300 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 000 235 767300 DEFAULT 1 7 Climb MaxClimb ZERO 3 000 767300 DEFAULT 1 8 Accelerate MaxClimb ZERO 1 000 250 767300 DEFAULT 1 9 Climb MaxClimb ZERO 5 500 767300 DEFAULT 1 10 Climb MaxClimb ZERO 7 500 767300 DEFAULT 1 11 Climb MaxClimb ZERO 10 000 767300 DEFAULT 2 1 Takeoff MaxTakeoff 15 767300 DEFAULT 2 2 Climb MaxTakeoff 15 1 000 767300 DEFAULT 2 3 Accelerate MaxTakeoff 15 2 112 155 767300 DEFAULT 2 4 Accelerate MaxTakeoff 5 2 112 1751.7.2015 EN Official Journal of the European Union L 168/383 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767300 DEFAULT 2 5 Accelerate MaxClimb INT 1 000 218 767300 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 000 238 767300 DEFAULT 2 7 Climb MaxClimb ZERO 3 000 767300 DEFAULT 2 8 Accelerate MaxClimb ZERO 1 000 250 767300 DEFAULT 2 9 Climb MaxClimb ZERO 5 500 767300 DEFAULT 2 10 Climb MaxClimb ZERO 7 500 767300 DEFAULT 2 11 Climb MaxClimb ZERO 10 000 767300 DEFAULT 3 1 Takeoff MaxTakeoff 15 767300 DEFAULT 3 2 Climb MaxTakeoff 15 1 000 767300 DEFAULT 3 3 Accelerate MaxTakeoff 15 2 029 158 767300 DEFAULT 3 4 Accelerate MaxTakeoff 5 2 029 178 767300 DEFAULT 3 5 Accelerate MaxClimb INT 1 000 221 767300 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 000 241 767300 DEFAULT 3 7 Climb MaxClimb ZERO 3 000 767300 DEFAULT 3 8 Accelerate MaxClimb ZERO 1 000 250 767300 DEFAULT 3 9 Climb MaxClimb ZERO 5 500 767300 DEFAULT 3 10 Climb MaxClimb ZERO 7 500 767300 DEFAULT 3 11 Climb MaxClimb ZERO 10 000 767300 DEFAULT 4 1 Takeoff MaxTakeoff 15 767300 DEFAULT 4 2 Climb MaxTakeoff 15 1 000L 168/384 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767300 DEFAULT 4 3 Accelerate MaxTakeoff 15 1 895 163 767300 DEFAULT 4 4 Accelerate MaxTakeoff 5 1 895 183 767300 DEFAULT 4 5 Accelerate MaxClimb INT 1 000 225 767300 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 000 245 767300 DEFAULT 4 7 Climb MaxClimb ZERO 3 000 767300 DEFAULT 4 8 Accelerate MaxClimb ZERO 1 000 250 767300 DEFAULT 4 9 Climb MaxClimb ZERO 5 500 767300 DEFAULT 4 10 Climb MaxClimb ZERO 7 500 767300 DEFAULT 4 11 Climb MaxClimb ZERO 10 000 767300 DEFAULT 5 1 Takeoff MaxTakeoff 15 767300 DEFAULT 5 2 Climb MaxTakeoff 15 1 000 767300 DEFAULT 5 3 Accelerate MaxTakeoff 15 1 744 169 767300 DEFAULT 5 4 Accelerate MaxTakeoff 5 1 744 189 767300 DEFAULT 5 5 Accelerate MaxClimb INT 1 000 231 767300 DEFAULT 5 6 Accelerate MaxClimb ZERO 1 000 251 767300 DEFAULT 5 7 Climb MaxClimb ZERO 3 000 767300 DEFAULT 5 8 Climb MaxClimb ZERO 5 500 767300 DEFAULT 5 9 Climb MaxClimb ZERO 7 500 767300 DEFAULT 5 10 Climb MaxClimb ZERO 10 000 767300 DEFAULT 6 1 Takeoff MaxTakeoff 151.7.2015 EN Official Journal of the European Union L 168/385 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767300 DEFAULT 6 2 Climb MaxTakeoff 15 1 000 767300 DEFAULT 6 3 Accelerate MaxTakeoff 15 1 602 175 767300 DEFAULT 6 4 Accelerate MaxTakeoff 5 1 602 195 767300 DEFAULT 6 5 Accelerate MaxClimb INT 1 000 237 767300 DEFAULT 6 6 Accelerate MaxClimb ZERO 1 000 257 767300 DEFAULT 6 7 Climb MaxClimb ZERO 3 000 767300 DEFAULT 6 8 Climb MaxClimb ZERO 5 500 767300 DEFAULT 6 9 Climb MaxClimb ZERO 7 500 767300 DEFAULT 6 10 Climb MaxClimb ZERO 10 000 767300 DEFAULT 7 1 Takeoff MaxTakeoff 15 767300 DEFAULT 7 2 Climb MaxTakeoff 15 1 000 767300 DEFAULT 7 3 Accelerate MaxTakeoff 15 1 542 178 767300 DEFAULT 7 4 Accelerate MaxTakeoff 5 1 542 198 767300 DEFAULT 7 5 Accelerate MaxClimb INT 1 000 240 767300 DEFAULT 7 6 Accelerate MaxClimb ZERO 1 000 260 767300 DEFAULT 7 7 Climb MaxClimb ZERO 3 000 767300 DEFAULT 7 8 Climb MaxClimb ZERO 5 500 767300 DEFAULT 7 9 Climb MaxClimb ZERO 7 500 767300 DEFAULT 7 10 Climb MaxClimb ZERO 10 000 767400 DEFAULT 1 1 Takeoff MaxTakeoff T_20_UL 168/386 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767400 DEFAULT 1 2 Climb MaxTakeoff T_20_U 1 000 767400 DEFAULT 1 3 Accelerate MaxClimb T_05_U 1 695,3 215,4 767400 DEFAULT 1 4 Climb MaxClimb T_00_U 3 000 767400 DEFAULT 1 5 Accelerate MaxClimb T_00_U 2 123,3 250 767400 DEFAULT 1 6 Climb MaxClimb T_00_U 5 500 767400 DEFAULT 1 7 Climb MaxClimb T_00_U 7 500 767400 DEFAULT 1 8 Climb MaxClimb T_00_U 10 000 767400 DEFAULT 2 1 Takeoff MaxTakeoff T_20_U 767400 DEFAULT 2 2 Climb MaxTakeoff T_20_U 1 000 767400 DEFAULT 2 3 Accelerate MaxClimb T_05_U 1 648,7 217,9 767400 DEFAULT 2 4 Climb MaxClimb T_00_U 3 000 767400 DEFAULT 2 5 Accelerate MaxClimb T_00_U 2 040,6 250 767400 DEFAULT 2 6 Climb MaxClimb T_00_U 5 500 767400 DEFAULT 2 7 Climb MaxClimb T_00_U 7 500 767400 DEFAULT 2 8 Climb MaxClimb T_00_U 10 000 767400 DEFAULT 3 1 Takeoff MaxTakeoff T_20_U 767400 DEFAULT 3 2 Climb MaxTakeoff T_20_U 1 000 767400 DEFAULT 3 3 Accelerate MaxClimb T_05_U 1 584,9 220,5 767400 DEFAULT 3 4 Climb MaxClimb T_00_U 3 000 767400 DEFAULT 3 5 Accelerate MaxClimb T_00_U 1 953,3 2501.7.2015 EN Official Journal of the European Union L 168/387 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767400 DEFAULT 3 6 Climb MaxClimb T_00_U 5 500 767400 DEFAULT 3 7 Climb MaxClimb T_00_U 7 500 767400 DEFAULT 3 8 Climb MaxClimb T_00_U 10 000 767400 DEFAULT 4 1 Takeoff MaxTakeoff T_20_U 767400 DEFAULT 4 2 Climb MaxTakeoff T_20_U 1 000 767400 DEFAULT 4 3 Accelerate MaxClimb T_05_U 1 482,5 225,1 767400 DEFAULT 4 4 Climb MaxClimb T_00_U 3 000 767400 DEFAULT 4 5 Accelerate MaxClimb T_00_U 1 821,8 250 767400 DEFAULT 4 6 Climb MaxClimb T_00_U 5 500 767400 DEFAULT 4 7 Climb MaxClimb T_00_U 7 500 767400 DEFAULT 4 8 Climb MaxClimb T_00_U 10 000 767400 DEFAULT 5 1 Takeoff MaxTakeoff T_20_U 767400 DEFAULT 5 2 Climb MaxTakeoff T_20_U 1 000 767400 DEFAULT 5 3 Accelerate MaxClimb T_05_U 1 360,1 230,5 767400 DEFAULT 5 4 Climb MaxClimb T_00_U 3 000 767400 DEFAULT 5 5 Accelerate MaxClimb T_00_U 1 661,5 250 767400 DEFAULT 5 6 Climb MaxClimb T_00_U 5 500 767400 DEFAULT 5 7 Climb MaxClimb T_00_U 7 500 767400 DEFAULT 5 8 Climb MaxClimb T_00_U 10 000 767400 DEFAULT 6 1 Takeoff MaxTakeoff T_20_UL 168/388 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767400 DEFAULT 6 2 Climb MaxTakeoff T_20_U 1 000 767400 DEFAULT 6 3 Accelerate MaxClimb T_05_U 1 246,4 236 767400 DEFAULT 6 4 Climb MaxClimb T_00_U 3 000 767400 DEFAULT 6 5 Accelerate MaxClimb T_00_U 1 508 250 767400 DEFAULT 6 6 Climb MaxClimb T_00_U 5 500 767400 DEFAULT 6 7 Climb MaxClimb T_00_U 7 500 767400 DEFAULT 6 8 Climb MaxClimb T_00_U 10 000 767400 DEFAULT 7 1 Takeoff MaxTakeoff T_20_U 767400 DEFAULT 7 2 Climb MaxTakeoff T_20_U 1 000 767400 DEFAULT 7 3 Accelerate MaxClimb T_05_U 1 091,3 244,3 767400 DEFAULT 7 4 Climb MaxClimb T_00_U 3 000 767400 DEFAULT 7 5 Accelerate MaxClimb T_00_U 1 303,8 250 767400 DEFAULT 7 6 Climb MaxClimb T_00_U 5 500 767400 DEFAULT 7 7 Climb MaxClimb T_00_U 7 500 767400 DEFAULT 7 8 Climb MaxClimb T_00_U 10 000 767400 ICAO_A 1 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_A 1 2 Climb MaxTakeoff T_20_U 1 500 767400 ICAO_A 1 3 Climb MaxClimb T_20_U 3 000 767400 ICAO_A 1 4 Accelerate MaxClimb T_05A 1 659,9 215,1 767400 ICAO_A 1 5 Climb MaxClimb T_00_U 4 6161.7.2015 EN Official Journal of the European Union L 168/389 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767400 ICAO_A 1 6 Accelerate MaxClimb T_00_U 2 098,5 250 767400 ICAO_A 1 7 Climb MaxClimb T_00_U 5 500 767400 ICAO_A 1 8 Climb MaxClimb T_00_U 7 500 767400 ICAO_A 1 9 Climb MaxClimb T_00_U 10 000 767400 ICAO_A 2 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_A 2 2 Climb MaxTakeoff T_20_U 1 500 767400 ICAO_A 2 3 Climb MaxClimb T_20_U 3 000 767400 ICAO_A 2 4 Accelerate MaxClimb T_05A 1 600 217,6 767400 ICAO_A 2 5 Climb MaxClimb T_00_U 4 536 767400 ICAO_A 2 6 Accelerate MaxClimb T_00_U 2 008 250 767400 ICAO_A 2 7 Climb MaxClimb T_00_U 5 500 767400 ICAO_A 2 8 Climb MaxClimb T_00_U 7 500 767400 ICAO_A 2 9 Climb MaxClimb T_00_U 10 000 767400 ICAO_A 3 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_A 3 2 Climb MaxTakeoff T_20_U 1 500 767400 ICAO_A 3 3 Climb MaxClimb T_20_U 3 000 767400 ICAO_A 3 4 Accelerate MaxClimb T_05B 1 536,2 220,4 767400 ICAO_A 3 5 Climb MaxClimb T_00_U 4 454 767400 ICAO_A 3 6 Accelerate MaxClimb T_00_U 1 935,8 250 767400 ICAO_A 3 7 Climb MaxClimb T_00_U 5 500L 168/390 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767400 ICAO_A 3 8 Climb MaxClimb T_00_U 7 500 767400 ICAO_A 3 9 Climb MaxClimb T_00_U 10 000 767400 ICAO_A 4 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_A 4 2 Climb MaxTakeoff T_20_U 1 500 767400 ICAO_A 4 3 Climb MaxClimb T_20_U 3 000 767400 ICAO_A 4 4 Accelerate MaxClimb T_05B 1 434,4 224,8 767400 ICAO_A 4 5 Climb MaxClimb T_00_U 4 323 767400 ICAO_A 4 6 Accelerate MaxClimb T_00_U 1 796,6 250 767400 ICAO_A 4 7 Climb MaxClimb T_00_U 5 500 767400 ICAO_A 4 8 Climb MaxClimb T_00_U 7 500 767400 ICAO_A 4 9 Climb MaxClimb T_00_U 10 000 767400 ICAO_A 5 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_A 5 2 Climb MaxTakeoff T_20_U 1 500 767400 ICAO_A 5 3 Climb MaxClimb T_20_U 3 000 767400 ICAO_A 5 4 Accelerate MaxClimb T_05B 1 318,8 230,2 767400 ICAO_A 5 5 Climb MaxClimb T_00_U 4 173 767400 ICAO_A 5 6 Accelerate MaxClimb T_00_U 1 640 250 767400 ICAO_A 5 7 Climb MaxClimb T_00_U 5 500 767400 ICAO_A 5 8 Climb MaxClimb T_00_U 7 500 767400 ICAO_A 5 9 Climb MaxClimb T_00_U 10 0001.7.2015 EN Official Journal of the European Union L 168/391 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767400 ICAO_A 6 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_A 6 2 Climb MaxTakeoff T_20_U 1 500 767400 ICAO_A 6 3 Climb MaxClimb T_20_U 3 000 767400 ICAO_A 6 4 Accelerate MaxClimb T_05B 1 258,5 250 767400 ICAO_A 6 5 Climb MaxClimb T_00_U 5 500 767400 ICAO_A 6 6 Climb MaxClimb T_00_U 7 500 767400 ICAO_A 6 7 Climb MaxClimb T_00_U 10 000 767400 ICAO_A 7 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_A 7 2 Climb MaxTakeoff T_20_U 1 500 767400 ICAO_A 7 3 Climb MaxClimb T_20_U 3 000 767400 ICAO_A 7 4 Accelerate MaxClimb T_05B 1 073 250 767400 ICAO_A 7 5 Climb MaxClimb T_00_U 5 500 767400 ICAO_A 7 6 Climb MaxClimb T_00_U 7 500 767400 ICAO_A 7 7 Climb MaxClimb T_00_U 10 000 767400 ICAO_B 1 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_B 1 2 Climb MaxTakeoff T_20_U 1 000 767400 ICAO_B 1 3 Accelerate MaxTakeoff T_05_U 2 330,5 215,3 767400 ICAO_B 1 4 Climb MaxTakeoff T_00_U 3 491 767400 ICAO_B 1 5 Accelerate MaxClimb T_00_U 2 147 250 767400 ICAO_B 1 6 Climb MaxClimb T_00_U 5 000L 168/392 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767400 ICAO_B 1 7 Climb MaxClimb T_00_U 7 500 767400 ICAO_B 1 8 Climb MaxClimb T_00_U 10 000 767400 ICAO_B 2 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_B 2 2 Climb MaxTakeoff T_20_U 1 000 767400 ICAO_B 2 3 Accelerate MaxTakeoff T_05_U 2 267,2 217,9 767400 ICAO_B 2 4 Climb MaxTakeoff T_00_U 3 393 767400 ICAO_B 2 5 Accelerate MaxClimb T_00_U 2 080,9 250 767400 ICAO_B 2 6 Climb MaxClimb T_00_U 5 000 767400 ICAO_B 2 7 Climb MaxClimb T_00_U 7 500 767400 ICAO_B 2 8 Climb MaxClimb T_00_U 10 000 767400 ICAO_B 3 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_B 3 2 Climb MaxTakeoff T_20_U 1 000 767400 ICAO_B 3 3 Accelerate MaxTakeoff T_05_U 2 183,7 220,6 767400 ICAO_B 3 4 Climb MaxTakeoff T_00_U 3 292 767400 ICAO_B 3 5 Accelerate MaxClimb T_00_U 1 975,7 250 767400 ICAO_B 3 6 Climb MaxClimb T_00_U 5 000 767400 ICAO_B 3 7 Climb MaxClimb T_00_U 7 500 767400 ICAO_B 3 8 Climb MaxClimb T_00_U 10 000 767400 ICAO_B 4 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_B 4 2 Climb MaxTakeoff T_20_U 1 0001.7.2015 EN Official Journal of the European Union L 168/393 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767400 ICAO_B 4 3 Accelerate MaxTakeoff T_05_U 2 054,4 225 767400 ICAO_B 4 4 Climb MaxTakeoff T_00_U 3 128 767400 ICAO_B 4 5 Accelerate MaxClimb T_00_U 1 850,9 250 767400 ICAO_B 4 6 Climb MaxClimb T_00_U 5 000 767400 ICAO_B 4 7 Climb MaxClimb T_00_U 7 500 767400 ICAO_B 4 8 Climb MaxClimb T_00_U 10 000 767400 ICAO_B 5 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_B 5 2 Climb MaxTakeoff T_20_U 1 000 767400 ICAO_B 5 3 Accelerate MaxTakeoff T_05_U 1 908,2 230,4 767400 ICAO_B 5 4 Climb MaxTakeoff T_00_U 2 944 767400 ICAO_B 5 5 Climb MaxClimb T_00_U 3 000 767400 ICAO_B 5 6 Accelerate MaxClimb T_00_U 1 653,1 250 767400 ICAO_B 5 7 Climb MaxClimb T_00_U 5 000 767400 ICAO_B 5 8 Climb MaxClimb T_00_U 7 500 767400 ICAO_B 5 9 Climb MaxClimb T_00_U 10 000 767400 ICAO_B 6 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_B 6 2 Climb MaxTakeoff T_20_U 1 000 767400 ICAO_B 6 3 Accelerate MaxTakeoff T_05_U 1 771,1 236 767400 ICAO_B 6 4 Climb MaxTakeoff T_00_U 2 766 767400 ICAO_B 6 5 Climb MaxClimb T_00_U 3 000L 168/394 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767400 ICAO_B 6 6 Accelerate MaxClimb T_00_U 1 521,4 250 767400 ICAO_B 6 7 Climb MaxClimb T_00_U 5 000 767400 ICAO_B 6 8 Climb MaxClimb T_00_U 7 500 767400 ICAO_B 6 9 Climb MaxClimb T_00_U 10 000 767400 ICAO_B 7 1 Takeoff MaxTakeoff T_20_U 767400 ICAO_B 7 2 Climb MaxTakeoff T_20_U 1 000 767400 ICAO_B 7 3 Accelerate MaxTakeoff T_05_U 1 560,3 239,8 767400 ICAO_B 7 4 Climb MaxTakeoff T_00_U 2 111 767400 ICAO_B 7 5 Accelerate MaxTakeoff T_00_U 1 840 244,3 767400 ICAO_B 7 6 Climb MaxTakeoff T_00_U 2 523 767400 ICAO_B 7 7 Climb MaxClimb T_00_U 3 000 767400 ICAO_B 7 8 Accelerate MaxClimb T_00_U 1 303,8 250 767400 ICAO_B 7 9 Climb MaxClimb T_00_U 5 000 767400 ICAO_B 7 10 Climb MaxClimb T_00_U 7 500 767400 ICAO_B 7 11 Climb MaxClimb T_00_U 10 000 767CF6 DEFAULT 1 1 Takeoff MaxTakeoff 15 767CF6 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 767CF6 DEFAULT 1 3 Accelerate MaxTakeoff 15 1 913 144 767CF6 DEFAULT 1 4 Accelerate MaxTakeoff 5 1 913 164 767CF6 DEFAULT 1 5 Accelerate MaxClimb 1 1 000 2041.7.2015 EN Official Journal of the European Union L 168/395 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767CF6 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 000 224 767CF6 DEFAULT 1 7 Climb MaxClimb ZERO 3 000 767CF6 DEFAULT 1 8 Accelerate MaxClimb ZERO 1 000 250 767CF6 DEFAULT 1 9 Climb MaxClimb ZERO 5 500 767CF6 DEFAULT 1 10 Climb MaxClimb ZERO 7 500 767CF6 DEFAULT 1 11 Climb MaxClimb ZERO 10 000 767CF6 DEFAULT 2 1 Takeoff MaxTakeoff 15 767CF6 DEFAULT 2 2 Climb MaxTakeoff 15 1 000 767CF6 DEFAULT 2 3 Accelerate MaxTakeoff 15 1 840 147 767CF6 DEFAULT 2 4 Accelerate MaxTakeoff 5 1 840 167 767CF6 DEFAULT 2 5 Accelerate MaxClimb 1 1 000 206 767CF6 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 000 226 767CF6 DEFAULT 2 7 Climb MaxClimb ZERO 3 000 767CF6 DEFAULT 2 8 Accelerate MaxClimb ZERO 1 000 250 767CF6 DEFAULT 2 9 Climb MaxClimb ZERO 5 500 767CF6 DEFAULT 2 10 Climb MaxClimb ZERO 7 500 767CF6 DEFAULT 2 11 Climb MaxClimb ZERO 10 000 767CF6 DEFAULT 3 1 Takeoff MaxTakeoff 15 767CF6 DEFAULT 3 2 Climb MaxTakeoff 15 1 000 767CF6 DEFAULT 3 3 Accelerate MaxTakeoff 15 1 769 150L 168/396 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767CF6 DEFAULT 3 4 Accelerate MaxTakeoff 5 1 769 170 767CF6 DEFAULT 3 5 Accelerate MaxClimb 1 1 000 209 767CF6 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 000 229 767CF6 DEFAULT 3 7 Climb MaxClimb ZERO 3 000 767CF6 DEFAULT 3 8 Accelerate MaxClimb ZERO 1 000 250 767CF6 DEFAULT 3 9 Climb MaxClimb ZERO 5 500 767CF6 DEFAULT 3 10 Climb MaxClimb ZERO 7 500 767CF6 DEFAULT 3 11 Climb MaxClimb ZERO 10 000 767CF6 DEFAULT 4 1 Takeoff MaxTakeoff 15 767CF6 DEFAULT 4 2 Climb MaxTakeoff 15 1 000 767CF6 DEFAULT 4 3 Accelerate MaxTakeoff 15 1 656 155 767CF6 DEFAULT 4 4 Accelerate MaxTakeoff 5 1 656 175 767CF6 DEFAULT 4 5 Accelerate MaxClimb 1 1 000 214 767CF6 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 000 234 767CF6 DEFAULT 4 7 Climb MaxClimb ZERO 3 000 767CF6 DEFAULT 4 8 Accelerate MaxClimb ZERO 1 000 250 767CF6 DEFAULT 4 9 Climb MaxClimb ZERO 5 500 767CF6 DEFAULT 4 10 Climb MaxClimb ZERO 7 500 767CF6 DEFAULT 4 11 Climb MaxClimb ZERO 10 000 767CF6 DEFAULT 5 1 Takeoff MaxTakeoff 151.7.2015 EN Official Journal of the European Union L 168/397 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767CF6 DEFAULT 5 2 Climb MaxTakeoff 15 1 000 767CF6 DEFAULT 5 3 Accelerate MaxTakeoff 15 1 529 160 767CF6 DEFAULT 5 4 Accelerate MaxTakeoff 5 1 529 180 767CF6 DEFAULT 5 5 Accelerate MaxClimb 1 1 000 219 767CF6 DEFAULT 5 6 Accelerate MaxClimb ZERO 1 000 239 767CF6 DEFAULT 5 7 Climb MaxClimb ZERO 3 000 767CF6 DEFAULT 5 8 Accelerate MaxClimb ZERO 1 000 250 767CF6 DEFAULT 5 9 Climb MaxClimb ZERO 5 500 767CF6 DEFAULT 5 10 Climb MaxClimb ZERO 7 500 767CF6 DEFAULT 5 11 Climb MaxClimb ZERO 10 000 767CF6 DEFAULT 6 1 Takeoff MaxTakeoff 15 767CF6 DEFAULT 6 2 Climb MaxTakeoff 15 1 000 767CF6 DEFAULT 6 3 Accelerate MaxTakeoff 15 1 407 166 767CF6 DEFAULT 6 4 Accelerate MaxTakeoff 5 1 407 186 767CF6 DEFAULT 6 5 Accelerate MaxClimb 1 1 000 225 767CF6 DEFAULT 6 6 Accelerate MaxClimb ZERO 1 000 245 767CF6 DEFAULT 6 7 Climb MaxClimb ZERO 3 000 767CF6 DEFAULT 6 8 Accelerate MaxClimb ZERO 1 000 250 767CF6 DEFAULT 6 9 Climb MaxClimb ZERO 5 500 767CF6 DEFAULT 6 10 Climb MaxClimb ZERO 7 500L 168/398 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767CF6 DEFAULT 6 11 Climb MaxClimb ZERO 10 000 767CF6 DEFAULT 7 1 Takeoff MaxTakeoff 15 767CF6 DEFAULT 7 2 Climb MaxTakeoff 15 1 000 767CF6 DEFAULT 7 3 Accelerate MaxTakeoff 15 1 345 169 767CF6 DEFAULT 7 4 Accelerate MaxTakeoff 5 1 345 189 767CF6 DEFAULT 7 5 Accelerate MaxClimb 1 1 000 228 767CF6 DEFAULT 7 6 Accelerate MaxClimb ZERO 1 000 248 767CF6 DEFAULT 7 7 Climb MaxClimb ZERO 3 000 767CF6 DEFAULT 7 8 Accelerate MaxClimb ZERO 1 000 250 767CF6 DEFAULT 7 9 Climb MaxClimb ZERO 5 500 767CF6 DEFAULT 7 10 Climb MaxClimb ZERO 7 500 767CF6 DEFAULT 7 11 Climb MaxClimb ZERO 10 000 767JT9 DEFAULT 1 1 Takeoff MaxTakeoff 15 767JT9 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 767JT9 DEFAULT 1 3 Accelerate MaxTakeoff 15 1 879 145 767JT9 DEFAULT 1 4 Accelerate MaxTakeoff 5 1 879 165 767JT9 DEFAULT 1 5 Accelerate MaxClimb 1 1 000 204 767JT9 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 000 224 767JT9 DEFAULT 1 7 Climb MaxClimb ZERO 3 000 767JT9 DEFAULT 1 8 Accelerate MaxClimb ZERO 1 000 2501.7.2015 EN Official Journal of the European Union L 168/399 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767JT9 DEFAULT 1 9 Climb MaxClimb ZERO 5 500 767JT9 DEFAULT 1 10 Climb MaxClimb ZERO 7 500 767JT9 DEFAULT 1 11 Climb MaxClimb ZERO 10 000 767JT9 DEFAULT 2 1 Takeoff MaxTakeoff 15 767JT9 DEFAULT 2 2 Climb MaxTakeoff 15 1 000 767JT9 DEFAULT 2 3 Accelerate MaxTakeoff 15 1 807 148 767JT9 DEFAULT 2 4 Accelerate MaxTakeoff 5 1 807 168 767JT9 DEFAULT 2 5 Accelerate MaxClimb 1 1 000 207 767JT9 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 000 227 767JT9 DEFAULT 2 7 Climb MaxClimb ZERO 3 000 767JT9 DEFAULT 2 8 Accelerate MaxClimb ZERO 1 000 250 767JT9 DEFAULT 2 9 Climb MaxClimb ZERO 5 500 767JT9 DEFAULT 2 10 Climb MaxClimb ZERO 7 500 767JT9 DEFAULT 2 11 Climb MaxClimb ZERO 10 000 767JT9 DEFAULT 3 1 Takeoff MaxTakeoff 15 767JT9 DEFAULT 3 2 Climb MaxTakeoff 15 1 000 767JT9 DEFAULT 3 3 Accelerate MaxTakeoff 15 1 738 150 767JT9 DEFAULT 3 4 Accelerate MaxTakeoff 5 1 738 170 767JT9 DEFAULT 3 5 Accelerate MaxClimb 1 1 000 210 767JT9 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 000 230L 168/400 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767JT9 DEFAULT 3 7 Climb MaxClimb ZERO 3 000 767JT9 DEFAULT 3 8 Accelerate MaxClimb ZERO 1 000 250 767JT9 DEFAULT 3 9 Climb MaxClimb ZERO 5 500 767JT9 DEFAULT 3 10 Climb MaxClimb ZERO 7 500 767JT9 DEFAULT 3 11 Climb MaxClimb ZERO 10 000 767JT9 DEFAULT 4 1 Takeoff MaxTakeoff 15 767JT9 DEFAULT 4 2 Climb MaxTakeoff 15 1 000 767JT9 DEFAULT 4 3 Accelerate MaxTakeoff 15 1 626 155 767JT9 DEFAULT 4 4 Accelerate MaxTakeoff 5 1 626 175 767JT9 DEFAULT 4 5 Accelerate MaxClimb 1 1 000 214 767JT9 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 000 234 767JT9 DEFAULT 4 7 Climb MaxClimb ZERO 3 000 767JT9 DEFAULT 4 8 Accelerate MaxClimb ZERO 1 000 250 767JT9 DEFAULT 4 9 Climb MaxClimb ZERO 5 500 767JT9 DEFAULT 4 10 Climb MaxClimb ZERO 7 500 767JT9 DEFAULT 4 11 Climb MaxClimb ZERO 10 000 767JT9 DEFAULT 5 1 Takeoff MaxTakeoff 15 767JT9 DEFAULT 5 2 Climb MaxTakeoff 15 1 000 767JT9 DEFAULT 5 3 Accelerate MaxTakeoff 15 1 499 161 767JT9 DEFAULT 5 4 Accelerate MaxTakeoff 5 1 499 1811.7.2015 EN Official Journal of the European Union L 168/401 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767JT9 DEFAULT 5 5 Accelerate MaxClimb 1 1 000 220 767JT9 DEFAULT 5 6 Accelerate MaxClimb ZERO 1 000 240 767JT9 DEFAULT 5 7 Climb MaxClimb ZERO 3 000 767JT9 DEFAULT 5 8 Accelerate MaxClimb ZERO 1 000 250 767JT9 DEFAULT 5 9 Climb MaxClimb ZERO 5 500 767JT9 DEFAULT 5 10 Climb MaxClimb ZERO 7 500 767JT9 DEFAULT 5 11 Climb MaxClimb ZERO 10 000 767JT9 DEFAULT 6 1 Takeoff MaxTakeoff 15 767JT9 DEFAULT 6 2 Climb MaxTakeoff 15 1 000 767JT9 DEFAULT 6 3 Accelerate MaxTakeoff 15 1 379 167 767JT9 DEFAULT 6 4 Accelerate MaxTakeoff 5 1 379 187 767JT9 DEFAULT 6 5 Accelerate MaxClimb 1 1 000 226 767JT9 DEFAULT 6 6 Accelerate MaxClimb ZERO 1 000 246 767JT9 DEFAULT 6 7 Climb MaxClimb ZERO 3 000 767JT9 DEFAULT 6 8 Accelerate MaxClimb ZERO 1 000 250 767JT9 DEFAULT 6 9 Climb MaxClimb ZERO 5 500 767JT9 DEFAULT 6 10 Climb MaxClimb ZERO 7 500 767JT9 DEFAULT 6 11 Climb MaxClimb ZERO 10 000 767JT9 DEFAULT 7 1 Takeoff MaxTakeoff 15 767JT9 DEFAULT 7 2 Climb MaxTakeoff 15 1 000L 168/402 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 767JT9 DEFAULT 7 3 Accelerate MaxTakeoff 15 1 328 170 767JT9 DEFAULT 7 4 Accelerate MaxTakeoff 5 1 328 190 767JT9 DEFAULT 7 5 Accelerate MaxClimb 1 1 000 228 767JT9 DEFAULT 7 6 Accelerate MaxClimb ZERO 1 000 248 767JT9 DEFAULT 7 7 Climb MaxClimb ZERO 3 000 767JT9 DEFAULT 7 8 Accelerate MaxClimb ZERO 1 000 250 767JT9 DEFAULT 7 9 Climb MaxClimb ZERO 5 500 767JT9 DEFAULT 7 10 Climb MaxClimb ZERO 7 500 767JT9 DEFAULT 7 11 Climb MaxClimb ZERO 10 000 777200 DEFAULT 1 1 Takeoff MaxTakeoff T_05 777200 DEFAULT 1 2 Climb MaxTakeoff T_05C 1 089 777200 DEFAULT 1 3 Accelerate MaxClimb T_01 1 583,4 205,9 777200 DEFAULT 1 4 Accelerate MaxClimb T_00 1 744,7 213,7 777200 DEFAULT 1 5 Climb MaxClimb T_00 3 000 777200 DEFAULT 1 6 Accelerate MaxClimb T_00 1 856,6 250 777200 DEFAULT 1 7 Climb MaxClimb T_00 5 500 777200 DEFAULT 1 8 Climb MaxClimb T_00 7 500 777200 DEFAULT 1 9 Climb MaxClimb T_00 10 000 777200 DEFAULT 2 1 Takeoff MaxTakeoff T_05 777200 DEFAULT 2 2 Climb MaxTakeoff T_05C 1 0571.7.2015 EN Official Journal of the European Union L 168/403 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777200 DEFAULT 2 3 Accelerate MaxClimb T_01 1 526,8 206,6 777200 DEFAULT 2 4 Accelerate MaxClimb T_00 1 681 215,6 777200 DEFAULT 2 5 Climb MaxClimb T_00 3 000 777200 DEFAULT 2 6 Accelerate MaxClimb T_00 1 791,2 250 777200 DEFAULT 2 7 Climb MaxClimb T_00 5 500 777200 DEFAULT 2 8 Climb MaxClimb T_00 7 500 777200 DEFAULT 2 9 Climb MaxClimb T_00 10 000 777200 DEFAULT 3 1 Takeoff MaxTakeoff T_05 777200 DEFAULT 3 2 Climb MaxTakeoff T_05C 1 022 777200 DEFAULT 3 3 Accelerate MaxClimb T_01 1 468,5 207,3 777200 DEFAULT 3 4 Accelerate MaxClimb T_00 1 618,3 217,7 777200 DEFAULT 3 5 Climb MaxClimb T_00 3 000 777200 DEFAULT 3 6 Accelerate MaxClimb T_00 1 725,7 250 777200 DEFAULT 3 7 Climb MaxClimb T_00 5 500 777200 DEFAULT 3 8 Climb MaxClimb T_00 7 500 777200 DEFAULT 3 9 Climb MaxClimb T_00 10 000 777200 DEFAULT 4 1 Takeoff MaxTakeoff T_05 777200 DEFAULT 4 2 Climb MaxTakeoff T_05C 1 000 777200 DEFAULT 4 3 Accelerate MaxClimb T_01 1 363,3 208,9 777200 DEFAULT 4 4 Accelerate MaxClimb T_00 1 510,5 221,7L 168/404 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777200 DEFAULT 4 5 Climb MaxClimb T_00 3 000 777200 DEFAULT 4 6 Accelerate MaxClimb T_00 1 601,3 250 777200 DEFAULT 4 7 Climb MaxClimb T_00 5 500 777200 DEFAULT 4 8 Climb MaxClimb T_00 7 500 777200 DEFAULT 4 9 Climb MaxClimb T_00 10 000 777200 DEFAULT 5 1 Takeoff MaxTakeoff T_05 777200 DEFAULT 5 2 Climb MaxTakeoff T_05C 1 000 777200 DEFAULT 5 3 Accelerate MaxClimb T_01 1 247,5 211 777200 DEFAULT 5 4 Accelerate MaxClimb T_00 1 389,1 225,5 777200 DEFAULT 5 5 Climb MaxClimb T_00 3 000 777200 DEFAULT 5 6 Accelerate MaxClimb T_00 1 467,1 250 777200 DEFAULT 5 7 Climb MaxClimb T_00 5 500 777200 DEFAULT 5 8 Climb MaxClimb T_00 7 500 777200 DEFAULT 5 9 Climb MaxClimb T_00 10 000 777200 DEFAULT 6 1 Takeoff MaxTakeoff T_05 777200 DEFAULT 6 2 Climb MaxTakeoff T_05C 1 000 777200 DEFAULT 6 3 Accelerate MaxClimb T_01 1 136,7 213,4 777200 DEFAULT 6 4 Accelerate MaxClimb T_00 1 275 231,5 777200 DEFAULT 6 5 Climb MaxClimb T_00 3 000 777200 DEFAULT 6 6 Accelerate MaxClimb T_00 1 337,6 2501.7.2015 EN Official Journal of the European Union L 168/405 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777200 DEFAULT 6 7 Climb MaxClimb T_00 5 500 777200 DEFAULT 6 8 Climb MaxClimb T_00 7 500 777200 DEFAULT 6 9 Climb MaxClimb T_00 10 000 777200 DEFAULT 7 1 Takeoff MaxTakeoff T_05 777200 DEFAULT 7 2 Climb MaxTakeoff T_05C 1 000 777200 DEFAULT 7 3 Accelerate MaxClimb T_01 1 032,4 216,2 777200 DEFAULT 7 4 Accelerate MaxClimb T_00 1 147 228,5 777200 DEFAULT 7 5 Accelerate MaxClimb T_00 1 189,4 236,6 777200 DEFAULT 7 6 Climb MaxClimb T_00 3 000 777200 DEFAULT 7 7 Accelerate MaxClimb T_00 1 215,6 250 777200 DEFAULT 7 8 Climb MaxClimb T_00 5 500 777200 DEFAULT 7 9 Climb MaxClimb T_00 7 500 777200 DEFAULT 7 10 Climb MaxClimb T_00 10 000 777200 DEFAULT 8 1 Takeoff MaxTakeoff T_05 777200 DEFAULT 8 2 Climb MaxTakeoff T_05C 1 000 777200 DEFAULT 8 3 Accelerate MaxClimb T_01 931,9 219,4 777200 DEFAULT 8 4 Accelerate MaxClimb T_00H 1 033,1 232,5 777200 DEFAULT 8 5 Accelerate MaxClimb T_00H 1 088,7 242 777200 DEFAULT 8 6 Climb MaxClimb T_00H 3 000 777200 DEFAULT 8 7 Accelerate MaxClimb T_00H 1 101,5 250L 168/406 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777200 DEFAULT 8 8 Climb MaxClimb T_00H 5 500 777200 DEFAULT 8 9 Climb MaxClimb T_00H 7 500 777200 DEFAULT 8 10 Climb MaxClimb T_00H 10 000 777200 DEFAULT 9 1 Takeoff MaxTakeoff T_05 777200 DEFAULT 9 2 Climb MaxTakeoff T_05C 1 000 777200 DEFAULT 9 3 Accelerate MaxClimb T_01 874,9 221,7 777200 DEFAULT 9 4 Accelerate MaxClimb T_00H 969,4 235,4 777200 DEFAULT 9 5 Accelerate MaxClimb T_00H 1 020,2 245,6 777200 DEFAULT 9 6 Climb MaxClimb T_00H 3 000 777200 DEFAULT 9 7 Accelerate MaxClimb T_00H 1 031,1 250 777200 DEFAULT 9 8 Climb MaxClimb T_00H 5 500 777200 DEFAULT 9 9 Climb MaxClimb T_00H 7 500 777200 DEFAULT 9 10 Climb MaxClimb T_00H 10 000 777200 ICAO_A 1 1 Takeoff MaxTakeoff T_05 777200 ICAO_A 1 2 Climb MaxTakeoff T_05C 1 500 777200 ICAO_A 1 3 Climb MaxClimb T_01 3 000 777200 ICAO_A 1 4 Accelerate MaxClimb T_05A 1 504 203,3 777200 ICAO_A 1 5 Accelerate MaxClimb T_01 1 700 213,4 777200 ICAO_A 1 6 Accelerate MaxClimb T_00 1 856,1 250 777200 ICAO_A 1 7 Climb MaxClimb T_00 5 5001.7.2015 EN Official Journal of the European Union L 168/407 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777200 ICAO_A 1 8 Climb MaxClimb T_00 7 500 777200 ICAO_A 1 9 Climb MaxClimb T_00 10 000 777200 ICAO_A 2 1 Takeoff MaxTakeoff T_05 777200 ICAO_A 2 2 Climb MaxTakeoff T_05C 1 500 777200 ICAO_A 2 3 Climb MaxClimb T_01 3 000 777200 ICAO_A 2 4 Accelerate MaxClimb T_05A 1 451,9 204 777200 ICAO_A 2 5 Accelerate MaxClimb T_01 1 633,4 215,4 777200 ICAO_A 2 6 Accelerate MaxClimb T_00 1 789,9 250 777200 ICAO_A 2 7 Climb MaxClimb T_00 5 500 777200 ICAO_A 2 8 Climb MaxClimb T_00 7 500 777200 ICAO_A 2 9 Climb MaxClimb T_00 10 000 777200 ICAO_A 3 1 Takeoff MaxTakeoff T_05 777200 ICAO_A 3 2 Climb MaxTakeoff T_05C 1 500 777200 ICAO_A 3 3 Climb MaxClimb T_01 3 000 777200 ICAO_A 3 4 Accelerate MaxClimb T_05A 1 395,1 204,9 777200 ICAO_A 3 5 Accelerate MaxClimb T_01 1 575 217,3 777200 ICAO_A 3 6 Accelerate MaxClimb T_00 1 719,4 250 777200 ICAO_A 3 7 Climb MaxClimb T_00 5 500 777200 ICAO_A 3 8 Climb MaxClimb T_00 7 500 777200 ICAO_A 3 9 Climb MaxClimb T_00 10 000L 168/408 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777200 ICAO_A 4 1 Takeoff MaxTakeoff T_05 777200 ICAO_A 4 2 Climb MaxTakeoff T_05C 1 500 777200 ICAO_A 4 3 Climb MaxClimb T_01 3 000 777200 ICAO_A 4 4 Accelerate MaxClimb T_05A 1 295,2 206,6 777200 ICAO_A 4 5 Accelerate MaxClimb T_01 1 477,7 221,3 777200 ICAO_A 4 6 Accelerate MaxClimb T_00 1 592,4 250 777200 ICAO_A 4 7 Climb MaxClimb T_00 5 500 777200 ICAO_A 4 8 Climb MaxClimb T_00 7 500 777200 ICAO_A 4 9 Climb MaxClimb T_00 10 000 777200 ICAO_A 5 1 Takeoff MaxTakeoff T_05 777200 ICAO_A 5 2 Climb MaxTakeoff T_05C 1 500 777200 ICAO_A 5 3 Climb MaxClimb T_01 3 000 777200 ICAO_A 5 4 Accelerate MaxClimb T_05A 1 182,6 208,8 777200 ICAO_A 5 5 Accelerate MaxClimb T_01 1 346,3 222,1 777200 ICAO_A 5 6 Accelerate MaxClimb T_00 1 451,1 250 777200 ICAO_A 5 7 Climb MaxClimb T_00 5 500 777200 ICAO_A 5 8 Climb MaxClimb T_00 7 500 777200 ICAO_A 5 9 Climb MaxClimb T_00 10 000 777200 ICAO_A 6 1 Takeoff MaxTakeoff T_05 777200 ICAO_A 6 2 Climb MaxTakeoff T_05C 1 5001.7.2015 EN Official Journal of the European Union L 168/409 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777200 ICAO_A 6 3 Climb MaxClimb T_01 3 000 777200 ICAO_A 6 4 Accelerate MaxClimb T_05 1 075,6 211,4 777200 ICAO_A 6 5 Accelerate MaxClimb T_01 1 217,4 223,4 777200 ICAO_A 6 6 Accelerate MaxClimb T_00 1 316,4 250 777200 ICAO_A 6 7 Climb MaxClimb T_00 5 500 777200 ICAO_A 6 8 Climb MaxClimb T_00 7 500 777200 ICAO_A 6 9 Climb MaxClimb T_00 10 000 777200 ICAO_A 7 1 Takeoff MaxTakeoff T_05 777200 ICAO_A 7 2 Climb MaxTakeoff T_05C 1 500 777200 ICAO_A 7 3 Climb MaxClimb T_01 3 000 777200 ICAO_A 7 4 Accelerate MaxClimb T_05 973,3 214,3 777200 ICAO_A 7 5 Accelerate MaxClimb T_01 1 104,3 227,2 777200 ICAO_A 7 6 Accelerate MaxClimb T_00 1 188,2 250 777200 ICAO_A 7 7 Climb MaxClimb T_00 5 500 777200 ICAO_A 7 8 Climb MaxClimb T_00 7 500 777200 ICAO_A 7 9 Climb MaxClimb T_00 10 000 777200 ICAO_A 8 1 Takeoff MaxTakeoff T_05 777200 ICAO_A 8 2 Climb MaxTakeoff T_05CH 1 500 777200 ICAO_A 8 3 Climb MaxClimb T_01 3 000 777200 ICAO_A 8 4 Accelerate MaxClimb T_05 877,9 217,6L 168/410 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777200 ICAO_A 8 5 Accelerate MaxClimb T_01 997,4 231,4 777200 ICAO_A 8 6 Accelerate MaxClimb T_00H 1 071,6 250 777200 ICAO_A 8 7 Climb MaxClimb T_00H 5 500 777200 ICAO_A 8 8 Climb MaxClimb T_00H 7 500 777200 ICAO_A 8 9 Climb MaxClimb T_00H 10 000 777200 ICAO_A 9 1 Takeoff MaxTakeoff T_05 777200 ICAO_A 9 2 Climb MaxTakeoff T_05CH 1 500 777200 ICAO_A 9 3 Climb MaxClimb T_05 3 000 777200 ICAO_A 9 4 Accelerate MaxClimb T_05 820,9 220 777200 ICAO_A 9 5 Accelerate MaxClimb T_01 930,3 234,3 777200 ICAO_A 9 6 Accelerate MaxClimb T_00H 1 000 250 777200 ICAO_A 9 7 Climb MaxClimb T_00H 5 500 777200 ICAO_A 9 8 Climb MaxClimb T_00 7 500 777200 ICAO_A 9 9 Climb MaxClimb T_00 10 000 777200 ICAO_B 1 1 Takeoff MaxTakeoff T_05 777200 ICAO_B 1 2 Climb MaxTakeoff T_05C 1 089 777200 ICAO_B 1 3 Accelerate MaxTakeoff T_05A 2 183,5 193,8 777200 ICAO_B 1 4 Accelerate MaxTakeoff T_01 1 783,1 213,6 777200 ICAO_B 1 5 Climb MaxClimb T_00 3 000 777200 ICAO_B 1 6 Accelerate MaxClimb T_00 1 857,4 2501.7.2015 EN Official Journal of the European Union L 168/411 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777200 ICAO_B 1 7 Climb MaxClimb T_00 5 500 777200 ICAO_B 1 8 Climb MaxClimb T_00 7 500 777200 ICAO_B 1 9 Climb MaxClimb T_00 10 000 777200 ICAO_B 2 1 Takeoff MaxTakeoff T_05 777200 ICAO_B 2 2 Climb MaxTakeoff T_05C 1 057 777200 ICAO_B 2 3 Accelerate MaxTakeoff T_05A 2 121,3 195,8 777200 ICAO_B 2 4 Accelerate MaxTakeoff T_01 1 722,3 215,5 777200 ICAO_B 2 5 Climb MaxClimb T_00 3 000 777200 ICAO_B 2 6 Accelerate MaxClimb T_00 1 789,8 250 777200 ICAO_B 2 7 Climb MaxClimb T_00 5 500 777200 ICAO_B 2 8 Climb MaxClimb T_00 7 500 777200 ICAO_B 2 9 Climb MaxClimb T_00 10 000 777200 ICAO_B 3 1 Takeoff MaxTakeoff T_05 777200 ICAO_B 3 2 Climb MaxTakeoff T_05C 1 022 777200 ICAO_B 3 3 Accelerate MaxTakeoff T_05A 2 059,4 197,9 777200 ICAO_B 3 4 Accelerate MaxTakeoff T_01 1 664,2 217,6 777200 ICAO_B 3 5 Climb MaxClimb T_00 3 000 777200 ICAO_B 3 6 Accelerate MaxClimb T_00 1 723 250 777200 ICAO_B 3 7 Climb MaxClimb T_00 5 500 777200 ICAO_B 3 8 Climb MaxClimb T_00 7 500L 168/412 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777200 ICAO_B 3 9 Climb MaxClimb T_00 10 000 777200 ICAO_B 4 1 Takeoff MaxTakeoff T_05 777200 ICAO_B 4 2 Climb MaxTakeoff T_05C 1 000 777200 ICAO_B 4 3 Accelerate MaxTakeoff T_05A 1 940,1 201,8 777200 ICAO_B 4 4 Accelerate MaxTakeoff T_01 1 555,7 221,6 777200 ICAO_B 4 5 Climb MaxClimb T_00 3 000 777200 ICAO_B 4 6 Accelerate MaxClimb T_00 1 602,1 250 777200 ICAO_B 4 7 Climb MaxClimb T_00 5 500 777200 ICAO_B 4 8 Climb MaxClimb T_00 7 500 777200 ICAO_B 4 9 Climb MaxClimb T_00 10 000 777200 ICAO_B 5 1 Takeoff MaxTakeoff T_05 777200 ICAO_B 5 2 Climb MaxTakeoff T_05C 1 000 777200 ICAO_B 5 3 Accelerate MaxTakeoff T_05A 1 809,2 206,7 777200 ICAO_B 5 4 Accelerate MaxTakeoff T_01 1 431,6 226,5 777200 ICAO_B 5 5 Climb MaxClimb T_00 3 000 777200 ICAO_B 5 6 Accelerate MaxClimb T_00 1 466,4 250 777200 ICAO_B 5 7 Climb MaxClimb T_00 5 500 777200 ICAO_B 5 8 Climb MaxClimb T_00 7 500 777200 ICAO_B 5 9 Climb MaxClimb T_00 10 000 777200 ICAO_B 6 1 Takeoff MaxTakeoff T_051.7.2015 EN Official Journal of the European Union L 168/413 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777200 ICAO_B 6 2 Climb MaxTakeoff T_05C 1 000 777200 ICAO_B 6 3 Accelerate MaxTakeoff T_05A 1 683,9 211,6 777200 ICAO_B 6 4 Accelerate MaxTakeoff T_01 1 315,7 231,4 777200 ICAO_B 6 5 Climb MaxClimb T_00 3 000 777200 ICAO_B 6 6 Accelerate MaxClimb T_00 1 337,6 250 777200 ICAO_B 6 7 Climb MaxClimb T_00 5 500 777200 ICAO_B 6 8 Climb MaxClimb T_00 7 500 777200 ICAO_B 6 9 Climb MaxClimb T_00 10 000 777200 ICAO_B 7 1 Takeoff MaxTakeoff T_05 777200 ICAO_B 7 2 Climb MaxTakeoff T_05C 1 000 777200 ICAO_B 7 3 Accelerate MaxTakeoff T_05A 1 562,2 216,6 777200 ICAO_B 7 4 Accelerate MaxTakeoff T_01 1 197,4 236,5 777200 ICAO_B 7 5 Climb MaxClimb T_00 3 000 777200 ICAO_B 7 6 Accelerate MaxClimb T_00 1 214,8 250 777200 ICAO_B 7 7 Climb MaxClimb T_00 5 500 777200 ICAO_B 7 8 Climb MaxClimb T_00 7 500 777200 ICAO_B 7 9 Climb MaxClimb T_00 10 000 777200 ICAO_B 8 1 Takeoff MaxTakeoff T_05 777200 ICAO_B 8 2 Climb MaxTakeoff T_05C 1 000 777200 ICAO_B 8 3 Accelerate MaxTakeoff T_05A 1 450,3 222,2L 168/414 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777200 ICAO_B 8 4 Accelerate MaxTakeoff T_01 1 090,6 241,9 777200 ICAO_B 8 5 Climb MaxClimb T_00 3 000 777200 ICAO_B 8 6 Accelerate MaxClimb T_00 1 101,5 250 777200 ICAO_B 8 7 Climb MaxClimb T_00 5 500 777200 ICAO_B 8 8 Climb MaxClimb T_00 7 500 777200 ICAO_B 8 9 Climb MaxClimb T_00 10 000 777200 ICAO_B 9 1 Takeoff MaxTakeoff T_05 777200 ICAO_B 9 2 Climb MaxTakeoff T_05C 1 000 777200 ICAO_B 9 3 Accelerate MaxTakeoff T_05A 1 381,9 225,8 777200 ICAO_B 9 4 Accelerate MaxTakeoff T_01 1 025,7 245,6 777200 ICAO_B 9 5 Climb MaxClimb T_00 3 000 777200 ICAO_B 9 6 Accelerate MaxClimb T_00 1 031,1 250 777200 ICAO_B 9 7 Climb MaxClimb T_00 5 500 777200 ICAO_B 9 8 Climb MaxClimb T_00 7 500 777200 ICAO_B 9 9 Climb MaxClimb T_00 10 000 777300 DEFAULT 1 1 Takeoff MaxTakeoff T_20_U 777300 DEFAULT 1 2 Climb MaxTakeoff T_20_U 1 068 777300 DEFAULT 1 3 Accelerate MaxClimb T_05_U 1 471,6 215,4 777300 DEFAULT 1 4 Climb MaxClimb T_00_U 3 000 777300 DEFAULT 1 5 Accelerate MaxClimb T_00_U 1 779,1 2501.7.2015 EN Official Journal of the European Union L 168/415 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777300 DEFAULT 1 6 Climb MaxClimb T_00_U 5 000 777300 DEFAULT 1 7 Climb MaxClimb T_00_U 7 500 777300 DEFAULT 1 8 Climb MaxClimb T_00_U 10 000 777300 DEFAULT 2 1 Takeoff MaxTakeoff T_20_U 777300 DEFAULT 2 2 Climb MaxTakeoff T_20_U 1 064 777300 DEFAULT 2 3 Accelerate MaxClimb T_05_U 1 418 217,8 777300 DEFAULT 2 4 Climb MaxClimb T_00_U 3 000 777300 DEFAULT 2 5 Accelerate MaxClimb T_00_U 1 713,9 250 777300 DEFAULT 2 6 Climb MaxClimb T_00_U 5 000 777300 DEFAULT 2 7 Climb MaxClimb T_00_U 7 500 777300 DEFAULT 2 8 Climb MaxClimb T_00_U 10 000 777300 DEFAULT 3 1 Takeoff MaxTakeoff T_20_U 777300 DEFAULT 3 2 Climb MaxTakeoff T_20_U 1 062 777300 DEFAULT 3 3 Accelerate MaxClimb T_05_U 1 368 220,3 777300 DEFAULT 3 4 Climb MaxClimb T_00_U 3 000 777300 DEFAULT 3 5 Accelerate MaxClimb T_00_U 1 638,9 250 777300 DEFAULT 3 6 Climb MaxClimb T_00_U 5 000 777300 DEFAULT 3 7 Climb MaxClimb T_00_U 7 500 777300 DEFAULT 3 8 Climb MaxClimb T_00_U 10 000 777300 DEFAULT 4 1 Takeoff MaxTakeoff T_20_UL 168/416 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777300 DEFAULT 4 2 Climb MaxTakeoff T_20_U 1 058 777300 DEFAULT 4 3 Accelerate MaxClimb T_05_U 1 279 224,3 777300 DEFAULT 4 4 Climb MaxClimb T_00_U 3 000 777300 DEFAULT 4 5 Accelerate MaxClimb T_00_U 1 519,4 250 777300 DEFAULT 4 6 Climb MaxClimb T_00_U 5 000 777300 DEFAULT 4 7 Climb MaxClimb T_00_U 7 500 777300 DEFAULT 4 8 Climb MaxClimb T_00_U 10 000 777300 DEFAULT 5 1 Takeoff MaxTakeoff T_20_U 777300 DEFAULT 5 2 Climb MaxTakeoff T_20_U 1 053 777300 DEFAULT 5 3 Accelerate MaxClimb T_05_U 1 179,2 229,4 777300 DEFAULT 5 4 Climb MaxClimb T_00_U 3 000 777300 DEFAULT 5 5 Accelerate MaxClimb T_00_U 1 392,1 250 777300 DEFAULT 5 6 Climb MaxClimb T_00_U 5 000 777300 DEFAULT 5 7 Climb MaxClimb T_00_U 7 500 777300 DEFAULT 5 8 Climb MaxClimb T_00_U 10 000 777300 DEFAULT 6 1 Takeoff MaxTakeoff T_20_U 777300 DEFAULT 6 2 Climb MaxTakeoff T_20_U 1 049 777300 DEFAULT 6 3 Accelerate MaxClimb T_05_U 1 082,8 234,4 777300 DEFAULT 6 4 Climb MaxClimb T_00_U 3 000 777300 DEFAULT 6 5 Accelerate MaxClimb T_00_U 1 260 2501.7.2015 EN Official Journal of the European Union L 168/417 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777300 DEFAULT 6 6 Climb MaxClimb T_00_U 5 000 777300 DEFAULT 6 7 Climb MaxClimb T_00_U 7 500 777300 DEFAULT 6 8 Climb MaxClimb T_00_U 10 000 777300 DEFAULT 7 1 Takeoff MaxTakeoff T_20_U 777300 DEFAULT 7 2 Climb MaxTakeoff T_20_U 1 042 777300 DEFAULT 7 3 Accelerate MaxClimb T_05_U 911,6 243,4 777300 DEFAULT 7 4 Climb MaxClimb T_00_U 3 000 777300 DEFAULT 7 5 Accelerate MaxClimb T_00_U 1 060,3 250 777300 DEFAULT 7 6 Climb MaxClimb T_00_U 5 000 777300 DEFAULT 7 7 Climb MaxClimb T_00_U 7 500 777300 DEFAULT 7 8 Climb MaxClimb T_00_U 10 000 777300 ICAO_A 1 1 Takeoff MaxTakeoff T_20_U 777300 ICAO_A 1 2 Climb MaxTakeoff T_20_U 1 565 777300 ICAO_A 1 3 Climb MaxClimb T_20_U 3 000 777300 ICAO_A 1 4 Accelerate MaxClimb T_05_U 1 420,7 215,2 777300 ICAO_A 1 5 Climb MaxClimb T_00_U 4 117 777300 ICAO_A 1 6 Accelerate MaxClimb T_00_U 1 762,5 250 777300 ICAO_A 1 7 Climb MaxClimb T_00_U 5 000 777300 ICAO_A 1 8 Climb MaxClimb T_00_U 7 500 777300 ICAO_A 1 9 Climb MaxClimb T_00_U 10 000L 168/418 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777300 ICAO_A 2 1 Takeoff MaxTakeoff T_20_U 777300 ICAO_A 2 2 Climb MaxTakeoff T_20_U 1 563 777300 ICAO_A 2 3 Climb MaxClimb T_20_U 3 000 777300 ICAO_A 2 4 Accelerate MaxClimb T_05_U 1 372,5 217,6 777300 ICAO_A 2 5 Climb MaxClimb T_00_U 4 014 777300 ICAO_A 2 6 Accelerate MaxClimb T_00_U 1 691,8 250 777300 ICAO_A 2 7 Climb MaxClimb T_00_U 5 000 777300 ICAO_A 2 8 Climb MaxClimb T_00_U 7 500 777300 ICAO_A 2 9 Climb MaxClimb T_00_U 10 000 777300 ICAO_A 3 1 Takeoff MaxTakeoff T_20_U 777300 ICAO_A 3 2 Climb MaxTakeoff T_20_U 1 561 777300 ICAO_A 3 3 Climb MaxClimb T_20_U 3 000 777300 ICAO_A 3 4 Accelerate MaxClimb T_05_U 1 320,6 220 777300 ICAO_A 3 5 Climb MaxClimb T_00_U 4 041 777300 ICAO_A 3 6 Accelerate MaxClimb T_00_U 1 616 250 777300 ICAO_A 3 7 Climb MaxClimb T_00_U 5 000 777300 ICAO_A 3 8 Climb MaxClimb T_00_U 7 500 777300 ICAO_A 3 9 Climb MaxClimb T_00_U 10 000 777300 ICAO_A 4 1 Takeoff MaxTakeoff T_20_U 777300 ICAO_A 4 2 Climb MaxTakeoff T_20_U 1 5571.7.2015 EN Official Journal of the European Union L 168/419 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777300 ICAO_A 4 3 Climb MaxClimb T_20_U 3 000 777300 ICAO_A 4 4 Accelerate MaxClimb T_00_U 1 320,5 250 777300 ICAO_A 4 5 Climb MaxClimb T_00_U 5 000 777300 ICAO_A 4 6 Climb MaxClimb T_00_U 7 500 777300 ICAO_A 4 7 Climb MaxClimb T_00_U 10 000 777300 ICAO_A 5 1 Takeoff MaxTakeoff T_05_U 777300 ICAO_A 5 2 Climb MaxTakeoff T_20_U 1 553 777300 ICAO_A 5 3 Climb MaxClimb T_20_U 3 000 777300 ICAO_A 5 4 Accelerate MaxClimb T_00_U 1 199,1 250 777300 ICAO_A 5 5 Climb MaxClimb T_00_U 5 000 777300 ICAO_A 5 6 Climb MaxClimb T_00_U 7 500 777300 ICAO_A 5 7 Climb MaxClimb T_00_U 10 000 777300 ICAO_A 6 1 Takeoff MaxTakeoff T_20_U 777300 ICAO_A 6 2 Climb MaxTakeoff T_20_U 1 553 777300 ICAO_A 6 3 Climb MaxClimb T_20_U 3 000 777300 ICAO_A 6 4 Accelerate MaxClimb T_00_U 1 083,7 250 777300 ICAO_A 6 5 Climb MaxClimb T_00_U 5 000 777300 ICAO_A 6 6 Climb MaxClimb T_00_U 7 500 777300 ICAO_A 6 7 Climb MaxClimb T_00_U 10 000 777300 ICAO_A 7 1 Takeoff MaxTakeoff T_20_UL 168/420 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777300 ICAO_A 7 2 Climb MaxTakeoff T_20_U 1 553 777300 ICAO_A 7 3 Climb MaxClimb T_20_U 3 000 777300 ICAO_A 7 4 Accelerate MaxClimb T_00_U 889 250 777300 ICAO_A 7 5 Climb MaxClimb T_00_U 5 000 777300 ICAO_A 7 6 Climb MaxClimb T_00_U 7 500 777300 ICAO_A 7 7 Climb MaxClimb T_00_U 10 000 777300 ICAO_B 1 1 Takeoff MaxTakeoff T_20_U 777300 ICAO_B 1 2 Climb MaxTakeoff T_20_U 1 000 777300 ICAO_B 1 3 Accelerate MaxTakeoff T_05_U 2 149,6 215,4 777300 ICAO_B 1 4 Climb MaxTakeoff T_00_U 3 416 777300 ICAO_B 1 5 Accelerate MaxClimb T_00_U 1 800 250 777300 ICAO_B 1 6 Climb MaxClimb T_00_U 5 000 777300 ICAO_B 1 7 Climb MaxClimb T_00_U 7 500 777300 ICAO_B 1 8 Climb MaxClimb T_00_U 10 000 777300 ICAO_B 2 1 Takeoff MaxTakeoff T_20_U 777300 ICAO_B 2 2 Climb MaxTakeoff T_20_U 1 000 777300 ICAO_B 2 3 Accelerate MaxTakeoff T_05_U 2 086,3 217,9 777300 ICAO_B 2 4 Climb MaxTakeoff T_00_U 3 205 777300 ICAO_B 2 5 Accelerate MaxClimb T_00_U 1 772,6 250 777300 ICAO_B 2 6 Climb MaxClimb T_00_U 5 0001.7.2015 EN Official Journal of the European Union L 168/421 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777300 ICAO_B 2 7 Climb MaxClimb T_00_U 7 500 777300 ICAO_B 2 8 Climb MaxClimb T_00_U 10 000 777300 ICAO_B 3 1 Takeoff MaxTakeoff T_20_U 777300 ICAO_B 3 2 Climb MaxTakeoff T_20_U 1 000 777300 ICAO_B 3 3 Accelerate MaxTakeoff T_05_U 2 020,6 220,3 777300 ICAO_B 3 4 Climb MaxTakeoff T_00_U 3 076 777300 ICAO_B 3 5 Accelerate MaxClimb T_00_U 1 708,6 250 777300 ICAO_B 3 6 Climb MaxClimb T_00_U 5 000 777300 ICAO_B 3 7 Climb MaxClimb T_00_U 7 500 777300 ICAO_B 3 8 Climb MaxClimb T_00_U 10 000 777300 ICAO_B 4 1 Takeoff MaxTakeoff T_20_U 777300 ICAO_B 4 2 Climb MaxTakeoff T_20_U 1 000 777300 ICAO_B 4 3 Accelerate MaxTakeoff T_05_U 1 895,3 226,3 777300 ICAO_B 4 4 Climb MaxTakeoff T_00_U 2 894 777300 ICAO_B 4 5 Climb MaxClimb T_00_U 3 000 777300 ICAO_B 4 6 Accelerate MaxClimb T_00_U 1 525,8 250 777300 ICAO_B 4 7 Climb MaxClimb T_00_U 5 000 777300 ICAO_B 4 8 Climb MaxClimb T_00_U 7 500 777300 ICAO_B 4 9 Climb MaxClimb T_00_U 10 000 777300 ICAO_B 5 1 Takeoff MaxTakeoff T_20_UL 168/422 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777300 ICAO_B 5 2 Climb MaxTakeoff T_20_U 1 000 777300 ICAO_B 5 3 Accelerate MaxTakeoff T_05_U 1 768,6 229,4 777300 ICAO_B 5 4 Climb MaxTakeoff T_00_U 2 679 777300 ICAO_B 5 5 Climb MaxClimb T_00_U 3 000 777300 ICAO_B 5 6 Accelerate MaxClimb T_00_U 1 387,7 250 777300 ICAO_B 5 7 Climb MaxClimb T_00_U 5 000 777300 ICAO_B 5 8 Climb MaxClimb T_00_U 7 500 777300 ICAO_B 5 9 Climb MaxClimb T_00_U 10 000 777300 ICAO_B 6 1 Takeoff MaxTakeoff T_20_U 777300 ICAO_B 6 2 Climb MaxTakeoff T_20_U 1 000 777300 ICAO_B 6 3 Accelerate MaxTakeoff T_05_U 1 639,4 235,5 777300 ICAO_B 6 4 Climb MaxTakeoff T_00_U 2 402 777300 ICAO_B 6 5 Climb MaxClimb T_00_U 3 000 777300 ICAO_B 6 6 Accelerate MaxClimb T_00_U 1 271,6 250 777300 ICAO_B 6 7 Climb MaxClimb T_00_U 5 000 777300 ICAO_B 6 8 Climb MaxClimb T_00_U 7 500 777300 ICAO_B 6 9 Climb MaxClimb T_00_U 10 000 777300 ICAO_B 7 1 Takeoff MaxTakeoff T_20_U 777300 ICAO_B 7 2 Climb MaxTakeoff T_20_U 1 000 777300 ICAO_B 7 3 Accelerate MaxTakeoff T_05_U 1 491 244,41.7.2015 EN Official Journal of the European Union L 168/423 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 777300 ICAO_B 7 4 Climb MaxTakeoff T_00_U 2 216 777300 ICAO_B 7 5 Climb MaxClimb T_00_U 3 000 777300 ICAO_B 7 6 Accelerate MaxClimb T_00_U 1 271,6 250 777300 ICAO_B 7 7 Climb MaxClimb T_00_U 5 000 777300 ICAO_B 7 8 Climb MaxClimb T_00_U 7 500 777300 ICAO_B 7 9 Climb MaxClimb T_00_U 10 000 7773ER DEFAULT 1 1 Takeoff MaxTakeoff FLAP_5 7773ER DEFAULT 1 2 Climb MaxTakeoff FLAP_5 1 434 7773ER DEFAULT 1 3 Accelerate_ MaxClimb FLAP_5 200 55 Percent 7773ER DEFAULT 1 4 Accelerate_ MaxClimb FLAP_1 223 50 Percent 7773ER DEFAULT 1 5 Climb MaxClimb FLAP_0 3 000 7773ER DEFAULT 1 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER DEFAULT 1 7 Climb MaxClimb FLAP_0 10 000 7773ER DEFAULT 2 1 Takeoff MaxTakeoff FLAP_5 7773ER DEFAULT 2 2 Climb MaxTakeoff FLAP_5 1 434 7773ER DEFAULT 2 3 Accelerate_ MaxClimb FLAP_5 200 55 Percent 7773ER DEFAULT 2 4 Accelerate_ MaxClimb FLAP_1 225 50 Percent 7773ER DEFAULT 2 5 Climb MaxClimb FLAP_0 3 000 7773ER DEFAULT 2 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER DEFAULT 2 7 Climb MaxClimb FLAP_0 10 000L 168/424 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7773ER DEFAULT 3 1 Takeoff MaxTakeoff FLAP_5 7773ER DEFAULT 3 2 Climb MaxTakeoff FLAP_5 1 355 7773ER DEFAULT 3 3 Accelerate_ MaxClimb FLAP_5 204 55 Percent 7773ER DEFAULT 3 4 Accelerate_ MaxClimb FLAP_1 228 50 Percent 7773ER DEFAULT 3 5 Climb MaxClimb FLAP_0 3 000 7773ER DEFAULT 3 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER DEFAULT 3 7 Climb MaxClimb FLAP_0 10 000 7773ER DEFAULT 4 1 Takeoff MaxTakeoff FLAP_5 7773ER DEFAULT 4 2 Climb MaxTakeoff FLAP_5 1 289 7773ER DEFAULT 4 3 Accelerate_ MaxClimb FLAP_5 205 55 Percent 7773ER DEFAULT 4 4 Accelerate_ MaxClimb FLAP_1 230 50 Percent 7773ER DEFAULT 4 5 Climb MaxClimb FLAP_0 3 000 7773ER DEFAULT 4 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER DEFAULT 4 7 Climb MaxClimb FLAP_0 10 000 7773ER DEFAULT 5 1 Takeoff MaxTakeoff FLAP_5 7773ER DEFAULT 5 2 Climb MaxTakeoff FLAP_5 1 214 7773ER DEFAULT 5 3 Accelerate_ MaxClimb FLAP_5 210 55 Percent 7773ER DEFAULT 5 4 Accelerate_ MaxClimb FLAP_1 235 50 Percent 7773ER DEFAULT 5 5 Climb MaxClimb FLAP_0 3 000 7773ER DEFAULT 5 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent1.7.2015 EN Official Journal of the European Union L 168/425 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7773ER DEFAULT 5 7 Climb MaxClimb FLAP_0 10 000 7773ER DEFAULT 6 1 Takeoff MaxTakeoff FLAP_5 7773ER DEFAULT 6 2 Climb MaxTakeoff FLAP_5 1 142 7773ER DEFAULT 6 3 Accelerate_ MaxClimb FLAP_5 215 55 Percent 7773ER DEFAULT 6 4 Accelerate_ MaxClimb FLAP_1 240 50 Percent 7773ER DEFAULT 6 5 Climb MaxClimb FLAP_0 3 000 7773ER DEFAULT 6 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER DEFAULT 6 7 Climb MaxClimb FLAP_0 10 000 7773ER DEFAULT 7 1 Takeoff MaxTakeoff FLAP_5 7773ER DEFAULT 7 2 Climb MaxTakeoff FLAP_5 1 067 7773ER DEFAULT 7 3 Accelerate_ MaxClimb FLAP_5 222 55 Percent 7773ER DEFAULT 7 4 Accelerate_ MaxClimb FLAP_1 248 50 Percent 7773ER DEFAULT 7 5 Climb MaxClimb FLAP_0 3 000 7773ER DEFAULT 7 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER DEFAULT 7 7 Climb MaxClimb FLAP_0 10 000 7773ER DEFAULT 8 1 Takeoff MaxTakeoff FLAP_5 7773ER DEFAULT 8 2 Climb MaxTakeoff FLAP_5 1 000 7773ER DEFAULT 8 3 Accelerate_ MaxClimb FLAP_5 222 55 Percent 7773ER DEFAULT 8 4 Accelerate_ MaxClimb FLAP_1 255 50 Percent 7773ER DEFAULT 8 5 Climb MaxClimb FLAP_0 3 000L 168/426 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7773ER DEFAULT 8 6 Accelerate_ MaxClimb FLAP_0 256 50 Percent 7773ER DEFAULT 8 7 Climb MaxClimb FLAP_0 10 000 7773ER DEFAULT 9 1 Takeoff MaxTakeoff FLAP_5 7773ER DEFAULT 9 2 Climb MaxTakeoff FLAP_5 1 000 7773ER DEFAULT 9 3 Accelerate_ MaxClimb FLAP_5 226 55 Percent 7773ER DEFAULT 9 4 Accelerate_ MaxClimb FLAP_1 261 50 Percent 7773ER DEFAULT 9 5 Climb MaxClimb FLAP_0 3 000 7773ER DEFAULT 9 6 Accelerate_ MaxClimb FLAP_0 261,1 50 Percent 7773ER DEFAULT 9 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_A 1 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_A 1 2 Climb MaxTakeoff FLAP_5 1 500 7773ER ICAO_A 1 3 Climb MaxClimb FLAP_5 3 000 7773ER ICAO_A 1 4 Accelerate_ MaxClimb FLAP_5 210 55 Percent 7773ER ICAO_A 1 5 Accelerate_ MaxClimb FLAP_1 220 55 Percent 7773ER ICAO_A 1 6 Climb MaxClimb FLAP_1 4 400 7773ER ICAO_A 1 7 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER ICAO_A 1 8 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_A 2 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_A 2 2 Climb MaxTakeoff FLAP_5 1 500 7773ER ICAO_A 2 3 Climb MaxClimb FLAP_5 3 0001.7.2015 EN Official Journal of the European Union L 168/427 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7773ER ICAO_A 2 4 Accelerate_ MaxClimb FLAP_5 220 55 Percent 7773ER ICAO_A 2 5 Accelerate_ MaxClimb FLAP_1 230 55 Percent 7773ER ICAO_A 2 6 Climb MaxClimb FLAP_1 4 300 7773ER ICAO_A 2 7 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER ICAO_A 2 8 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_A 3 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_A 3 2 Climb MaxTakeoff FLAP_5 1 500 7773ER ICAO_A 3 3 Climb MaxClimb FLAP_5 3 000 7773ER ICAO_A 3 4 Accelerate_ MaxClimb FLAP_5 220 55 Percent 7773ER ICAO_A 3 5 Accelerate_ MaxClimb FLAP_1 230 55 Percent 7773ER ICAO_A 3 6 Climb MaxClimb FLAP_1 4 200 7773ER ICAO_A 3 7 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER ICAO_A 3 8 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_A 4 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_A 4 2 Climb MaxTakeoff FLAP_5 1 500 7773ER ICAO_A 4 3 Climb MaxClimb FLAP_5 3 000 7773ER ICAO_A 4 4 Accelerate_ MaxClimb FLAP_5 220 55 Percent 7773ER ICAO_A 4 5 Accelerate_ MaxClimb FLAP_1 230 55 Percent 7773ER ICAO_A 4 6 Climb MaxClimb FLAP_1 4 100 7773ER ICAO_A 4 7 Accelerate_ MaxClimb FLAP_0 250 50 PercentL 168/428 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7773ER ICAO_A 4 8 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_A 5 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_A 5 2 Climb MaxTakeoff FLAP_5 1 500 7773ER ICAO_A 5 3 Climb MaxClimb FLAP_5 3 000 7773ER ICAO_A 5 4 Accelerate_ MaxClimb FLAP_5 220 55 Percent 7773ER ICAO_A 5 5 Accelerate_ MaxClimb FLAP_1 230 55 Percent 7773ER ICAO_A 5 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER ICAO_A 5 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_A 6 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_A 6 2 Climb MaxTakeoff FLAP_5 1 500 7773ER ICAO_A 6 3 Climb MaxClimb FLAP_5 3 000 7773ER ICAO_A 6 4 Accelerate_ MaxClimb FLAP_5 220 55 Percent 7773ER ICAO_A 6 5 Accelerate_ MaxClimb FLAP_1 230 55 Percent 7773ER ICAO_A 6 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER ICAO_A 6 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_A 7 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_A 7 2 Climb MaxTakeoff FLAP_5 1 500 7773ER ICAO_A 7 3 Climb MaxClimb FLAP_5 3 000 7773ER ICAO_A 7 4 Accelerate_ MaxClimb FLAP_5 220 55 Percent 7773ER ICAO_A 7 5 Accelerate_ MaxClimb FLAP_1 230 55 Percent1.7.2015 EN Official Journal of the European Union L 168/429 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7773ER ICAO_A 7 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER ICAO_A 7 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_A 8 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_A 8 2 Climb MaxTakeoff FLAP_5 1 500 7773ER ICAO_A 8 3 Climb MaxClimb FLAP_5 3 000 7773ER ICAO_A 8 4 Accelerate_ MaxClimb FLAP_5 220 55 Percent 7773ER ICAO_A 8 5 Accelerate_ MaxClimb FLAP_1 230 55 Percent 7773ER ICAO_A 8 6 Accelerate_ MaxClimb FLAP_0 255 50 Percent 7773ER ICAO_A 8 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_A 9 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_A 9 2 Climb MaxTakeoff FLAP_5 1 500 7773ER ICAO_A 9 3 Climb MaxClimb FLAP_5 3 000 7773ER ICAO_A 9 4 Accelerate_ MaxClimb FLAP_5 230 55 Percent 7773ER ICAO_A 9 5 Accelerate_ MaxClimb FLAP_1 240 55 Percent 7773ER ICAO_A 9 6 Accelerate_ MaxClimb FLAP_0 260 50 Percent 7773ER ICAO_A 9 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_B 1 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_B 1 2 Climb MaxTakeoff FLAP_5 1 434 7773ER ICAO_B 1 3 Accelerate_ MaxTakeoff FLAP_5 223 55 Percent 7773ER ICAO_B 1 4 Climb MaxTakeoff FLAP_1 3 564L 168/430 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7773ER ICAO_B 1 5 Accelerate_ MaxClimb FLAP_0 240 50 Percent 7773ER ICAO_B 1 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER ICAO_B 1 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_B 2 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_B 2 2 Climb MaxTakeoff FLAP_5 1 396 7773ER ICAO_B 2 3 Accelerate_ MaxTakeoff FLAP_5 225 55 Percent 7773ER ICAO_B 2 4 Climb MaxTakeoff FLAP_1 3 442 7773ER ICAO_B 2 5 Accelerate_ MaxClimb FLAP_0 240 50 Percent 7773ER ICAO_B 2 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER ICAO_B 2 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_B 3 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_B 3 2 Climb MaxTakeoff FLAP_5 1 355 7773ER ICAO_B 3 3 Accelerate_ MaxTakeoff FLAP_5 228 55 Percent 7773ER ICAO_B 3 4 Climb MaxTakeoff FLAP_1 3 314 7773ER ICAO_B 3 5 Accelerate_ MaxClimb FLAP_0 240 50 Percent 7773ER ICAO_B 3 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER ICAO_B 3 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_B 4 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_B 4 2 Climb MaxTakeoff FLAP_5 1 289 7773ER ICAO_B 4 3 Accelerate_ MaxTakeoff FLAP_5 231 55 Percent1.7.2015 EN Official Journal of the European Union L 168/431 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7773ER ICAO_B 4 4 Climb MaxTakeoff FLAP_1 3 104 7773ER ICAO_B 4 5 Accelerate_ MaxClimb FLAP_0 240 50 Percent 7773ER ICAO_B 4 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER ICAO_B 4 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_B 5 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_B 5 2 Climb MaxTakeoff FLAP_5 1 214 7773ER ICAO_B 5 3 Accelerate_ MaxTakeoff FLAP_5 236 55 Percent 7773ER ICAO_B 5 4 Climb MaxTakeoff FLAP_1 3 000 7773ER ICAO_B 5 5 Accelerate_ MaxClimb FLAP_0 245 50 Percent 7773ER ICAO_B 5 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER ICAO_B 5 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_B 6 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_B 6 2 Climb MaxTakeoff FLAP_5 1 138 7773ER ICAO_B 6 3 Accelerate_ MaxTakeoff FLAP_5 241 55 Percent 7773ER ICAO_B 6 4 Climb MaxTakeoff FLAP_1 3 000 7773ER ICAO_B 6 5 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7773ER ICAO_B 6 6 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_B 7 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_B 7 2 Climb MaxTakeoff FLAP_5 1 067 7773ER ICAO_B 7 3 Accelerate_ MaxTakeoff FLAP_5 249 55 PercentL 168/432 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7773ER ICAO_B 7 4 Climb MaxTakeoff FLAP_1 2 451 7773ER ICAO_B 7 5 Accelerate_ MaxClimb FLAP_1 250 55 Percent 7773ER ICAO_B 7 6 Climb MaxClimb FLAP_0 3 000 7773ER ICAO_B 7 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_B 8 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_B 8 2 Climb MaxTakeoff FLAP_5 1 000 7773ER ICAO_B 8 3 Accelerate_ MaxTakeoff FLAP_5 257 55 Percent 7773ER ICAO_B 8 4 Climb MaxTakeoff FLAP_1 2 280 7773ER ICAO_B 8 5 Accelerate_ MaxClimb FLAP_1 257 55 Percent 7773ER ICAO_B 8 6 Climb MaxClimb FLAP_0 3 000 7773ER ICAO_B 8 7 Climb MaxClimb FLAP_0 10 000 7773ER ICAO_B 9 1 Takeoff MaxTakeoff FLAP_5 7773ER ICAO_B 9 2 Climb MaxTakeoff FLAP_5 1 000 7773ER ICAO_B 9 3 Accelerate_ MaxTakeoff FLAP_5 261 55 Percent 7773ER ICAO_B 9 4 Climb MaxTakeoff FLAP_1 2 180 7773ER ICAO_B 9 5 Accelerate_ MaxClimb FLAP_1 262 55 Percent 7773ER ICAO_B 9 6 Climb MaxClimb FLAP_0 3 000 7773ER ICAO_B 9 7 Climb MaxClimb FLAP_0 10 000 7878R DEFAULT 1 1 Takeoff MaxTakeoff FLAP_5 7878R DEFAULT 1 2 Climb MaxTakeoff FLAP_5 1 0001.7.2015 EN Official Journal of the European Union L 168/433 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7878R DEFAULT 1 3 Accelerate_ MaxClimb FLAP_5 214 55 Percent 7878R DEFAULT 1 4 Accelerate_ MaxClimb FLAP_1 225 55 Percent 7878R DEFAULT 1 5 Climb MaxClimb FLAP_0 3 000 7878R DEFAULT 1 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R DEFAULT 1 7 Climb MaxClimb FLAP_0 10 000 7878R DEFAULT 2 1 Takeoff MaxTakeoff FLAP_5 7878R DEFAULT 2 2 Climb MaxTakeoff FLAP_5 1 000 7878R DEFAULT 2 3 Accelerate_ MaxClimb FLAP_5 214 55 Percent 7878R DEFAULT 2 4 Accelerate_ MaxClimb FLAP_1 222 55 Percent 7878R DEFAULT 2 5 Climb MaxClimb FLAP_0 3 000 7878R DEFAULT 2 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R DEFAULT 2 7 Climb MaxClimb FLAP_0 10 000 7878R DEFAULT 3 1 Takeoff MaxTakeoff FLAP_5 7878R DEFAULT 3 2 Climb MaxTakeoff FLAP_5 1 000 7878R DEFAULT 3 3 Accelerate_ MaxClimb FLAP_5 215 55 Percent 7878R DEFAULT 3 4 Accelerate_ MaxClimb FLAP_1 230 55 Percent 7878R DEFAULT 3 5 Climb MaxClimb FLAP_0 3 000 7878R DEFAULT 3 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R DEFAULT 3 7 Climb MaxClimb FLAP_0 10 000 7878R DEFAULT 4 1 Takeoff MaxTakeoff FLAP_5L 168/434 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7878R DEFAULT 4 2 Climb MaxTakeoff FLAP_5 1 000 7878R DEFAULT 4 3 Accelerate_ MaxClimb FLAP_5 215 55 Percent 7878R DEFAULT 4 4 Accelerate_ MaxClimb FLAP_1 228 55 Percent 7878R DEFAULT 4 5 Climb MaxClimb FLAP_0 3 000 7878R DEFAULT 4 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R DEFAULT 4 7 Climb MaxClimb FLAP_0 10 000 7878R DEFAULT 5 1 Takeoff MaxTakeoff FLAP_5 7878R DEFAULT 5 2 Climb MaxTakeoff FLAP_5 1 000 7878R DEFAULT 5 3 Accelerate_ MaxClimb FLAP_5 218 55 Percent 7878R DEFAULT 5 4 Accelerate_ MaxClimb FLAP_1 235 55 Percent 7878R DEFAULT 5 5 Climb MaxClimb FLAP_0 3 000 7878R DEFAULT 5 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R DEFAULT 5 7 Climb MaxClimb FLAP_0 10 000 7878R DEFAULT 6 1 Takeoff MaxTakeoff FLAP_5 7878R DEFAULT 6 2 Climb MaxTakeoff FLAP_5 1 000 7878R DEFAULT 6 3 Accelerate_ MaxClimb FLAP_5 220 55 Percent 7878R DEFAULT 6 4 Accelerate_ MaxClimb FLAP_1 238 55 Percent 7878R DEFAULT 6 5 Climb MaxClimb FLAP_0 3 000 7878R DEFAULT 6 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R DEFAULT 6 7 Climb MaxClimb FLAP_0 10 0001.7.2015 EN Official Journal of the European Union L 168/435 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7878R DEFAULT 7 1 Takeoff MaxTakeoff FLAP_5 7878R DEFAULT 7 2 Climb MaxTakeoff FLAP_5 1 000 7878R DEFAULT 7 3 Accelerate_ MaxClimb FLAP_5 224 55 Percent 7878R DEFAULT 7 4 Accelerate_ MaxClimb FLAP_1 243 55 Percent 7878R DEFAULT 7 5 Climb MaxClimb FLAP_0 3 000 7878R DEFAULT 7 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R DEFAULT 7 7 Climb MaxClimb FLAP_0 10 000 7878R DEFAULT 8 1 Takeoff MaxTakeoff FLAP_5 7878R DEFAULT 8 2 Climb MaxTakeoff FLAP_5 1 000 7878R DEFAULT 8 3 Accelerate_ MaxClimb FLAP_5 226 55 Percent 7878R DEFAULT 8 4 Accelerate_ MaxClimb FLAP_1 246 55 Percent 7878R DEFAULT 8 5 Climb MaxClimb FLAP_0 3 000 7878R DEFAULT 8 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R DEFAULT 8 7 Climb MaxClimb FLAP_0 10 000 7878R DEFAULT 9 1 Takeoff MaxTakeoff FLAP_5 7878R DEFAULT 9 2 Climb MaxTakeoff FLAP_5 1 000 7878R DEFAULT 9 3 Accelerate_ MaxClimb FLAP_5 230 55 Percent 7878R DEFAULT 9 4 Accelerate_ MaxClimb FLAP_1 245 55 Percent 7878R DEFAULT 9 5 Climb MaxClimb FLAP_0 3 000 7878R DEFAULT 9 6 Accelerate_ MaxClimb FLAP_0 250 50 PercentL 168/436 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7878R DEFAULT 9 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_A 1 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_A 1 2 Climb MaxTakeoff FLAP_5 1 500 7878R ICAO_A 1 3 Climb MaxClimb FLAP_5 3 000 7878R ICAO_A 1 4 Accelerate_ MaxClimb FLAP_5 220 55 Percent 7878R ICAO_A 1 5 Climb MaxClimb FLAP_1 4 500 7878R ICAO_A 1 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_A 1 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_A 2 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_A 2 2 Climb MaxTakeoff FLAP_5 1 500 7878R ICAO_A 2 3 Climb MaxClimb FLAP_5 3 000 7878R ICAO_A 2 4 Accelerate_ MaxClimb FLAP_5 220 55 Percent 7878R ICAO_A 2 5 Climb MaxClimb FLAP_1 4 400 7878R ICAO_A 2 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_A 2 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_A 3 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_A 3 2 Climb MaxTakeoff FLAP_5 1 500 7878R ICAO_A 3 3 Climb MaxClimb FLAP_5 3 000 7878R ICAO_A 3 4 Accelerate_ MaxClimb FLAP_5 220 55 Percent 7878R ICAO_A 3 5 Climb MaxClimb FLAP_1 4 4001.7.2015 EN Official Journal of the European Union L 168/437 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7878R ICAO_A 3 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_A 3 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_A 4 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_A 4 2 Climb MaxTakeoff FLAP_5 1 500 7878R ICAO_A 4 3 Climb MaxClimb FLAP_5 3 000 7878R ICAO_A 4 4 Accelerate_ MaxClimb FLAP_5 220 55 Percent 7878R ICAO_A 4 5 Climb MaxClimb FLAP_1 4 300 7878R ICAO_A 4 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_A 4 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_A 5 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_A 5 2 Climb MaxTakeoff FLAP_5 1 500 7878R ICAO_A 5 3 Climb MaxClimb FLAP_5 3 000 7878R ICAO_A 5 4 Accelerate_ MaxClimb FLAP_5 224 55 Percent 7878R ICAO_A 5 5 Climb MaxClimb FLAP_1 4 200 7878R ICAO_A 5 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_A 5 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_A 6 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_A 6 2 Climb MaxTakeoff FLAP_5 1 500 7878R ICAO_A 6 3 Climb MaxClimb FLAP_5 3 000 7878R ICAO_A 6 4 Accelerate_ MaxClimb FLAP_5 226 55 PercentL 168/438 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7878R ICAO_A 6 5 Climb MaxClimb FLAP_1 4 100 7878R ICAO_A 6 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_A 6 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_A 7 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_A 7 2 Climb MaxTakeoff FLAP_5 1 500 7878R ICAO_A 7 3 Climb MaxClimb FLAP_5 3 000 7878R ICAO_A 7 4 Accelerate_ MaxClimb FLAP_5 232 55 Percent 7878R ICAO_A 7 5 Climb MaxClimb FLAP_1 4 000 7878R ICAO_A 7 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_A 7 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_A 8 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_A 8 2 Climb MaxTakeoff FLAP_5 1 500 7878R ICAO_A 8 3 Climb MaxClimb FLAP_5 3 000 7878R ICAO_A 8 4 Accelerate_ MaxClimb FLAP_5 232 55 Percent 7878R ICAO_A 8 5 Climb MaxClimb FLAP_1 4 000 7878R ICAO_A 8 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_A 8 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_A 9 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_A 9 2 Climb MaxTakeoff FLAP_5 1 500 7878R ICAO_A 9 3 Climb MaxClimb FLAP_5 3 0001.7.2015 EN Official Journal of the European Union L 168/439 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7878R ICAO_A 9 4 Accelerate_ MaxClimb FLAP_5 235 55 Percent 7878R ICAO_A 9 5 Climb MaxClimb FLAP_1 4 000 7878R ICAO_A 9 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_A 9 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_B 1 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_B 1 2 Climb MaxTakeoff FLAP_5 1 000 7878R ICAO_B 1 3 Accelerate_ MaxTakeoff FLAP_5 220 55 Percent 7878R ICAO_B 1 4 Climb MaxTakeoff FLAP_1 2 700 7878R ICAO_B 1 5 Climb MaxClimb FLAP_0 3 000 7878R ICAO_B 1 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_B 1 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_B 2 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_B 2 2 Climb MaxTakeoff FLAP_5 1 000 7878R ICAO_B 2 3 Accelerate_ MaxTakeoff FLAP_5 220 55 Percent 7878R ICAO_B 2 4 Climb MaxTakeoff FLAP_1 2 700 7878R ICAO_B 2 5 Climb MaxClimb FLAP_0 3 000 7878R ICAO_B 2 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_B 2 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_B 3 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_B 3 2 Climb MaxTakeoff FLAP_5 1 000L 168/440 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7878R ICAO_B 3 3 Accelerate_ MaxTakeoff FLAP_5 220 55 Percent 7878R ICAO_B 3 4 Climb MaxTakeoff FLAP_1 2 700 7878R ICAO_B 3 5 Climb MaxClimb FLAP_0 3 000 7878R ICAO_B 3 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_B 3 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_B 4 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_B 4 2 Climb MaxTakeoff FLAP_5 1 000 7878R ICAO_B 4 3 Accelerate_ MaxTakeoff FLAP_5 225 55 Percent 7878R ICAO_B 4 4 Climb MaxTakeoff FLAP_1 2 600 7878R ICAO_B 4 5 Climb MaxClimb FLAP_0 3 000 7878R ICAO_B 4 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_B 4 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_B 5 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_B 5 2 Climb MaxTakeoff FLAP_5 1 000 7878R ICAO_B 5 3 Accelerate_ MaxTakeoff FLAP_5 230 55 Percent 7878R ICAO_B 5 4 Climb MaxTakeoff FLAP_1 2 500 7878R ICAO_B 5 5 Climb MaxClimb FLAP_0 3 000 7878R ICAO_B 5 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_B 5 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_B 6 1 Takeoff MaxTakeoff FLAP_51.7.2015 EN Official Journal of the European Union L 168/441 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7878R ICAO_B 6 2 Climb MaxTakeoff FLAP_5 1 000 7878R ICAO_B 6 3 Accelerate_ MaxTakeoff FLAP_5 230 55 Percent 7878R ICAO_B 6 4 Climb MaxTakeoff FLAP_1 2 400 7878R ICAO_B 6 5 Climb MaxClimb FLAP_0 3 000 7878R ICAO_B 6 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_B 6 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_B 7 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_B 7 2 Climb MaxTakeoff FLAP_5 1 000 7878R ICAO_B 7 3 Accelerate_ MaxTakeoff FLAP_5 235 55 Percent 7878R ICAO_B 7 4 Climb MaxTakeoff FLAP_1 2 200 7878R ICAO_B 7 5 Climb MaxClimb FLAP_0 3 000 7878R ICAO_B 7 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_B 7 7 Climb MaxClimb FLAP_0 10 000 7878R ICAO_B 8 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_B 8 2 Climb MaxTakeoff FLAP_5 1 000 7878R ICAO_B 8 3 Accelerate_ MaxTakeoff FLAP_5 240 55 Percent 7878R ICAO_B 8 4 Climb MaxTakeoff FLAP_1 2 100 7878R ICAO_B 8 5 Climb MaxClimb FLAP_0 3 000 7878R ICAO_B 8 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_B 8 7 Climb MaxClimb FLAP_0 10 000L 168/442 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) 7878R ICAO_B 9 1 Takeoff MaxTakeoff FLAP_5 7878R ICAO_B 9 2 Climb MaxTakeoff FLAP_5 1 000 7878R ICAO_B 9 3 Accelerate_ MaxTakeoff FLAP_5 245 55 Percent 7878R ICAO_B 9 4 Climb MaxTakeoff FLAP_1 2 100 7878R ICAO_B 9 5 Climb MaxClimb FLAP_0 3 000 7878R ICAO_B 9 6 Accelerate_ MaxClimb FLAP_0 250 50 Percent 7878R ICAO_B 9 7 Climb MaxClimb FLAP_0 10 000 A300-622R DEFAULT 1 1 Takeoff MaxTakeoff 1 500 A300-622R DEFAULT 1 2 Climb MaxTakeoff 1 500 1 000 A300-622R DEFAULT 1 3 Accelerate MaxTakeoff 1 500 1 419,5 185,3 A300-622R DEFAULT 1 4 Climb MaxClimb 0 3 000 A300-622R DEFAULT 1 5 Accelerate MaxClimb 0 1 275 250 A300-622R DEFAULT 1 6 Climb MaxClimb 0 5 500 A300-622R DEFAULT 1 7 Climb MaxClimb 0 7 500 A300-622R DEFAULT 1 8 Climb MaxClimb 0 10 000 A300-622R DEFAULT 2 1 Takeoff MaxTakeoff 1 500 A300-622R DEFAULT 2 2 Climb MaxTakeoff 1 500 1 000 A300-622R DEFAULT 2 3 Accelerate MaxTakeoff 1 500 1 361,3 189,3 A300-622R DEFAULT 2 4 Climb MaxClimb 0 3 000 A300-622R DEFAULT 2 5 Accelerate MaxClimb 0 1 216,8 2501.7.2015 EN Official Journal of the European Union L 168/443 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A300-622R DEFAULT 2 6 Climb MaxClimb 0 5 500 A300-622R DEFAULT 2 7 Climb MaxClimb 0 7 500 A300-622R DEFAULT 2 8 Climb MaxClimb 0 10 000 A300-622R DEFAULT 3 1 Takeoff MaxTakeoff 1 500 A300-622R DEFAULT 3 2 Climb MaxTakeoff 1 500 1 000 A300-622R DEFAULT 3 3 Accelerate MaxTakeoff 1 500 1 303,7 193,2 A300-622R DEFAULT 3 4 Climb MaxClimb 0 3 000 A300-622R DEFAULT 3 5 Accelerate MaxClimb 0 1 159,4 250 A300-622R DEFAULT 3 6 Climb MaxClimb 0 5 500 A300-622R DEFAULT 3 7 Climb MaxClimb 0 7 500 A300-622R DEFAULT 3 8 Climb MaxClimb 0 10 000 A300-622R DEFAULT 4 1 Takeoff MaxTakeoff 1 500 A300-622R DEFAULT 4 2 Climb MaxTakeoff 1 500 1 000 A300-622R DEFAULT 4 3 Accelerate MaxTakeoff 1 500 1 210,4 200,1 A300-622R DEFAULT 4 4 Climb MaxClimb 0 3 000 A300-622R DEFAULT 4 5 Accelerate MaxClimb 0 1 065,5 250 A300-622R DEFAULT 4 6 Climb MaxClimb 0 5 500 A300-622R DEFAULT 4 7 Climb MaxClimb 0 7 500 A300-622R DEFAULT 4 8 Climb MaxClimb 0 10 000 A300-622R DEFAULT 5 1 Takeoff MaxTakeoff 1 500L 168/444 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A300-622R DEFAULT 5 2 Climb MaxTakeoff 1 500 1 000 A300-622R DEFAULT 5 3 Accelerate MaxTakeoff 1 500 1 099,6 209,1 A300-622R DEFAULT 5 4 Climb MaxClimb 0 3 000 A300-622R DEFAULT 5 5 Accelerate MaxClimb 0 953,9 250 A300-622R DEFAULT 5 6 Climb MaxClimb 0 5 500 A300-622R DEFAULT 5 7 Climb MaxClimb 0 7 500 A300-622R DEFAULT 5 8 Climb MaxClimb 0 10 000 A300-622R DEFAULT 6 1 Takeoff MaxTakeoff 1 500 A300-622R DEFAULT 6 2 Climb MaxTakeoff 1 500 1 000 A300-622R DEFAULT 6 3 Accelerate MaxTakeoff 1 500 1 015,3 216,4 A300-622R DEFAULT 6 4 Climb MaxClimb 0 3 000 A300-622R DEFAULT 6 5 Accelerate MaxClimb 0 870,9 250 A300-622R DEFAULT 6 6 Climb MaxClimb 0 5 500 A300-622R DEFAULT 6 7 Climb MaxClimb 0 7 500 A300-622R DEFAULT 6 8 Climb MaxClimb 0 10 000 A300-622R ICAO_A 1 1 Takeoff MaxTakeoff 1 500 A300-622R ICAO_A 1 2 Climb MaxTakeoff 1 500 1 500 A300-622R ICAO_A 1 3 Climb MaxClimb 1 500 3 000 A300-622R ICAO_A 1 4 Accelerate MaxClimb 1 500 979,6 185,2 A300-622R ICAO_A 1 5 Accelerate MaxClimb 0 1 107,6 204,51.7.2015 EN Official Journal of the European Union L 168/445 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A300-622R ICAO_A 1 6 Accelerate MaxClimb 0 1 303,7 250 A300-622R ICAO_A 1 7 Climb MaxClimb 0 5 500 A300-622R ICAO_A 1 8 Climb MaxClimb 0 7 500 A300-622R ICAO_A 1 9 Climb MaxClimb 0 10 000 A300-622R ICAO_A 2 1 Takeoff MaxTakeoff 1 500 A300-622R ICAO_A 2 2 Climb MaxTakeoff 1 500 1 500 A300-622R ICAO_A 2 3 Climb MaxClimb 1 500 3 000 A300-622R ICAO_A 2 4 Accelerate MaxClimb 1 500 935 189,1 A300-622R ICAO_A 2 5 Accelerate MaxClimb 0 1 059,7 207,3 A300-622R ICAO_A 2 6 Accelerate MaxClimb 0 1 241,6 250 A300-622R ICAO_A 2 7 Climb MaxClimb 0 5 500 A300-622R ICAO_A 2 8 Climb MaxClimb 0 7 500 A300-622R ICAO_A 2 9 Climb MaxClimb 0 10 000 A300-622R ICAO_A 3 1 Takeoff MaxTakeoff 1 500 A300-622R ICAO_A 3 2 Climb MaxTakeoff 1 500 1 500 A300-622R ICAO_A 3 3 Climb MaxClimb 1 500 3 000 A300-622R ICAO_A 3 4 Accelerate MaxClimb 1 500 890,5 193,1 A300-622R ICAO_A 3 5 Accelerate MaxClimb 0 1 012,1 210,1 A300-622R ICAO_A 3 6 Accelerate MaxClimb 0 1 180,8 250 A300-622R ICAO_A 3 7 Climb MaxClimb 0 5 500L 168/446 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A300-622R ICAO_A 3 8 Climb MaxClimb 0 7 500 A300-622R ICAO_A 3 9 Climb MaxClimb 0 10 000 A300-622R ICAO_A 4 1 Takeoff MaxTakeoff 1 500 A300-622R ICAO_A 4 2 Climb MaxTakeoff 1 500 1 500 A300-622R ICAO_A 4 3 Climb MaxClimb 1 500 3 000 A300-622R ICAO_A 4 4 Accelerate MaxClimb 1 500 817,4 200 A300-622R ICAO_A 4 5 Accelerate MaxClimb 0 933,4 215,2 A300-622R ICAO_A 4 6 Accelerate MaxClimb 0 1 081,4 250 A300-622R ICAO_A 4 7 Climb MaxClimb 0 5 500 A300-622R ICAO_A 4 8 Climb MaxClimb 0 7 500 A300-622R ICAO_A 4 9 Climb MaxClimb 0 10 000 A300-622R ICAO_A 5 1 Takeoff MaxTakeoff 1 500 A300-622R ICAO_A 5 2 Climb MaxTakeoff 1 500 1 500 A300-622R ICAO_A 5 3 Climb MaxClimb 1 500 3 000 A300-622R ICAO_A 5 4 Accelerate MaxClimb 1 500 729 208,9 A300-622R ICAO_A 5 5 Accelerate MaxClimb 0 839,1 222,1 A300-622R ICAO_A 5 6 Accelerate MaxClimb 0 963,8 250 A300-622R ICAO_A 5 7 Climb MaxClimb 0 5 500 A300-622R ICAO_A 5 8 Climb MaxClimb 0 7 500 A300-622R ICAO_A 5 9 Climb MaxClimb 0 10 0001.7.2015 EN Official Journal of the European Union L 168/447 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A300-622R ICAO_A 6 1 Takeoff MaxTakeoff 1 500 A300-622R ICAO_A 6 2 Climb MaxTakeoff 1 500 1 500 A300-622R ICAO_A 6 3 Climb MaxClimb 1 500 3 000 A300-622R ICAO_A 6 4 Accelerate MaxClimb 1 500 660,6 216,3 A300-622R ICAO_A 6 5 Accelerate MaxClimb 0 765,7 227,9 A300-622R ICAO_A 6 6 Accelerate MaxClimb 0 876,5 250 A300-622R ICAO_A 6 7 Climb MaxClimb 0 5 500 A300-622R ICAO_A 6 8 Climb MaxClimb 0 7 500 A300-622R ICAO_A 6 9 Climb MaxClimb 0 10 000 A300-622R ICAO_B 1 1 Takeoff MaxTakeoff 1 500 A300-622R ICAO_B 1 2 Climb MaxTakeoff 1 500 1 000 A300-622R ICAO_B 1 3 Accelerate MaxTakeoff 1 500 1 419,5 185,3 A300-622R ICAO_B 1 4 Climb MaxClimb 0 3 000 A300-622R ICAO_B 1 5 Accelerate MaxClimb 0 1 275 250 A300-622R ICAO_B 1 6 Climb MaxClimb 0 5 500 A300-622R ICAO_B 1 7 Climb MaxClimb 0 7 500 A300-622R ICAO_B 1 8 Climb MaxClimb 0 10 000 A300-622R ICAO_B 2 1 Takeoff MaxTakeoff 1 500 A300-622R ICAO_B 2 2 Climb MaxTakeoff 1 500 1 000 A300-622R ICAO_B 2 3 Accelerate MaxTakeoff 1 500 1 361,3 189,3L 168/448 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A300-622R ICAO_B 2 4 Climb MaxClimb 0 3 000 A300-622R ICAO_B 2 5 Accelerate MaxClimb 0 1 216,8 250 A300-622R ICAO_B 2 6 Climb MaxClimb 0 5 500 A300-622R ICAO_B 2 7 Climb MaxClimb 0 7 500 A300-622R ICAO_B 2 8 Climb MaxClimb 0 10 000 A300-622R ICAO_B 3 1 Takeoff MaxTakeoff 1 500 A300-622R ICAO_B 3 2 Climb MaxTakeoff 1 500 1 000 A300-622R ICAO_B 3 3 Accelerate MaxTakeoff 1 500 1 303,7 193,2 A300-622R ICAO_B 3 4 Climb MaxClimb 0 3 000 A300-622R ICAO_B 3 5 Accelerate MaxClimb 0 1 159,4 250 A300-622R ICAO_B 3 6 Climb MaxClimb 0 5 500 A300-622R ICAO_B 3 7 Climb MaxClimb 0 7 500 A300-622R ICAO_B 3 8 Climb MaxClimb 0 10 000 A300-622R ICAO_B 4 1 Takeoff MaxTakeoff 1 500 A300-622R ICAO_B 4 2 Climb MaxTakeoff 1 500 1 000 A300-622R ICAO_B 4 3 Accelerate MaxTakeoff 1 500 1 210,4 200,1 A300-622R ICAO_B 4 4 Climb MaxClimb 0 3 000 A300-622R ICAO_B 4 5 Accelerate MaxClimb 0 1 065,5 250 A300-622R ICAO_B 4 6 Climb MaxClimb 0 5 500 A300-622R ICAO_B 4 7 Climb MaxClimb 0 7 5001.7.2015 EN Official Journal of the European Union L 168/449 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A300-622R ICAO_B 4 8 Climb MaxClimb 0 10 000 A300-622R ICAO_B 5 1 Takeoff MaxTakeoff 1 500 A300-622R ICAO_B 5 2 Climb MaxTakeoff 1 500 1 000 A300-622R ICAO_B 5 3 Accelerate MaxTakeoff 1 500 1 099,6 209,1 A300-622R ICAO_B 5 4 Climb MaxClimb 0 3 000 A300-622R ICAO_B 5 5 Accelerate MaxClimb 0 953,9 250 A300-622R ICAO_B 5 6 Climb MaxClimb 0 5 500 A300-622R ICAO_B 5 7 Climb MaxClimb 0 7 500 A300-622R ICAO_B 5 8 Climb MaxClimb 0 10 000 A300-622R ICAO_B 6 1 Takeoff MaxTakeoff 1 500 A300-622R ICAO_B 6 2 Climb MaxTakeoff 1 500 1 000 A300-622R ICAO_B 6 3 Accelerate MaxTakeoff 1 500 1 015,3 216,4 A300-622R ICAO_B 6 4 Climb MaxClimb 0 3 000 A300-622R ICAO_B 6 5 Accelerate MaxClimb 0 870,9 250 A300-622R ICAO_B 6 6 Climb MaxClimb 0 5 500 A300-622R ICAO_B 6 7 Climb MaxClimb 0 7 500 A300-622R ICAO_B 6 8 Climb MaxClimb 0 10 000 A300B4-203 DEFAULT 1 1 Takeoff MaxTakeoff 8 A300B4-203 DEFAULT 1 2 Climb MaxTakeoff 8 1 000 A300B4-203 DEFAULT 1 3 Accelerate MaxTakeoff 8 2 440 169L 168/450 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A300B4-203 DEFAULT 1 4 Accelerate MaxTakeoff 1 1 830 189 A300B4-203 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 209 A300B4-203 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 A300B4-203 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 A300B4-203 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 A300B4-203 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 A300B4-203 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 A300B4-203 DEFAULT 2 1 Takeoff MaxTakeoff 8 A300B4-203 DEFAULT 2 2 Climb MaxTakeoff 8 1 000 A300B4-203 DEFAULT 2 3 Accelerate MaxTakeoff 8 2 268 174 A300B4-203 DEFAULT 2 4 Accelerate MaxTakeoff 1 1 701 194 A300B4-203 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 214 A300B4-203 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 A300B4-203 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 A300B4-203 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 A300B4-203 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 A300B4-203 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 A300B4-203 DEFAULT 3 1 Takeoff MaxTakeoff 8 A300B4-203 DEFAULT 3 2 Climb MaxTakeoff 8 1 000 A300B4-203 DEFAULT 3 3 Accelerate MaxTakeoff 8 2 137 1781.7.2015 EN Official Journal of the European Union L 168/451 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A300B4-203 DEFAULT 3 4 Accelerate MaxTakeoff 1 1 603 198 A300B4-203 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 218 A300B4-203 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 A300B4-203 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 A300B4-203 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 A300B4-203 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 A300B4-203 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 A300B4-203 DEFAULT 4 1 Takeoff MaxTakeoff 8 A300B4-203 DEFAULT 4 2 Climb MaxTakeoff 8 1 000 A300B4-203 DEFAULT 4 3 Accelerate MaxTakeoff 8 1 912 186 A300B4-203 DEFAULT 4 4 Accelerate MaxTakeoff 1 1 434 206 A300B4-203 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 226 A300B4-203 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 A300B4-203 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 A300B4-203 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 A300B4-203 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 A300B4-203 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 A300B4-203 DEFAULT 5 1 Takeoff MaxTakeoff 8 A300B4-203 DEFAULT 5 2 Climb MaxTakeoff 8 1 000 A300B4-203 DEFAULT 5 3 Accelerate MaxTakeoff 8 1 688 194L 168/452 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A300B4-203 DEFAULT 5 4 Accelerate MaxTakeoff 1 1 266 214 A300B4-203 DEFAULT 5 5 Accelerate MaxClimb ZERO 1 000 234 A300B4-203 DEFAULT 5 6 Climb MaxClimb ZERO 3 000 A300B4-203 DEFAULT 5 7 Accelerate MaxClimb ZERO 1 000 250 A300B4-203 DEFAULT 5 8 Climb MaxClimb ZERO 5 500 A300B4-203 DEFAULT 5 9 Climb MaxClimb ZERO 7 500 A300B4-203 DEFAULT 5 10 Climb MaxClimb ZERO 10 000 A310-304 DEFAULT 1 1 Takeoff MaxTakeoff 1 500 A310-304 DEFAULT 1 2 Climb MaxTakeoff 1 500 1 000 A310-304 DEFAULT 1 3 Accelerate MaxTakeoff 1 500 1 475,7 179,5 A310-304 DEFAULT 1 4 Climb MaxClimb 0 3 000 A310-304 DEFAULT 1 5 Accelerate MaxClimb 0 1 454,9 250 A310-304 DEFAULT 1 6 Climb MaxClimb 0 5 500 A310-304 DEFAULT 1 7 Climb MaxClimb 0 7 500 A310-304 DEFAULT 1 8 Climb MaxClimb 0 10 000 A310-304 DEFAULT 2 1 Takeoff MaxTakeoff 1 500 A310-304 DEFAULT 2 2 Climb MaxTakeoff 1 500 1 000 A310-304 DEFAULT 2 3 Accelerate MaxTakeoff 1 500 1 415,7 183 A310-304 DEFAULT 2 4 Climb MaxClimb 0 3 000 A310-304 DEFAULT 2 5 Accelerate MaxClimb 0 1 392,7 2501.7.2015 EN Official Journal of the European Union L 168/453 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A310-304 DEFAULT 2 6 Climb MaxClimb 0 5 500 A310-304 DEFAULT 2 7 Climb MaxClimb 0 7 500 A310-304 DEFAULT 2 8 Climb MaxClimb 0 10 000 A310-304 DEFAULT 3 1 Takeoff MaxTakeoff 1 500 A310-304 DEFAULT 3 2 Climb MaxTakeoff 1 500 1 000 A310-304 DEFAULT 3 3 Accelerate MaxTakeoff 1 500 1 357 186,6 A310-304 DEFAULT 3 4 Climb MaxClimb 0 3 000 A310-304 DEFAULT 3 5 Accelerate MaxClimb 0 1 332,3 250 A310-304 DEFAULT 3 6 Climb MaxClimb 0 5 500 A310-304 DEFAULT 3 7 Climb MaxClimb 0 7 500 A310-304 DEFAULT 3 8 Climb MaxClimb 0 10 000 A310-304 DEFAULT 4 1 Takeoff MaxTakeoff 1 500 A310-304 DEFAULT 4 2 Climb MaxTakeoff 1 500 1 000 A310-304 DEFAULT 4 3 Accelerate MaxTakeoff 1 500 1 262,8 192,8 A310-304 DEFAULT 4 4 Climb MaxClimb 0 3 000 A310-304 DEFAULT 4 5 Accelerate MaxClimb 0 1 234,1 250 A310-304 DEFAULT 4 6 Climb MaxClimb 0 5 500 A310-304 DEFAULT 4 7 Climb MaxClimb 0 7 500 A310-304 DEFAULT 4 8 Climb MaxClimb 0 10 000 A310-304 DEFAULT 5 1 Takeoff MaxTakeoff 1 500L 168/454 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A310-304 DEFAULT 5 2 Climb MaxTakeoff 1 500 1 000 A310-304 DEFAULT 5 3 Accelerate MaxTakeoff 1 500 1 151,8 200,9 A310-304 DEFAULT 5 4 Climb MaxClimb 0 3 000 A310-304 DEFAULT 5 5 Accelerate MaxClimb 0 1 117,9 250 A310-304 DEFAULT 5 6 Climb MaxClimb 0 5 500 A310-304 DEFAULT 5 7 Climb MaxClimb 0 7 500 A310-304 DEFAULT 5 8 Climb MaxClimb 0 10 000 A310-304 DEFAULT 6 1 Takeoff MaxTakeoff 1 500 A310-304 DEFAULT 6 2 Climb MaxTakeoff 1 500 1 000 A310-304 DEFAULT 6 3 Accelerate MaxTakeoff 1 500 990,5 214,3 A310-304 DEFAULT 6 4 Climb MaxClimb 0 3 000 A310-304 DEFAULT 6 5 Accelerate MaxClimb 0 944,8 250 A310-304 DEFAULT 6 6 Climb MaxClimb 0 5 500 A310-304 DEFAULT 6 7 Climb MaxClimb 0 7 500 A310-304 DEFAULT 6 8 Climb MaxClimb 0 10 000 A310-304 ICAO_A 1 1 Takeoff MaxTakeoff 1 500 A310-304 ICAO_A 1 2 Climb MaxTakeoff 1 500 1 500 A310-304 ICAO_A 1 3 Climb MaxClimb 1 500 3 000 A310-304 ICAO_A 1 4 Accelerate MaxClimb 1 500 1 167,6 179,4 A310-304 ICAO_A 1 5 Accelerate MaxClimb 0 1 273,6 200,41.7.2015 EN Official Journal of the European Union L 168/455 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A310-304 ICAO_A 1 6 Accelerate MaxClimb 0 1 496,6 250 A310-304 ICAO_A 1 7 Climb MaxClimb 0 5 500 A310-304 ICAO_A 1 8 Climb MaxClimb 0 7 500 A310-304 ICAO_A 1 9 Climb MaxClimb 0 10 000 A310-304 ICAO_A 2 1 Takeoff MaxTakeoff 1 500 A310-304 ICAO_A 2 2 Climb MaxTakeoff 1 500 1 500 A310-304 ICAO_A 2 3 Climb MaxClimb 1 500 3 000 A310-304 ICAO_A 2 4 Accelerate MaxClimb 1 500 1 115,8 182,9 A310-304 ICAO_A 2 5 Accelerate MaxClimb 0 1 222,3 202,8 A310-304 ICAO_A 2 6 Accelerate MaxClimb 0 1 430,5 250 A310-304 ICAO_A 2 7 Climb MaxClimb 0 5 500 A310-304 ICAO_A 2 8 Climb MaxClimb 0 7 500 A310-304 ICAO_A 2 9 Climb MaxClimb 0 10 000 A310-304 ICAO_A 3 1 Takeoff MaxTakeoff 1 500 A310-304 ICAO_A 3 2 Climb MaxTakeoff 1 500 1 500 A310-304 ICAO_A 3 3 Climb MaxClimb 1 500 3 000 A310-304 ICAO_A 3 4 Accelerate MaxClimb 1 500 1 065,4 186,5 A310-304 ICAO_A 3 5 Accelerate MaxClimb 0 1 172,6 205,3 A310-304 ICAO_A 3 6 Accelerate MaxClimb 0 1 366,6 250 A310-304 ICAO_A 3 7 Climb MaxClimb 0 5 500L 168/456 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A310-304 ICAO_A 3 8 Climb MaxClimb 0 7 500 A310-304 ICAO_A 3 9 Climb MaxClimb 0 10 000 A310-304 ICAO_A 4 1 Takeoff MaxTakeoff 1 500 A310-304 ICAO_A 4 2 Climb MaxTakeoff 1 500 1 500 A310-304 ICAO_A 4 3 Climb MaxClimb 1 500 3 000 A310-304 ICAO_A 4 4 Accelerate MaxClimb 1 500 984,3 192,7 A310-304 ICAO_A 4 5 Accelerate MaxClimb 0 1 091,4 209,7 A310-304 ICAO_A 4 6 Accelerate MaxClimb 0 1 262,9 250 A310-304 ICAO_A 4 7 Climb MaxClimb 0 5 500 A310-304 ICAO_A 4 8 Climb MaxClimb 0 7 500 A310-304 ICAO_A 4 9 Climb MaxClimb 0 10 000 A310-304 ICAO_A 5 1 Takeoff MaxTakeoff 1 500 A310-304 ICAO_A 5 2 Climb MaxTakeoff 1 500 1 500 A310-304 ICAO_A 5 3 Climb MaxClimb 1 500 3 000 A310-304 ICAO_A 5 4 Accelerate MaxClimb 1 500 888,4 200,8 A310-304 ICAO_A 5 5 Accelerate MaxClimb 0 994,5 215,7 A310-304 ICAO_A 5 6 Accelerate MaxClimb 0 1 140,7 250 A310-304 ICAO_A 5 7 Climb MaxClimb 0 5 500 A310-304 ICAO_A 5 8 Climb MaxClimb 0 7 500 A310-304 ICAO_A 5 9 Climb MaxClimb 0 10 0001.7.2015 EN Official Journal of the European Union L 168/457 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A310-304 ICAO_A 6 1 Takeoff MaxTakeoff 1 500 A310-304 ICAO_A 6 2 Climb MaxTakeoff 1 500 1 500 A310-304 ICAO_A 6 3 Climb MaxClimb 1 500 3 000 A310-304 ICAO_A 6 4 Accelerate MaxClimb 1 500 747,4 214,2 A310-304 ICAO_A 6 5 Accelerate MaxClimb 0 848,6 226,2 A310-304 ICAO_A 6 6 Accelerate MaxClimb 0 959,5 250 A310-304 ICAO_A 6 7 Climb MaxClimb 0 5 500 A310-304 ICAO_A 6 8 Climb MaxClimb 0 7 500 A310-304 ICAO_A 6 9 Climb MaxClimb 0 10 000 A310-304 ICAO_B 1 1 Takeoff MaxTakeoff 1 500 A310-304 ICAO_B 1 2 Climb MaxTakeoff 1 500 1 000 A310-304 ICAO_B 1 3 Accelerate MaxTakeoff 1 500 1 475,7 179,5 A310-304 ICAO_B 1 4 Climb MaxClimb 0 3 000 A310-304 ICAO_B 1 5 Accelerate MaxClimb 0 1 454,9 250 A310-304 ICAO_B 1 6 Climb MaxClimb 0 5 500 A310-304 ICAO_B 1 7 Climb MaxClimb 0 7 500 A310-304 ICAO_B 1 8 Climb MaxClimb 0 10 000 A310-304 ICAO_B 2 1 Takeoff MaxTakeoff 1 500 A310-304 ICAO_B 2 2 Climb MaxTakeoff 1 500 1 000 A310-304 ICAO_B 2 3 Accelerate MaxTakeoff 1 500 1 415,7 183L 168/458 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A310-304 ICAO_B 2 4 Climb MaxClimb 0 3 000 A310-304 ICAO_B 2 5 Accelerate MaxClimb 0 1 392,7 250 A310-304 ICAO_B 2 6 Climb MaxClimb 0 5 500 A310-304 ICAO_B 2 7 Climb MaxClimb 0 7 500 A310-304 ICAO_B 2 8 Climb MaxClimb 0 10 000 A310-304 ICAO_B 3 1 Takeoff MaxTakeoff 1 500 A310-304 ICAO_B 3 2 Climb MaxTakeoff 1 500 1 000 A310-304 ICAO_B 3 3 Accelerate MaxTakeoff 1 500 1 357 186,6 A310-304 ICAO_B 3 4 Climb MaxClimb 0 3 000 A310-304 ICAO_B 3 5 Accelerate MaxClimb 0 1 332,3 250 A310-304 ICAO_B 3 6 Climb MaxClimb 0 5 500 A310-304 ICAO_B 3 7 Climb MaxClimb 0 7 500 A310-304 ICAO_B 3 8 Climb MaxClimb 0 10 000 A310-304 ICAO_B 4 1 Takeoff MaxTakeoff 1 500 A310-304 ICAO_B 4 2 Climb MaxTakeoff 1 500 1 000 A310-304 ICAO_B 4 3 Accelerate MaxTakeoff 1 500 1 262,8 192,8 A310-304 ICAO_B 4 4 Climb MaxClimb 0 3 000 A310-304 ICAO_B 4 5 Accelerate MaxClimb 0 1 234,1 250 A310-304 ICAO_B 4 6 Climb MaxClimb 0 5 500 A310-304 ICAO_B 4 7 Climb MaxClimb 0 7 5001.7.2015 EN Official Journal of the European Union L 168/459 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A310-304 ICAO_B 4 8 Climb MaxClimb 0 10 000 A310-304 ICAO_B 5 1 Takeoff MaxTakeoff 1 500 A310-304 ICAO_B 5 2 Climb MaxTakeoff 1 500 1 000 A310-304 ICAO_B 5 3 Accelerate MaxTakeoff 1 500 1 151,8 200,9 A310-304 ICAO_B 5 4 Climb MaxClimb 0 3 000 A310-304 ICAO_B 5 5 Accelerate MaxClimb 0 1 117,9 250 A310-304 ICAO_B 5 6 Climb MaxClimb 0 5 500 A310-304 ICAO_B 5 7 Climb MaxClimb 0 7 500 A310-304 ICAO_B 5 8 Climb MaxClimb 0 10 000 A310-304 ICAO_B 6 1 Takeoff MaxTakeoff 1 500 A310-304 ICAO_B 6 2 Climb MaxTakeoff 1 500 1 000 A310-304 ICAO_B 6 3 Accelerate MaxTakeoff 1 500 990,5 214,3 A310-304 ICAO_B 6 4 Climb MaxClimb 0 3 000 A310-304 ICAO_B 6 5 Accelerate MaxClimb 0 944,8 250 A310-304 ICAO_B 6 6 Climb MaxClimb 0 5 500 A310-304 ICAO_B 6 7 Climb MaxClimb 0 7 500 A310-304 ICAO_B 6 8 Climb MaxClimb 0 10 000 A319-131 DEFAULT 1 1 Takeoff MaxTakeoff 1+F A319-131 DEFAULT 1 2 Climb MaxTakeoff 1+F 1 000 A319-131 DEFAULT 1 3 Accelerate MaxTakeoff 1+F 1 042,6 181,6L 168/460 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A319-131 DEFAULT 1 4 Accelerate MaxTakeoff 1 1 177,5 200,7 A319-131 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 A319-131 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 320,8 250 A319-131 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 A319-131 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 A319-131 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 A319-131 DEFAULT 2 1 Takeoff MaxTakeoff 1+F A319-131 DEFAULT 2 2 Climb MaxTakeoff 1+F 1 000 A319-131 DEFAULT 2 3 Accelerate MaxTakeoff 1+F 997,1 185,3 A319-131 DEFAULT 2 4 Accelerate MaxTakeoff 1 1 128,9 203,3 A319-131 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 A319-131 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 264 250 A319-131 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 A319-131 DEFAULT 2 8 Climb MaxClimb ZERO 7 500 A319-131 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 A319-131 DEFAULT 3 1 Takeoff MaxTakeoff 1+F A319-131 DEFAULT 3 2 Climb MaxTakeoff 1+F 1 000 A319-131 DEFAULT 3 3 Accelerate MaxTakeoff 1+F 952,7 189 A319-131 DEFAULT 3 4 Accelerate MaxTakeoff 1 1 081 206 A319-131 DEFAULT 3 5 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/461 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A319-131 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 208,7 250 A319-131 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 A319-131 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 A319-131 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 A319-131 DEFAULT 4 1 Takeoff MaxTakeoff 1+F A319-131 DEFAULT 4 2 Climb MaxTakeoff 1+F 1 000 A319-131 DEFAULT 4 3 Accelerate MaxTakeoff 1+F 880,8 195,6 A319-131 DEFAULT 4 4 Accelerate MaxTakeoff 1 1 001,7 210,8 A319-131 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 A319-131 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 119,6 250 A319-131 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 A319-131 DEFAULT 4 8 Climb MaxClimb ZERO 7 500 A319-131 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 A319-131 DEFAULT 5 1 Takeoff MaxTakeoff 1+F A319-131 DEFAULT 5 2 Accelerate MaxTakeoff 1+F 735,2 169,7 A319-131 DEFAULT 5 3 Climb MaxTakeoff 1+F 1 000 A319-131 DEFAULT 5 4 Accelerate MaxTakeoff 1+F 793,4 208,8 A319-131 DEFAULT 5 5 Accelerate MaxTakeoff ZERO 860 221,2 A319-131 DEFAULT 5 6 Climb MaxClimb ZERO 3 000 A319-131 DEFAULT 5 7 Accelerate MaxClimb ZERO 964,2 250L 168/462 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A319-131 DEFAULT 5 8 Climb MaxClimb ZERO 5 500 A319-131 DEFAULT 5 9 Climb MaxClimb ZERO 7 500 A319-131 DEFAULT 5 10 Climb MaxClimb ZERO 10 000 A319-131 ICAO_A 1 1 Takeoff MaxTakeoff 1+F A319-131 ICAO_A 1 2 Climb MaxTakeoff 1+F 1 500 A319-131 ICAO_A 1 3 Climb MaxClimb 1+F 3 000 A319-131 ICAO_A 1 4 Accelerate MaxClimb 1+F 822,7 181,4 A319-131 ICAO_A 1 5 Accelerate MaxClimb 1 972,3 196,5 A319-131 ICAO_A 1 6 Accelerate MaxClimb ZERO 1 162,8 223,8 A319-131 ICAO_A 1 7 Accelerate MaxClimb ZERO 1 374,2 250 A319-131 ICAO_A 1 8 Climb MaxClimb ZERO 5 500 A319-131 ICAO_A 1 9 Climb MaxClimb ZERO 7 500 A319-131 ICAO_A 1 10 Climb MaxClimb ZERO 10 000 A319-131 ICAO_A 2 1 Takeoff MaxTakeoff 1+F A319-131 ICAO_A 2 2 Climb MaxTakeoff 1+F 1 500 A319-131 ICAO_A 2 3 Climb MaxClimb 1+F 3 000 A319-131 ICAO_A 2 4 Accelerate MaxClimb 1+F 786,5 185,2 A319-131 ICAO_A 2 5 Accelerate MaxClimb 1 935,4 199,4 A319-131 ICAO_A 2 6 Accelerate MaxClimb ZERO 1 115,9 225,3 A319-131 ICAO_A 2 7 Accelerate MaxClimb ZERO 1 312,1 2501.7.2015 EN Official Journal of the European Union L 168/463 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A319-131 ICAO_A 2 8 Climb MaxClimb ZERO 5 500 A319-131 ICAO_A 2 9 Climb MaxClimb ZERO 7 500 A319-131 ICAO_A 2 10 Climb MaxClimb ZERO 10 000 A319-131 ICAO_A 3 1 Takeoff MaxTakeoff 1+F A319-131 ICAO_A 3 2 Climb MaxTakeoff 1+F 1 500 A319-131 ICAO_A 3 3 Climb MaxClimb 1+F 3 000 A319-131 ICAO_A 3 4 Accelerate MaxClimb 1+F 751,1 188,9 A319-131 ICAO_A 3 5 Accelerate MaxClimb 1 899,4 202,4 A319-131 ICAO_A 3 6 Accelerate MaxClimb ZERO 1 070,2 226,9 A319-131 ICAO_A 3 7 Accelerate MaxClimb ZERO 1 252 250 A319-131 ICAO_A 3 8 Climb MaxClimb ZERO 5 500 A319-131 ICAO_A 3 9 Climb MaxClimb ZERO 7 500 A319-131 ICAO_A 3 10 Climb MaxClimb ZERO 10 000 A319-131 ICAO_A 4 1 Takeoff MaxTakeoff 1+F A319-131 ICAO_A 4 2 Climb MaxTakeoff 1+F 1 500 A319-131 ICAO_A 4 3 Climb MaxClimb 1+F 3 000 A319-131 ICAO_A 4 4 Accelerate MaxClimb 1+F 693,7 195,4 A319-131 ICAO_A 4 5 Accelerate MaxClimb 1 840,2 207,6 A319-131 ICAO_A 4 6 Accelerate MaxClimb ZERO 996,8 230 A319-131 ICAO_A 4 7 Accelerate MaxClimb ZERO 1 155,3 250L 168/464 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A319-131 ICAO_A 4 8 Climb MaxClimb ZERO 5 500 A319-131 ICAO_A 4 9 Climb MaxClimb ZERO 7 500 A319-131 ICAO_A 4 10 Climb MaxClimb ZERO 10 000 A319-131 ICAO_A 5 1 Takeoff MaxTakeoff 1+F A319-131 ICAO_A 5 2 Accelerate MaxTakeoff 1+F 735,2 169,7 A319-131 ICAO_A 5 3 Climb MaxTakeoff 1+F 1 500 A319-131 ICAO_A 5 4 Climb MaxClimb 1+F 3 000 A319-131 ICAO_A 5 5 Accelerate MaxClimb 1+F 637,2 208,7 A319-131 ICAO_A 5 6 Accelerate MaxClimb 1 733,4 218,7 A319-131 ICAO_A 5 7 Accelerate MaxClimb ZERO 869,2 237,4 A319-131 ICAO_A 5 8 Accelerate MaxClimb ZERO 987,8 250 A319-131 ICAO_A 5 9 Climb MaxClimb ZERO 5 500 A319-131 ICAO_A 5 10 Climb MaxClimb ZERO 7 500 A319-131 ICAO_A 5 11 Climb MaxClimb ZERO 10 000 A319-131 ICAO_B 1 1 Takeoff MaxTakeoff 1+F A319-131 ICAO_B 1 2 Climb MaxTakeoff 1+F 1 000 A319-131 ICAO_B 1 3 Accelerate MaxTakeoff 1+F 1 042,6 181,6 A319-131 ICAO_B 1 4 Accelerate MaxTakeoff 1 1 177,5 200,7 A319-131 ICAO_B 1 5 Climb MaxClimb ZERO 3 000 A319-131 ICAO_B 1 6 Accelerate MaxClimb ZERO 1 320,8 2501.7.2015 EN Official Journal of the European Union L 168/465 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A319-131 ICAO_B 1 7 Climb MaxClimb ZERO 5 500 A319-131 ICAO_B 1 8 Climb MaxClimb ZERO 7 500 A319-131 ICAO_B 1 9 Climb MaxClimb ZERO 10 000 A319-131 ICAO_B 2 1 Takeoff MaxTakeoff 1+F A319-131 ICAO_B 2 2 Climb MaxTakeoff 1+F 1 000 A319-131 ICAO_B 2 3 Accelerate MaxTakeoff 1+F 997,1 185,3 A319-131 ICAO_B 2 4 Accelerate MaxTakeoff 1 1 128,9 203,3 A319-131 ICAO_B 2 5 Climb MaxClimb ZERO 3 000 A319-131 ICAO_B 2 6 Accelerate MaxClimb ZERO 1 264 250 A319-131 ICAO_B 2 7 Climb MaxClimb ZERO 5 500 A319-131 ICAO_B 2 8 Climb MaxClimb ZERO 7 500 A319-131 ICAO_B 2 9 Climb MaxClimb ZERO 10 000 A319-131 ICAO_B 3 1 Takeoff MaxTakeoff 1+F A319-131 ICAO_B 3 2 Climb MaxTakeoff 1+F 1 000 A319-131 ICAO_B 3 3 Accelerate MaxTakeoff 1+F 952,7 189 A319-131 ICAO_B 3 4 Accelerate MaxTakeoff 1 1 081 206 A319-131 ICAO_B 3 5 Climb MaxClimb ZERO 3 000 A319-131 ICAO_B 3 6 Accelerate MaxClimb ZERO 1 208,7 250 A319-131 ICAO_B 3 7 Climb MaxClimb ZERO 5 500 A319-131 ICAO_B 3 8 Climb MaxClimb ZERO 7 500L 168/466 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A319-131 ICAO_B 3 9 Climb MaxClimb ZERO 10 000 A319-131 ICAO_B 4 1 Takeoff MaxTakeoff 1+F A319-131 ICAO_B 4 2 Climb MaxTakeoff 1+F 1 000 A319-131 ICAO_B 4 3 Accelerate MaxTakeoff 1+F 880,8 195,6 A319-131 ICAO_B 4 4 Accelerate MaxTakeoff 1 1 001,7 210,8 A319-131 ICAO_B 4 5 Climb MaxClimb ZERO 3 000 A319-131 ICAO_B 4 6 Accelerate MaxClimb ZERO 1 119,6 250 A319-131 ICAO_B 4 7 Climb MaxClimb ZERO 5 500 A319-131 ICAO_B 4 8 Climb MaxClimb ZERO 7 500 A319-131 ICAO_B 4 9 Climb MaxClimb ZERO 10 000 A319-131 ICAO_B 5 1 Takeoff MaxTakeoff 1+F A319-131 ICAO_B 5 2 Accelerate MaxTakeoff 1+F 735,2 169,7 A319-131 ICAO_B 5 3 Climb MaxTakeoff 1+F 1 000 A319-131 ICAO_B 5 4 Accelerate MaxTakeoff 1+F 793,4 208,8 A319-131 ICAO_B 5 5 Accelerate MaxTakeoff ZERO 860 221,2 A319-131 ICAO_B 5 6 Climb MaxClimb ZERO 3 000 A319-131 ICAO_B 5 7 Accelerate MaxClimb ZERO 964,2 250 A319-131 ICAO_B 5 8 Climb MaxClimb ZERO 5 500 A319-131 ICAO_B 5 9 Climb MaxClimb ZERO 7 500 A319-131 ICAO_B 5 10 Climb MaxClimb ZERO 10 0001.7.2015 EN Official Journal of the European Union L 168/467 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-211 DEFAULT 1 1 Takeoff MaxTakeoff 1+F A320-211 DEFAULT 1 2 Climb MaxTakeoff 1+F 1 000 A320-211 DEFAULT 1 3 Accelerate MaxTakeoff 1+F 1 150,5 186,2 A320-211 DEFAULT 1 4 Accelerate MaxTakeoff 1 1 300,7 208,1 A320-211 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 A320-211 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 230,7 250 A320-211 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 A320-211 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 A320-211 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 A320-211 DEFAULT 2 1 Takeoff MaxTakeoff 1+F A320-211 DEFAULT 2 2 Climb MaxTakeoff 1+F 1 000 A320-211 DEFAULT 2 3 Accelerate MaxTakeoff 1+F 1 098,5 190,2 A320-211 DEFAULT 2 4 Accelerate MaxTakeoff 1 1 243,7 210,7 A320-211 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 A320-211 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 171 250 A320-211 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 A320-211 DEFAULT 2 8 Climb MaxClimb ZERO 7 500 A320-211 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 A320-211 DEFAULT 3 1 Takeoff MaxTakeoff 1+F A320-211 DEFAULT 3 2 Climb MaxTakeoff 1+F 1 000L 168/468 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-211 DEFAULT 3 3 Accelerate MaxTakeoff 1+F 1 049,6 194,3 A320-211 DEFAULT 3 4 Accelerate MaxTakeoff 1 1 189,2 213,5 A320-211 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 A320-211 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 113,9 250 A320-211 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 A320-211 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 A320-211 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 A320-211 DEFAULT 4 1 Takeoff MaxTakeoff 1+F A320-211 DEFAULT 4 2 Climb MaxTakeoff 1+F 1 000 A320-211 DEFAULT 4 3 Accelerate MaxTakeoff 1+F 972,6 201,4 A320-211 DEFAULT 4 4 Accelerate MaxTakeoff 1 1 101 218,7 A320-211 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 A320-211 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 021 250 A320-211 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 A320-211 DEFAULT 4 8 Climb MaxClimb ZERO 7 500 A320-211 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 A320-211 DEFAULT 5 1 Takeoff MaxTakeoff 1+F A320-211 DEFAULT 5 2 Climb MaxTakeoff 1+F 1 000 A320-211 DEFAULT 5 3 Accelerate MaxTakeoff 1+F 933,1 205,1 A320-211 DEFAULT 5 4 Accelerate MaxTakeoff 1 1 056 221,41.7.2015 EN Official Journal of the European Union L 168/469 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-211 DEFAULT 5 5 Climb MaxClimb ZERO 3 000 A320-211 DEFAULT 5 6 Accelerate MaxClimb ZERO 973,2 250 A320-211 DEFAULT 5 7 Climb MaxClimb ZERO 5 500 A320-211 DEFAULT 5 8 Climb MaxClimb ZERO 7 500 A320-211 DEFAULT 5 9 Climb MaxClimb ZERO 10 000 A320-211 ICAO_A 1 1 Takeoff MaxTakeoff 1+F A320-211 ICAO_A 1 2 Climb MaxTakeoff 1+F 1 500 A320-211 ICAO_A 1 3 Climb MaxClimb 1+F 3 000 A320-211 ICAO_A 1 4 Accelerate MaxClimb 1+F 812,1 186,1 A320-211 ICAO_A 1 5 Accelerate MaxClimb 1 933,5 201,2 A320-211 ICAO_A 1 6 Accelerate MaxClimb ZERO 1 119,7 228,2 A320-211 ICAO_A 1 7 Accelerate MaxClimb ZERO 1 240,5 250 A320-211 ICAO_A 1 8 Climb MaxClimb ZERO 5 500 A320-211 ICAO_A 1 9 Climb MaxClimb ZERO 7 500 A320-211 ICAO_A 1 10 Climb MaxClimb ZERO 10 000 A320-211 ICAO_A 2 1 Takeoff MaxTakeoff 1+F A320-211 ICAO_A 2 2 Climb MaxTakeoff 1+F 1 500 A320-211 ICAO_A 2 3 Climb MaxClimb 1+F 3 000 A320-211 ICAO_A 2 4 Accelerate MaxClimb 1+F 769,5 190,1 A320-211 ICAO_A 2 5 Accelerate MaxClimb 1 899,8 204,3L 168/470 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-211 ICAO_A 2 6 Accelerate MaxClimb ZERO 1 069,9 229,9 A320-211 ICAO_A 2 7 Accelerate MaxClimb ZERO 1 176,4 250 A320-211 ICAO_A 2 8 Climb MaxClimb ZERO 5 500 A320-211 ICAO_A 2 9 Climb MaxClimb ZERO 7 500 A320-211 ICAO_A 2 10 Climb MaxClimb ZERO 10 000 A320-211 ICAO_A 3 1 Takeoff MaxTakeoff 1+F A320-211 ICAO_A 3 2 Climb MaxTakeoff 1+F 1 500 A320-211 ICAO_A 3 3 Climb MaxClimb 1+F 3 000 A320-211 ICAO_A 3 4 Accelerate MaxClimb 1+F 730,3 194,1 A320-211 ICAO_A 3 5 Accelerate MaxClimb 1 868 207,6 A320-211 ICAO_A 3 6 Accelerate MaxClimb ZERO 1 021,8 231,7 A320-211 ICAO_A 3 7 Accelerate MaxClimb ZERO 1 115,4 250 A320-211 ICAO_A 3 8 Climb MaxClimb ZERO 5 500 A320-211 ICAO_A 3 9 Climb MaxClimb ZERO 7 500 A320-211 ICAO_A 3 10 Climb MaxClimb ZERO 10 000 A320-211 ICAO_A 4 1 Takeoff MaxTakeoff 1+F A320-211 ICAO_A 4 2 Climb MaxTakeoff 1+F 1 500 A320-211 ICAO_A 4 3 Climb MaxClimb 1+F 3 000 A320-211 ICAO_A 4 4 Accelerate MaxClimb 1+F 670,3 201,2 A320-211 ICAO_A 4 5 Accelerate MaxClimb 1 816,4 213,51.7.2015 EN Official Journal of the European Union L 168/471 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-211 ICAO_A 4 6 Accelerate MaxClimb ZERO 942 235,2 A320-211 ICAO_A 4 7 Accelerate MaxClimb ZERO 1 017,5 250 A320-211 ICAO_A 4 8 Climb MaxClimb ZERO 5 500 A320-211 ICAO_A 4 9 Climb MaxClimb ZERO 7 500 A320-211 ICAO_A 4 10 Climb MaxClimb ZERO 10 000 A320-211 ICAO_A 5 1 Takeoff MaxTakeoff 1+F A320-211 ICAO_A 5 2 Climb MaxTakeoff 1+F 1 500 A320-211 ICAO_A 5 3 Climb MaxClimb 1+F 3 000 A320-211 ICAO_A 5 4 Accelerate MaxClimb 1+F 640,5 205 A320-211 ICAO_A 5 5 Accelerate MaxClimb 1 789,5 216,6 A320-211 ICAO_A 5 6 Accelerate MaxClimb ZERO 899,5 237,1 A320-211 ICAO_A 5 7 Accelerate MaxClimb ZERO 968,2 250 A320-211 ICAO_A 5 8 Climb MaxClimb ZERO 5 500 A320-211 ICAO_A 5 9 Climb MaxClimb ZERO 7 500 A320-211 ICAO_A 5 10 Climb MaxClimb ZERO 10 000 A320-211 ICAO_B 1 1 Takeoff MaxTakeoff 1+F A320-211 ICAO_B 1 2 Climb MaxTakeoff 1+F 1 000 A320-211 ICAO_B 1 3 Accelerate MaxTakeoff 1+F 1 150,5 186,2 A320-211 ICAO_B 1 4 Accelerate MaxTakeoff 1 1 300,7 208,1 A320-211 ICAO_B 1 5 Climb MaxClimb ZERO 3 000L 168/472 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-211 ICAO_B 1 6 Accelerate MaxClimb ZERO 1 230,7 250 A320-211 ICAO_B 1 7 Climb MaxClimb ZERO 5 500 A320-211 ICAO_B 1 8 Climb MaxClimb ZERO 7 500 A320-211 ICAO_B 1 9 Climb MaxClimb ZERO 10 000 A320-211 ICAO_B 2 1 Takeoff MaxTakeoff 1+F A320-211 ICAO_B 2 2 Climb MaxTakeoff 1+F 1 000 A320-211 ICAO_B 2 3 Accelerate MaxTakeoff 1+F 1 098,5 190,2 A320-211 ICAO_B 2 4 Accelerate MaxTakeoff 1 1 243,7 210,7 A320-211 ICAO_B 2 5 Climb MaxClimb ZERO 3 000 A320-211 ICAO_B 2 6 Accelerate MaxClimb ZERO 1 171 250 A320-211 ICAO_B 2 7 Climb MaxClimb ZERO 5 500 A320-211 ICAO_B 2 8 Climb MaxClimb ZERO 7 500 A320-211 ICAO_B 2 9 Climb MaxClimb ZERO 10 000 A320-211 ICAO_B 3 1 Takeoff MaxTakeoff 1+F A320-211 ICAO_B 3 2 Climb MaxTakeoff 1+F 1 000 A320-211 ICAO_B 3 3 Accelerate MaxTakeoff 1+F 1 049,6 194,3 A320-211 ICAO_B 3 4 Accelerate MaxTakeoff 1 1 189,2 213,5 A320-211 ICAO_B 3 5 Climb MaxClimb ZERO 3 000 A320-211 ICAO_B 3 6 Accelerate MaxClimb ZERO 1 113,9 250 A320-211 ICAO_B 3 7 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/473 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-211 ICAO_B 3 8 Climb MaxClimb ZERO 7 500 A320-211 ICAO_B 3 9 Climb MaxClimb ZERO 10 000 A320-211 ICAO_B 4 1 Takeoff MaxTakeoff 1+F A320-211 ICAO_B 4 2 Climb MaxTakeoff 1+F 1 000 A320-211 ICAO_B 4 3 Accelerate MaxTakeoff 1+F 972,6 201,4 A320-211 ICAO_B 4 4 Accelerate MaxTakeoff 1 1 101 218,7 A320-211 ICAO_B 4 5 Climb MaxClimb ZERO 3 000 A320-211 ICAO_B 4 6 Accelerate MaxClimb ZERO 1 021 250 A320-211 ICAO_B 4 7 Climb MaxClimb ZERO 5 500 A320-211 ICAO_B 4 8 Climb MaxClimb ZERO 7 500 A320-211 ICAO_B 4 9 Climb MaxClimb ZERO 10 000 A320-211 ICAO_B 5 1 Takeoff MaxTakeoff 1+F A320-211 ICAO_B 5 2 Climb MaxTakeoff 1+F 1 000 A320-211 ICAO_B 5 3 Accelerate MaxTakeoff 1+F 933,1 205,1 A320-211 ICAO_B 5 4 Accelerate MaxTakeoff 1 1 056 221,4 A320-211 ICAO_B 5 5 Climb MaxClimb ZERO 3 000 A320-211 ICAO_B 5 6 Accelerate MaxClimb ZERO 973,2 250 A320-211 ICAO_B 5 7 Climb MaxClimb ZERO 5 500 A320-211 ICAO_B 5 8 Climb MaxClimb ZERO 7 500 A320-211 ICAO_B 5 9 Climb MaxClimb ZERO 10 000L 168/474 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-232 DEFAULT 1 1 Takeoff MaxTakeoff 1+F A320-232 DEFAULT 1 2 Climb MaxTakeoff 1+F 1 000 A320-232 DEFAULT 1 3 Accelerate MaxTakeoff 1+F 1 219,6 185,5 A320-232 DEFAULT 1 4 Accelerate MaxTakeoff 1 1 372,6 208,6 A320-232 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 A320-232 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 192,1 250 A320-232 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 A320-232 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 A320-232 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 A320-232 DEFAULT 2 1 Takeoff MaxTakeoff 1+F A320-232 DEFAULT 2 2 Climb MaxTakeoff 1+F 1 000 A320-232 DEFAULT 2 3 Accelerate MaxTakeoff 1+F 1 167,9 189,3 A320-232 DEFAULT 2 4 Accelerate MaxTakeoff 1 1 315,7 211 A320-232 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 A320-232 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 137,4 250 A320-232 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 A320-232 DEFAULT 2 8 Climb MaxClimb ZERO 7 500 A320-232 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 A320-232 DEFAULT 3 1 Takeoff MaxTakeoff 1+F A320-232 DEFAULT 3 2 Climb MaxTakeoff 1+F 1 0001.7.2015 EN Official Journal of the European Union L 168/475 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-232 DEFAULT 3 3 Accelerate MaxTakeoff 1+F 1 118,6 193,2 A320-232 DEFAULT 3 4 Accelerate MaxTakeoff 1 1 260,6 213,6 A320-232 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 A320-232 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 085,2 250 A320-232 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 A320-232 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 A320-232 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 A320-232 DEFAULT 4 1 Takeoff MaxTakeoff 1+F A320-232 DEFAULT 4 2 Climb MaxTakeoff 1+F 1 000 A320-232 DEFAULT 4 3 Accelerate MaxTakeoff 1+F 1 040,6 199,9 A320-232 DEFAULT 4 4 Accelerate MaxTakeoff 1 1 170,7 218,4 A320-232 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 A320-232 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 001,5 250 A320-232 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 A320-232 DEFAULT 4 8 Climb MaxClimb ZERO 7 500 A320-232 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 A320-232 DEFAULT 5 1 Takeoff MaxTakeoff 1+F A320-232 DEFAULT 5 2 Climb MaxTakeoff 1+F 1 000 A320-232 DEFAULT 5 3 Accelerate MaxTakeoff 1+F 921,9 210,9 A320-232 DEFAULT 5 4 Accelerate MaxTakeoff 1 1 033,9 226,5L 168/476 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-232 DEFAULT 5 5 Climb MaxClimb ZERO 3 000 A320-232 DEFAULT 5 6 Accelerate MaxClimb ZERO 876,3 250 A320-232 DEFAULT 5 7 Climb MaxClimb ZERO 5 500 A320-232 DEFAULT 5 8 Climb MaxClimb ZERO 7 500 A320-232 DEFAULT 5 9 Climb MaxClimb ZERO 10 000 A320-232 ICAO_A 1 1 Takeoff MaxTakeoff 1+F A320-232 ICAO_A 1 2 Climb MaxTakeoff 1+F 1 500 A320-232 ICAO_A 1 3 Climb MaxClimb 1+F 3 000 A320-232 ICAO_A 1 4 Accelerate MaxClimb 1+F 776,1 185,4 A320-232 ICAO_A 1 5 Accelerate MaxClimb 1 906,7 200,1 A320-232 ICAO_A 1 6 Accelerate MaxClimb ZERO 1 062 226 A320-232 ICAO_A 1 7 Accelerate MaxClimb ZERO 1 218,7 250 A320-232 ICAO_A 1 8 Climb MaxClimb ZERO 5 500 A320-232 ICAO_A 1 9 Climb MaxClimb ZERO 7 500 A320-232 ICAO_A 1 10 Climb MaxClimb ZERO 10 000 A320-232 ICAO_A 2 1 Takeoff MaxTakeoff 1+F A320-232 ICAO_A 2 2 Climb MaxTakeoff 1+F 1 500 A320-232 ICAO_A 2 3 Climb MaxClimb 1+F 3 000 A320-232 ICAO_A 2 4 Accelerate MaxClimb 1+F 739,7 189,1 A320-232 ICAO_A 2 5 Accelerate MaxClimb 1 870 2031.7.2015 EN Official Journal of the European Union L 168/477 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-232 ICAO_A 2 6 Accelerate MaxClimb ZERO 1 015,7 227,5 A320-232 ICAO_A 2 7 Accelerate MaxClimb ZERO 1 160,7 250 A320-232 ICAO_A 2 8 Climb MaxClimb ZERO 5 500 A320-232 ICAO_A 2 9 Climb MaxClimb ZERO 7 500 A320-232 ICAO_A 2 10 Climb MaxClimb ZERO 10 000 A320-232 ICAO_A 3 1 Takeoff MaxTakeoff 1+F A320-232 ICAO_A 3 2 Climb MaxTakeoff 1+F 1 500 A320-232 ICAO_A 3 3 Climb MaxClimb 1+F 3 000 A320-232 ICAO_A 3 4 Accelerate MaxClimb 1+F 705 193 A320-232 ICAO_A 3 5 Accelerate MaxClimb 1 834,6 206,1 A320-232 ICAO_A 3 6 Accelerate MaxClimb ZERO 971,6 229,2 A320-232 ICAO_A 3 7 Accelerate MaxClimb ZERO 1 105,4 250 A320-232 ICAO_A 3 8 Climb MaxClimb ZERO 5 500 A320-232 ICAO_A 3 9 Climb MaxClimb ZERO 7 500 A320-232 ICAO_A 3 10 Climb MaxClimb ZERO 10 000 A320-232 ICAO_A 4 1 Takeoff MaxTakeoff 1+F A320-232 ICAO_A 4 2 Climb MaxTakeoff 1+F 1 500 A320-232 ICAO_A 4 3 Climb MaxClimb 1+F 3 000 A320-232 ICAO_A 4 4 Accelerate MaxClimb 1+F 650,5 199,8 A320-232 ICAO_A 4 5 Accelerate MaxClimb 1 776,9 211,6L 168/478 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-232 ICAO_A 4 6 Accelerate MaxClimb ZERO 901,1 232,6 A320-232 ICAO_A 4 7 Accelerate MaxClimb ZERO 1 016,8 250 A320-232 ICAO_A 4 8 Climb MaxClimb ZERO 5 500 A320-232 ICAO_A 4 9 Climb MaxClimb ZERO 7 500 A320-232 ICAO_A 4 10 Climb MaxClimb ZERO 10 000 A320-232 ICAO_A 5 1 Takeoff MaxTakeoff 1+F A320-232 ICAO_A 5 2 Climb MaxTakeoff 1+F 1 500 A320-232 ICAO_A 5 3 Climb MaxClimb 1+F 3 000 A320-232 ICAO_A 5 4 Accelerate MaxClimb 1+F 568,3 210,7 A320-232 ICAO_A 5 5 Accelerate MaxClimb 1 687,3 220,6 A320-232 ICAO_A 5 6 Accelerate MaxClimb ZERO 794,5 238,5 A320-232 ICAO_A 5 7 Accelerate MaxClimb ZERO 884,4 250 A320-232 ICAO_A 5 8 Climb MaxClimb ZERO 5 500 A320-232 ICAO_A 5 9 Climb MaxClimb ZERO 7 500 A320-232 ICAO_A 5 10 Climb MaxClimb ZERO 10 000 A320-232 ICAO_B 1 1 Takeoff MaxTakeoff 1+F A320-232 ICAO_B 1 2 Climb MaxTakeoff 1+F 1 000 A320-232 ICAO_B 1 3 Accelerate MaxTakeoff 1+F 1 219,6 185,5 A320-232 ICAO_B 1 4 Accelerate MaxTakeoff 1 1 372,6 208,6 A320-232 ICAO_B 1 5 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/479 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-232 ICAO_B 1 6 Accelerate MaxClimb ZERO 1 192,1 250 A320-232 ICAO_B 1 7 Climb MaxClimb ZERO 5 500 A320-232 ICAO_B 1 8 Climb MaxClimb ZERO 7 500 A320-232 ICAO_B 1 9 Climb MaxClimb ZERO 10 000 A320-232 ICAO_B 2 1 Takeoff MaxTakeoff 1+F A320-232 ICAO_B 2 2 Climb MaxTakeoff 1+F 1 000 A320-232 ICAO_B 2 3 Accelerate MaxTakeoff 1+F 1 167,9 189,3 A320-232 ICAO_B 2 4 Accelerate MaxTakeoff 1 1 315,7 211 A320-232 ICAO_B 2 5 Climb MaxClimb ZERO 3 000 A320-232 ICAO_B 2 6 Accelerate MaxClimb ZERO 1 137,4 250 A320-232 ICAO_B 2 7 Climb MaxClimb ZERO 5 500 A320-232 ICAO_B 2 8 Climb MaxClimb ZERO 7 500 A320-232 ICAO_B 2 9 Climb MaxClimb ZERO 10 000 A320-232 ICAO_B 3 1 Takeoff MaxTakeoff 1+F A320-232 ICAO_B 3 2 Climb MaxTakeoff 1+F 1 000 A320-232 ICAO_B 3 3 Accelerate MaxTakeoff 1+F 1 118,6 193,2 A320-232 ICAO_B 3 4 Accelerate MaxTakeoff 1 1 260,6 213,6 A320-232 ICAO_B 3 5 Climb MaxClimb ZERO 3 000 A320-232 ICAO_B 3 6 Accelerate MaxClimb ZERO 1 085,2 250 A320-232 ICAO_B 3 7 Climb MaxClimb ZERO 5 500L 168/480 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-232 ICAO_B 3 8 Climb MaxClimb ZERO 7 500 A320-232 ICAO_B 3 9 Climb MaxClimb ZERO 10 000 Table I-4 (part 3) Default departures procedural steps Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-232 ICAO_B 4 1 Takeoff MaxTakeoff 1+F A320-232 ICAO_B 4 2 Climb MaxTakeoff 1+F 1 000 A320-232 ICAO_B 4 3 Accelerate MaxTakeoff 1+F 1 040,6 199,9 A320-232 ICAO_B 4 4 Accelerate MaxTakeoff 1 1 170,7 218,4 A320-232 ICAO_B 4 5 Climb MaxClimb ZERO 3 000 A320-232 ICAO_B 4 6 Accelerate MaxClimb ZERO 1 001,5 250 A320-232 ICAO_B 4 7 Climb MaxClimb ZERO 5 500 A320-232 ICAO_B 4 8 Climb MaxClimb ZERO 7 500 A320-232 ICAO_B 4 9 Climb MaxClimb ZERO 10 000 A320-232 ICAO_B 5 1 Takeoff MaxTakeoff 1+F A320-232 ICAO_B 5 2 Climb MaxTakeoff 1+F 1 000 A320-232 ICAO_B 5 3 Accelerate MaxTakeoff 1+F 921,9 210,9 A320-232 ICAO_B 5 4 Accelerate MaxTakeoff 1 1 033,9 226,5 A320-232 ICAO_B 5 5 Climb MaxClimb ZERO 3 000 A320-232 ICAO_B 5 6 Accelerate MaxClimb ZERO 876,3 2501.7.2015 EN Official Journal of the European Union L 168/481 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A320-232 ICAO_B 5 7 Climb MaxClimb ZERO 5 500 A320-232 ICAO_B 5 8 Climb MaxClimb ZERO 7 500 A320-232 ICAO_B 5 9 Climb MaxClimb ZERO 10 000 A321-232 DEFAULT 1 1 Takeoff MaxTakeoff 1+F A321-232 DEFAULT 1 2 Climb MaxTakeoff 1+F 1 000 A321-232 DEFAULT 1 3 Accelerate MaxTakeoff 1+F 1 235,6 195 A321-232 DEFAULT 1 4 Accelerate MaxTakeoff 1 1 376 219,7 A321-232 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 A321-232 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 127,8 250 A321-232 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 A321-232 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 A321-232 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 A321-232 DEFAULT 2 1 Takeoff MaxTakeoff 1+F A321-232 DEFAULT 2 2 Climb MaxTakeoff 1+F 1 000 A321-232 DEFAULT 2 3 Accelerate MaxTakeoff 1+F 1 180,9 199 A321-232 DEFAULT 2 4 Accelerate MaxTakeoff 1 1 316,8 222,2 A321-232 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 A321-232 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 070,3 250 A321-232 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 A321-232 DEFAULT 2 8 Climb MaxClimb ZERO 7 500L 168/482 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A321-232 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 A321-232 DEFAULT 3 1 Takeoff MaxTakeoff 1+F A321-232 DEFAULT 3 2 Climb MaxTakeoff 1+F 1 000 A321-232 DEFAULT 3 3 Accelerate MaxTakeoff 1+F 1 127,9 203 A321-232 DEFAULT 3 4 Accelerate MaxTakeoff 1 1 259,2 224,8 A321-232 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 A321-232 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 015,1 250 A321-232 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 A321-232 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 A321-232 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 A321-232 DEFAULT 4 1 Takeoff MaxTakeoff 1+F A321-232 DEFAULT 4 2 Climb MaxTakeoff 1+F 1 000 A321-232 DEFAULT 4 3 Accelerate MaxTakeoff 1+F 1 039 209 A321-232 DEFAULT 4 4 Accelerate MaxTakeoff 1 1 161,6 228,6 A321-232 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 A321-232 DEFAULT 4 6 Accelerate MaxClimb ZERO 923,7 250 A321-232 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 A321-232 DEFAULT 4 8 Climb MaxClimb ZERO 7 500 A321-232 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 A321-232 DEFAULT 5 1 Takeoff MaxTakeoff 1+F1.7.2015 EN Official Journal of the European Union L 168/483 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A321-232 DEFAULT 5 2 Climb MaxTakeoff 1+F 1 000 A321-232 DEFAULT 5 3 Accelerate MaxTakeoff 1+F 889,6 210 A321-232 DEFAULT 5 4 Accelerate MaxTakeoff 1 969,1 226,5 A321-232 DEFAULT 5 5 Climb MaxClimb ZERO 3 000 A321-232 DEFAULT 5 6 Accelerate MaxClimb ZERO 752,3 250 A321-232 DEFAULT 5 7 Climb MaxClimb ZERO 5 500 A321-232 DEFAULT 5 8 Climb MaxClimb ZERO 7 500 A321-232 DEFAULT 5 9 Climb MaxClimb ZERO 10 000 A321-232 ICAO_A 1 1 Takeoff MaxTakeoff 1+F A321-232 ICAO_A 1 2 Climb MaxTakeoff 1+F 1 500 A321-232 ICAO_A 1 3 Climb MaxClimb 1+F 3 000 A321-232 ICAO_A 1 4 Accelerate MaxClimb 1+F 819,7 194,9 A321-232 ICAO_A 1 5 Accelerate MaxClimb 1 920,7 210,8 A321-232 ICAO_A 1 6 Accelerate MaxClimb ZERO 1 039,9 234,6 A321-232 ICAO_A 1 7 Accelerate MaxClimb ZERO 1 125,4 250 A321-232 ICAO_A 1 8 Climb MaxClimb ZERO 5 500 A321-232 ICAO_A 1 9 Climb MaxClimb ZERO 7 500 A321-232 ICAO_A 1 10 Climb MaxClimb ZERO 10 000 A321-232 ICAO_A 2 1 Takeoff MaxTakeoff 1+F A321-232 ICAO_A 2 2 Climb MaxTakeoff 1+F 1 500L 168/484 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A321-232 ICAO_A 2 3 Climb MaxClimb 1+F 3 000 A321-232 ICAO_A 2 4 Accelerate MaxClimb 1+F 778,4 198,9 A321-232 ICAO_A 2 5 Accelerate MaxClimb 1 874,3 213,7 A321-232 ICAO_A 2 6 Accelerate MaxClimb ZERO 987,1 236,1 A321-232 ICAO_A 2 7 Accelerate MaxClimb ZERO 1 066,3 250 A321-232 ICAO_A 2 8 Climb MaxClimb ZERO 5 500 A321-232 ICAO_A 2 9 Climb MaxClimb ZERO 7 500 A321-232 ICAO_A 2 10 Climb MaxClimb ZERO 10 000 A321-232 ICAO_A 3 1 Takeoff MaxTakeoff 1+F A321-232 ICAO_A 3 2 Climb MaxTakeoff 1+F 1 500 A321-232 ICAO_A 3 3 Climb MaxClimb 1+F 3 000 A321-232 ICAO_A 3 4 Accelerate MaxClimb 1+F 737,9 202,9 A321-232 ICAO_A 3 5 Accelerate MaxClimb 1 829,1 216,7 A321-232 ICAO_A 3 6 Accelerate MaxClimb ZERO 936,1 237,7 A321-232 ICAO_A 3 7 Accelerate MaxClimb ZERO 1 009,5 250 A321-232 ICAO_A 3 8 Climb MaxClimb ZERO 5 500 A321-232 ICAO_A 3 9 Climb MaxClimb ZERO 7 500 A321-232 ICAO_A 3 10 Climb MaxClimb ZERO 10 000 A321-232 ICAO_A 4 1 Takeoff MaxTakeoff 1+F A321-232 ICAO_A 4 2 Climb MaxTakeoff 1+F 1 5001.7.2015 EN Official Journal of the European Union L 168/485 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A321-232 ICAO_A 4 3 Climb MaxClimb 1+F 3 000 A321-232 ICAO_A 4 4 Accelerate MaxClimb 1+F 670,5 209,9 A321-232 ICAO_A 4 5 Accelerate MaxClimb 1 754,2 222,1 A321-232 ICAO_A 4 6 Accelerate MaxClimb ZERO 852,9 240,9 A321-232 ICAO_A 4 7 Accelerate MaxClimb ZERO 917,2 250 A321-232 ICAO_A 4 8 Climb MaxClimb ZERO 5 500 A321-232 ICAO_A 4 9 Climb MaxClimb ZERO 7 500 A321-232 ICAO_A 4 10 Climb MaxClimb ZERO 10 000 A321-232 ICAO_A 5 1 Takeoff MaxTakeoff 1+F A321-232 ICAO_A 5 2 Climb MaxTakeoff 1+F 1 500 A321-232 ICAO_A 5 3 Climb MaxClimb 1+F 3 000 A321-232 ICAO_A 5 4 Accelerate MaxClimb 1+F 551,5 210 A321-232 ICAO_A 5 5 Accelerate MaxClimb 1 604,9 219,9 A321-232 ICAO_A 5 6 Accelerate MaxClimb ZERO 685,2 235,3 A321-232 ICAO_A 5 7 Accelerate MaxClimb ZERO 749,8 250 A321-232 ICAO_A 5 8 Climb MaxClimb ZERO 5 500 A321-232 ICAO_A 5 9 Climb MaxClimb ZERO 7 500 A321-232 ICAO_A 5 10 Climb MaxClimb ZERO 10 000 A321-232 ICAO_B 1 1 Takeoff MaxTakeoff 1+F A321-232 ICAO_B 1 2 Climb MaxTakeoff 1+F 1 000L 168/486 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A321-232 ICAO_B 1 3 Accelerate MaxTakeoff 1+F 1 235,6 195 A321-232 ICAO_B 1 4 Accelerate MaxTakeoff 1 1 376 219,7 A321-232 ICAO_B 1 5 Climb MaxClimb ZERO 3 000 A321-232 ICAO_B 1 6 Accelerate MaxClimb ZERO 1 127,8 250 A321-232 ICAO_B 1 7 Climb MaxClimb ZERO 5 500 A321-232 ICAO_B 1 8 Climb MaxClimb ZERO 7 500 A321-232 ICAO_B 1 9 Climb MaxClimb ZERO 10 000 A321-232 ICAO_B 2 1 Takeoff MaxTakeoff 1+F A321-232 ICAO_B 2 2 Climb MaxTakeoff 1+F 1 000 A321-232 ICAO_B 2 3 Accelerate MaxTakeoff 1+F 1 180,9 199 A321-232 ICAO_B 2 4 Accelerate MaxTakeoff 1 1 316,8 222,2 A321-232 ICAO_B 2 5 Climb MaxClimb ZERO 3 000 A321-232 ICAO_B 2 6 Accelerate MaxClimb ZERO 1 070,3 250 A321-232 ICAO_B 2 7 Climb MaxClimb ZERO 5 500 A321-232 ICAO_B 2 8 Climb MaxClimb ZERO 7 500 A321-232 ICAO_B 2 9 Climb MaxClimb ZERO 10 000 A321-232 ICAO_B 3 1 Takeoff MaxTakeoff 1+F A321-232 ICAO_B 3 2 Climb MaxTakeoff 1+F 1 000 A321-232 ICAO_B 3 3 Accelerate MaxTakeoff 1+F 1 127,9 203 A321-232 ICAO_B 3 4 Accelerate MaxTakeoff 1 1 259,2 224,81.7.2015 EN Official Journal of the European Union L 168/487 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A321-232 ICAO_B 3 5 Climb MaxClimb ZERO 3 000 A321-232 ICAO_B 3 6 Accelerate MaxClimb ZERO 1 015,1 250 A321-232 ICAO_B 3 7 Climb MaxClimb ZERO 5 500 A321-232 ICAO_B 3 8 Climb MaxClimb ZERO 7 500 A321-232 ICAO_B 3 9 Climb MaxClimb ZERO 10 000 A321-232 ICAO_B 4 1 Takeoff MaxTakeoff 1+F A321-232 ICAO_B 4 2 Climb MaxTakeoff 1+F 1 000 A321-232 ICAO_B 4 3 Accelerate MaxTakeoff 1+F 1 039 209 A321-232 ICAO_B 4 4 Accelerate MaxTakeoff 1 1 161,6 228,6 A321-232 ICAO_B 4 5 Climb MaxClimb ZERO 3 000 A321-232 ICAO_B 4 6 Accelerate MaxClimb ZERO 923,7 250 A321-232 ICAO_B 4 7 Climb MaxClimb ZERO 5 500 A321-232 ICAO_B 4 8 Climb MaxClimb ZERO 7 500 A321-232 ICAO_B 4 9 Climb MaxClimb ZERO 10 000 A321-232 ICAO_B 5 1 Takeoff MaxTakeoff 1+F A321-232 ICAO_B 5 2 Climb MaxTakeoff 1+F 1 000 A321-232 ICAO_B 5 3 Accelerate MaxTakeoff 1+F 889,6 210 A321-232 ICAO_B 5 4 Accelerate MaxTakeoff 1 969,1 226,5 A321-232 ICAO_B 5 5 Climb MaxClimb ZERO 3 000 A321-232 ICAO_B 5 6 Accelerate MaxClimb ZERO 752,3 250L 168/488 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A321-232 ICAO_B 5 7 Climb MaxClimb ZERO 5 500 A321-232 ICAO_B 5 8 Climb MaxClimb ZERO 7 500 A321-232 ICAO_B 5 9 Climb MaxClimb ZERO 10 000 A330-301 DEFAULT 1 1 Takeoff MaxTakeoff 1+F A330-301 DEFAULT 1 2 Climb MaxTakeoff 1+F 1 000 A330-301 DEFAULT 1 3 Accelerate MaxTakeoff 1+F 1 160,6 170,7 A330-301 DEFAULT 1 4 Accelerate MaxTakeoff 1 1 267,7 207,4 A330-301 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 A330-301 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 218,2 250 A330-301 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 A330-301 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 A330-301 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 A330-301 DEFAULT 2 1 Takeoff MaxTakeoff 1+F A330-301 DEFAULT 2 2 Climb MaxTakeoff 1+F 1 000 A330-301 DEFAULT 2 3 Accelerate MaxTakeoff 1+F 1 121,7 173,4 A330-301 DEFAULT 2 4 Accelerate MaxTakeoff 1 1 228,7 208,6 A330-301 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 A330-301 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 176 250 A330-301 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 A330-301 DEFAULT 2 8 Climb MaxClimb ZERO 7 5001.7.2015 EN Official Journal of the European Union L 168/489 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-301 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 A330-301 DEFAULT 3 1 Takeoff MaxTakeoff 1+F A330-301 DEFAULT 3 2 Climb MaxTakeoff 1+F 1 000 A330-301 DEFAULT 3 3 Accelerate MaxTakeoff 1+F 1 083,6 176,1 A330-301 DEFAULT 3 4 Accelerate MaxTakeoff 1 1 190,2 209,8 A330-301 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 A330-301 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 134,5 250 A330-301 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 A330-301 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 A330-301 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 A330-301 DEFAULT 4 1 Takeoff MaxTakeoff 1+F A330-301 DEFAULT 4 2 Climb MaxTakeoff 1+F 1 000 A330-301 DEFAULT 4 3 Accelerate MaxTakeoff 1+F 1 022,6 180,8 A330-301 DEFAULT 4 4 Accelerate MaxTakeoff 1 1 126,6 212,1 A330-301 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 A330-301 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 066,4 250 A330-301 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 A330-301 DEFAULT 4 8 Climb MaxClimb ZERO 7 500 A330-301 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 A330-301 DEFAULT 5 1 Takeoff MaxTakeoff 1+FL 168/490 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-301 DEFAULT 5 2 Climb MaxTakeoff 1+F 1 000 A330-301 DEFAULT 5 3 Accelerate MaxTakeoff 1+F 951,6 186,7 A330-301 DEFAULT 5 4 Accelerate MaxTakeoff 1 1 051,7 215,3 A330-301 DEFAULT 5 5 Climb MaxClimb ZERO 3 000 A330-301 DEFAULT 5 6 Accelerate MaxClimb ZERO 986,6 250 A330-301 DEFAULT 5 7 Climb MaxClimb ZERO 5 500 A330-301 DEFAULT 5 8 Climb MaxClimb ZERO 7 500 A330-301 DEFAULT 5 9 Climb MaxClimb ZERO 10 000 A330-301 DEFAULT 6 1 Takeoff MaxTakeoff 1+F A330-301 DEFAULT 6 2 Climb MaxTakeoff 1+F 1 000 A330-301 DEFAULT 6 3 Accelerate MaxTakeoff 1+F 883,9 193 A330-301 DEFAULT 6 4 Accelerate MaxTakeoff 1 978,1 218,9 A330-301 DEFAULT 6 5 Climb MaxClimb ZERO 3 000 A330-301 DEFAULT 6 6 Accelerate MaxClimb ZERO 908,7 250 A330-301 DEFAULT 6 7 Climb MaxClimb ZERO 5 500 A330-301 DEFAULT 6 8 Climb MaxClimb ZERO 7 500 A330-301 DEFAULT 6 9 Climb MaxClimb ZERO 10 000 A330-301 DEFAULT 7 1 Takeoff MaxTakeoff 1+F A330-301 DEFAULT 7 2 Climb MaxTakeoff 1+F 1 000 A330-301 DEFAULT 7 3 Accelerate MaxTakeoff 1+F 864,2 1951.7.2015 EN Official Journal of the European Union L 168/491 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-301 DEFAULT 7 4 Accelerate MaxTakeoff 1 956,5 220,1 A330-301 DEFAULT 7 5 Climb MaxClimb ZERO 3 000 A330-301 DEFAULT 7 6 Accelerate MaxClimb ZERO 885,7 250 A330-301 DEFAULT 7 7 Climb MaxClimb ZERO 5 500 A330-301 DEFAULT 7 8 Climb MaxClimb ZERO 7 500 A330-301 DEFAULT 7 9 Climb MaxClimb ZERO 10 000 A330-301 ICAO_A 1 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_A 1 2 Climb MaxTakeoff 1+F 1 500 A330-301 ICAO_A 1 3 Climb MaxClimb 1+F 3 000 A330-301 ICAO_A 1 4 Accelerate MaxClimb 1+F 722,8 170,7 A330-301 ICAO_A 1 5 Accelerate MaxClimb 1 783,9 193 A330-301 ICAO_A 1 6 Accelerate MaxClimb ZERO 965 210,2 A330-301 ICAO_A 1 7 Accelerate MaxClimb ZERO 1 210,9 250 A330-301 ICAO_A 1 8 Climb MaxClimb ZERO 5 500 A330-301 ICAO_A 1 9 Climb MaxClimb ZERO 7 500 A330-301 ICAO_A 1 10 Climb MaxClimb ZERO 10 000 A330-301 ICAO_A 2 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_A 2 2 Climb MaxTakeoff 1+F 1 500 A330-301 ICAO_A 2 3 Climb MaxClimb 1+F 3 000 A330-301 ICAO_A 2 4 Accelerate MaxClimb 1+F 694,4 173,3L 168/492 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-301 ICAO_A 2 5 Accelerate MaxClimb 1 758,4 194,7 A330-301 ICAO_A 2 6 Accelerate MaxClimb ZERO 938 211,3 A330-301 ICAO_A 2 7 Accelerate MaxClimb ZERO 1 168,1 250 A330-301 ICAO_A 2 8 Climb MaxClimb ZERO 5 500 A330-301 ICAO_A 2 9 Climb MaxClimb ZERO 7 500 A330-301 ICAO_A 2 10 Climb MaxClimb ZERO 10 000 A330-301 ICAO_A 3 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_A 3 2 Climb MaxTakeoff 1+F 1 500 A330-301 ICAO_A 3 3 Climb MaxClimb 1+F 3 000 A330-301 ICAO_A 3 4 Accelerate MaxClimb 1+F 668,3 176 A330-301 ICAO_A 3 5 Accelerate MaxClimb 1 734,4 196,4 A330-301 ICAO_A 3 6 Accelerate MaxClimb ZERO 911,9 212,4 A330-301 ICAO_A 3 7 Accelerate MaxClimb ZERO 1 126,3 250 A330-301 ICAO_A 3 8 Climb MaxClimb ZERO 5 500 A330-301 ICAO_A 3 9 Climb MaxClimb ZERO 7 500 A330-301 ICAO_A 3 10 Climb MaxClimb ZERO 10 000 A330-301 ICAO_A 4 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_A 4 2 Climb MaxTakeoff 1+F 1 500 A330-301 ICAO_A 4 3 Climb MaxClimb 1+F 3 000 A330-301 ICAO_A 4 4 Accelerate MaxClimb 1+F 622 180,81.7.2015 EN Official Journal of the European Union L 168/493 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-301 ICAO_A 4 5 Accelerate MaxClimb 1 698,3 199,8 A330-301 ICAO_A 4 6 Accelerate MaxClimb ZERO 871,8 214,9 A330-301 ICAO_A 4 7 Accelerate MaxClimb ZERO 1 057,8 250 A330-301 ICAO_A 4 8 Climb MaxClimb ZERO 5 500 A330-301 ICAO_A 4 9 Climb MaxClimb ZERO 7 500 A330-301 ICAO_A 4 10 Climb MaxClimb ZERO 10 000 A330-301 ICAO_A 5 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_A 5 2 Climb MaxTakeoff 1+F 1 500 A330-301 ICAO_A 5 3 Climb MaxClimb 1+F 3 000 A330-301 ICAO_A 5 4 Accelerate MaxClimb 1+F 569,3 186,8 A330-301 ICAO_A 5 5 Accelerate MaxClimb 1 663,1 204,4 A330-301 ICAO_A 5 6 Accelerate MaxClimb ZERO 827,1 218,4 A330-301 ICAO_A 5 7 Accelerate MaxClimb ZERO 977,1 250 A330-301 ICAO_A 5 8 Climb MaxClimb ZERO 5 500 A330-301 ICAO_A 5 9 Climb MaxClimb ZERO 7 500 A330-301 ICAO_A 5 10 Climb MaxClimb ZERO 10 000 A330-301 ICAO_A 6 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_A 6 2 Climb MaxTakeoff 1+F 1 500 A330-301 ICAO_A 6 3 Climb MaxClimb 1+F 3 000 A330-301 ICAO_A 6 4 Accelerate MaxClimb 1+F 519,8 193L 168/494 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-301 ICAO_A 6 5 Accelerate MaxClimb 1 634,2 209,3 A330-301 ICAO_A 6 6 Accelerate MaxClimb ZERO 781 222,2 A330-301 ICAO_A 6 7 Accelerate MaxClimb ZERO 898,1 250 A330-301 ICAO_A 6 8 Climb MaxClimb ZERO 5 500 A330-301 ICAO_A 6 9 Climb MaxClimb ZERO 7 500 A330-301 ICAO_A 6 10 Climb MaxClimb ZERO 10 000 A330-301 ICAO_A 7 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_A 7 2 Climb MaxTakeoff 1+F 1 500 A330-301 ICAO_A 7 3 Climb MaxClimb 1+F 3 000 A330-301 ICAO_A 7 4 Accelerate MaxClimb 1+F 506,2 194,9 A330-301 ICAO_A 7 5 Accelerate MaxClimb 1 625,8 210,8 A330-301 ICAO_A 7 6 Accelerate MaxClimb ZERO 766,4 223,5 A330-301 ICAO_A 7 7 Accelerate MaxClimb ZERO 875,2 250 A330-301 ICAO_A 7 8 Climb MaxClimb ZERO 5 500 A330-301 ICAO_A 7 9 Climb MaxClimb ZERO 7 500 A330-301 ICAO_A 7 10 Climb MaxClimb ZERO 10 000 A330-301 ICAO_B 1 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_B 1 2 Climb MaxTakeoff 1+F 1 000 A330-301 ICAO_B 1 3 Accelerate MaxTakeoff 1+F 1 160,6 170,7 A330-301 ICAO_B 1 4 Accelerate MaxTakeoff 1 1 267,7 207,41.7.2015 EN Official Journal of the European Union L 168/495 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-301 ICAO_B 1 5 Climb MaxClimb ZERO 3 000 A330-301 ICAO_B 1 6 Accelerate MaxClimb ZERO 1 218,2 250 A330-301 ICAO_B 1 7 Climb MaxClimb ZERO 5 500 A330-301 ICAO_B 1 8 Climb MaxClimb ZERO 7 500 A330-301 ICAO_B 1 9 Climb MaxClimb ZERO 10 000 A330-301 ICAO_B 2 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_B 2 2 Climb MaxTakeoff 1+F 1 000 A330-301 ICAO_B 2 3 Accelerate MaxTakeoff 1+F 1 121,7 173,4 A330-301 ICAO_B 2 4 Accelerate MaxTakeoff 1 1 228,7 208,6 A330-301 ICAO_B 2 5 Climb MaxClimb ZERO 3 000 A330-301 ICAO_B 2 6 Accelerate MaxClimb ZERO 1 176 250 A330-301 ICAO_B 2 7 Climb MaxClimb ZERO 5 500 A330-301 ICAO_B 2 8 Climb MaxClimb ZERO 7 500 A330-301 ICAO_B 2 9 Climb MaxClimb ZERO 10 000 A330-301 ICAO_B 3 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_B 3 2 Climb MaxTakeoff 1+F 1 000 A330-301 ICAO_B 3 3 Accelerate MaxTakeoff 1+F 1 083,6 176,1 A330-301 ICAO_B 3 4 Accelerate MaxTakeoff 1 1 190,2 209,8 A330-301 ICAO_B 3 5 Climb MaxClimb ZERO 3 000 A330-301 ICAO_B 3 6 Accelerate MaxClimb ZERO 1 134,5 250L 168/496 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-301 ICAO_B 3 7 Climb MaxClimb ZERO 5 500 A330-301 ICAO_B 3 8 Climb MaxClimb ZERO 7 500 A330-301 ICAO_B 3 9 Climb MaxClimb ZERO 10 000 A330-301 ICAO_B 4 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_B 4 2 Climb MaxTakeoff 1+F 1 000 A330-301 ICAO_B 4 3 Accelerate MaxTakeoff 1+F 1 022,6 180,8 A330-301 ICAO_B 4 4 Accelerate MaxTakeoff 1 1 126,6 212,1 A330-301 ICAO_B 4 5 Climb MaxClimb ZERO 3 000 A330-301 ICAO_B 4 6 Accelerate MaxClimb ZERO 1 066,4 250 A330-301 ICAO_B 4 7 Climb MaxClimb ZERO 5 500 A330-301 ICAO_B 4 8 Climb MaxClimb ZERO 7 500 A330-301 ICAO_B 4 9 Climb MaxClimb ZERO 10 000 A330-301 ICAO_B 5 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_B 5 2 Climb MaxTakeoff 1+F 1 000 A330-301 ICAO_B 5 3 Accelerate MaxTakeoff 1+F 951,6 186,7 A330-301 ICAO_B 5 4 Accelerate MaxTakeoff 1 1 051,7 215,3 A330-301 ICAO_B 5 5 Climb MaxClimb ZERO 3 000 A330-301 ICAO_B 5 6 Accelerate MaxClimb ZERO 986,6 250 A330-301 ICAO_B 5 7 Climb MaxClimb ZERO 5 500 A330-301 ICAO_B 5 8 Climb MaxClimb ZERO 7 5001.7.2015 EN Official Journal of the European Union L 168/497 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-301 ICAO_B 5 9 Climb MaxClimb ZERO 10 000 A330-301 ICAO_B 6 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_B 6 2 Climb MaxTakeoff 1+F 1 000 A330-301 ICAO_B 6 3 Accelerate MaxTakeoff 1+F 883,9 193 A330-301 ICAO_B 6 4 Accelerate MaxTakeoff 1 978,1 218,9 A330-301 ICAO_B 6 5 Climb MaxClimb ZERO 3 000 A330-301 ICAO_B 6 6 Accelerate MaxClimb ZERO 908,7 250 A330-301 ICAO_B 6 7 Climb MaxClimb ZERO 5 500 A330-301 ICAO_B 6 8 Climb MaxClimb ZERO 7 500 A330-301 ICAO_B 6 9 Climb MaxClimb ZERO 10 000 A330-301 ICAO_B 7 1 Takeoff MaxTakeoff 1+F A330-301 ICAO_B 7 2 Climb MaxTakeoff 1+F 1 000 A330-301 ICAO_B 7 3 Accelerate MaxTakeoff 1+F 864,2 195 A330-301 ICAO_B 7 4 Accelerate MaxTakeoff 1 956,5 220,1 A330-301 ICAO_B 7 5 Climb MaxClimb ZERO 3 000 A330-301 ICAO_B 7 6 Accelerate MaxClimb ZERO 885,7 250 A330-301 ICAO_B 7 7 Climb MaxClimb ZERO 5 500 A330-301 ICAO_B 7 8 Climb MaxClimb ZERO 7 500 A330-301 ICAO_B 7 9 Climb MaxClimb ZERO 10 000 A330-343 DEFAULT 1 1 Takeoff MaxTakeoff 1+FL 168/498 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-343 DEFAULT 1 2 Climb MaxTakeoff 1+F 1 000 A330-343 DEFAULT 1 3 Accelerate MaxTakeoff 1+F 1 273,5 174,9 A330-343 DEFAULT 1 4 Accelerate MaxTakeoff 1 1 384,8 213,9 A330-343 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 A330-343 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 268,1 250 A330-343 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 A330-343 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 A330-343 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 A330-343 DEFAULT 2 1 Takeoff MaxTakeoff 1+F A330-343 DEFAULT 2 2 Climb MaxTakeoff 1+F 1 000 A330-343 DEFAULT 2 3 Accelerate MaxTakeoff 1+F 1 218,9 177,7 A330-343 DEFAULT 2 4 Accelerate MaxTakeoff 1 1 340,4 215 A330-343 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 A330-343 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 223,6 250 A330-343 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 A330-343 DEFAULT 2 8 Climb MaxClimb ZERO 7 500 A330-343 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 A330-343 DEFAULT 3 1 Takeoff MaxTakeoff 1+F A330-343 DEFAULT 3 2 Climb MaxTakeoff 1+F 1 000 A330-343 DEFAULT 3 3 Accelerate MaxTakeoff 1+F 1 181,2 180,41.7.2015 EN Official Journal of the European Union L 168/499 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-343 DEFAULT 3 4 Accelerate MaxTakeoff 1 1 296,6 216,1 A330-343 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 A330-343 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 180 250 A330-343 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 A330-343 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 A330-343 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 A330-343 DEFAULT 4 1 Takeoff MaxTakeoff 1+F A330-343 DEFAULT 4 2 Climb MaxTakeoff 1+F 1 000 A330-343 DEFAULT 4 3 Accelerate MaxTakeoff 1+F 1 115,2 185,2 A330-343 DEFAULT 4 4 Accelerate MaxTakeoff 1 1 224,1 218,3 A330-343 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 A330-343 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 108,4 250 A330-343 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 A330-343 DEFAULT 4 8 Climb MaxClimb ZERO 7 500 A330-343 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 A330-343 DEFAULT 5 1 Takeoff MaxTakeoff 1+F A330-343 DEFAULT 5 2 Climb MaxTakeoff 1+F 1 000 A330-343 DEFAULT 5 3 Accelerate MaxTakeoff 1+F 1 038,3 191,3 A330-343 DEFAULT 5 4 Accelerate MaxTakeoff 1 1 139,2 221,4 A330-343 DEFAULT 5 5 Climb MaxClimb ZERO 3 000L 168/500 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-343 DEFAULT 5 6 Accelerate MaxClimb ZERO 1 025,2 250 A330-343 DEFAULT 5 7 Climb MaxClimb ZERO 5 500 A330-343 DEFAULT 5 8 Climb MaxClimb ZERO 7 500 A330-343 DEFAULT 5 9 Climb MaxClimb ZERO 10 000 A330-343 DEFAULT 6 1 Takeoff MaxTakeoff 1+F A330-343 DEFAULT 6 2 Climb MaxTakeoff 1+F 1 000 A330-343 DEFAULT 6 3 Accelerate MaxTakeoff 1+F 962,8 197,3 A330-343 DEFAULT 6 4 Accelerate MaxTakeoff 1 1 054,3 224,5 A330-343 DEFAULT 6 5 Climb MaxClimb ZERO 3 000 A330-343 DEFAULT 6 6 Accelerate MaxClimb ZERO 943,3 250 A330-343 DEFAULT 6 7 Climb MaxClimb ZERO 5 500 A330-343 DEFAULT 6 8 Climb MaxClimb ZERO 7 500 A330-343 DEFAULT 6 9 Climb MaxClimb ZERO 10 000 A330-343 DEFAULT 7 1 Takeoff MaxTakeoff 1+F A330-343 DEFAULT 7 2 Climb MaxTakeoff 1+F 1 000 A330-343 DEFAULT 7 3 Accelerate MaxTakeoff 1+F 869,5 200,8 A330-343 DEFAULT 7 4 Accelerate MaxTakeoff 1 948,6 225 A330-343 DEFAULT 7 5 Climb MaxClimb ZERO 3 000 A330-343 DEFAULT 7 6 Accelerate MaxClimb ZERO 842 250 A330-343 DEFAULT 7 7 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/501 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-343 DEFAULT 7 8 Climb MaxClimb ZERO 7 500 A330-343 DEFAULT 7 9 Climb MaxClimb ZERO 10 000 A330-343 ICAO_A 1 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_A 1 2 Climb MaxTakeoff 1+F 1 500 A330-343 ICAO_A 1 3 Climb MaxClimb 1+F 3 000 A330-343 ICAO_A 1 4 Accelerate MaxClimb 1+F 839,6 174,8 A330-343 ICAO_A 1 5 Accelerate MaxClimb 1 914,2 200,1 A330-343 ICAO_A 1 6 Accelerate MaxClimb ZERO 1 103,7 218,9 A330-343 ICAO_A 1 7 Accelerate MaxClimb ZERO 1 253,2 250 A330-343 ICAO_A 1 8 Climb MaxClimb ZERO 5 500 A330-343 ICAO_A 1 9 Climb MaxClimb ZERO 7 500 A330-343 ICAO_A 1 10 Climb MaxClimb ZERO 10 000 A330-343 ICAO_A 2 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_A 2 2 Climb MaxTakeoff 1+F 1 500 A330-343 ICAO_A 2 3 Climb MaxClimb 1+F 3 000 A330-343 ICAO_A 2 4 Accelerate MaxClimb 1+F 801,5 177,5 A330-343 ICAO_A 2 5 Accelerate MaxClimb 1 885,4 201,7 A330-343 ICAO_A 2 6 Accelerate MaxClimb ZERO 1 068,3 219,8 A330-343 ICAO_A 2 7 Accelerate MaxClimb ZERO 1 208,4 250 A330-343 ICAO_A 2 8 Climb MaxClimb ZERO 5 500L 168/502 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-343 ICAO_A 2 9 Climb MaxClimb ZERO 7 500 A330-343 ICAO_A 2 10 Climb MaxClimb ZERO 10 000 A330-343 ICAO_A 3 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_A 3 2 Climb MaxTakeoff 1+F 1 500 A330-343 ICAO_A 3 3 Climb MaxClimb 1+F 3 000 A330-343 ICAO_A 3 4 Accelerate MaxClimb 1+F 766,4 180,3 A330-343 ICAO_A 3 5 Accelerate MaxClimb 1 857,9 203,5 A330-343 ICAO_A 3 6 Accelerate MaxClimb ZERO 1 033,8 220,9 A330-343 ICAO_A 3 7 Accelerate MaxClimb ZERO 1 164,8 250 A330-343 ICAO_A 3 8 Climb MaxClimb ZERO 5 500 A330-343 ICAO_A 3 9 Climb MaxClimb ZERO 7 500 A330-343 ICAO_A 3 10 Climb MaxClimb ZERO 10 000 A330-343 ICAO_A 4 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_A 4 2 Climb MaxTakeoff 1+F 1 500 A330-343 ICAO_A 4 3 Climb MaxClimb 1+F 3 000 A330-343 ICAO_A 4 4 Accelerate MaxClimb 1+F 717,5 185,3 A330-343 ICAO_A 4 5 Accelerate MaxClimb 1 814,6 206,8 A330-343 ICAO_A 4 6 Accelerate MaxClimb ZERO 977,3 223 A330-343 ICAO_A 4 7 Accelerate MaxClimb ZERO 1 093,5 250 A330-343 ICAO_A 4 8 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/503 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-343 ICAO_A 4 9 Climb MaxClimb ZERO 7 500 A330-343 ICAO_A 4 10 Climb MaxClimb ZERO 10 000 A330-343 ICAO_A 5 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_A 5 2 Climb MaxTakeoff 1+F 1 500 A330-343 ICAO_A 5 3 Climb MaxClimb 1+F 3 000 A330-343 ICAO_A 5 4 Accelerate MaxClimb 1+F 661,1 191,5 A330-343 ICAO_A 5 5 Accelerate MaxClimb 1 767 211,2 A330-343 ICAO_A 5 6 Accelerate MaxClimb ZERO 910,6 226,1 A330-343 ICAO_A 5 7 Accelerate MaxClimb ZERO 1 011 250 A330-343 ICAO_A 5 8 Climb MaxClimb ZERO 5 500 A330-343 ICAO_A 5 9 Climb MaxClimb ZERO 7 500 A330-343 ICAO_A 5 10 Climb MaxClimb ZERO 10 000 A330-343 ICAO_A 6 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_A 6 2 Climb MaxTakeoff 1+F 1 500 A330-343 ICAO_A 6 3 Climb MaxClimb 1+F 3 000 A330-343 ICAO_A 6 4 Accelerate MaxClimb 1+F 607,1 197,4 A330-343 ICAO_A 6 5 Accelerate MaxClimb 1 717 215,3 A330-343 ICAO_A 6 6 Accelerate MaxClimb ZERO 840,3 228,8 A330-343 ICAO_A 6 7 Accelerate MaxClimb ZERO 929,9 250 A330-343 ICAO_A 6 8 Climb MaxClimb ZERO 5 500L 168/504 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-343 ICAO_A 6 9 Climb MaxClimb ZERO 7 500 A330-343 ICAO_A 6 10 Climb MaxClimb ZERO 10 000 A330-343 ICAO_A 7 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_A 7 2 Climb MaxTakeoff 1+F 1 500 A330-343 ICAO_A 7 3 Climb MaxClimb 1+F 3 000 A330-343 ICAO_A 7 4 Accelerate MaxClimb 1+F 538 200,4 A330-343 ICAO_A 7 5 Accelerate MaxClimb 1 638,8 216,2 A330-343 ICAO_A 7 6 Accelerate MaxClimb ZERO 743,9 228,1 A330-343 ICAO_A 7 7 Accelerate MaxClimb ZERO 830,4 250 A330-343 ICAO_A 7 8 Climb MaxClimb ZERO 5 500 A330-343 ICAO_A 7 9 Climb MaxClimb ZERO 7 500 A330-343 ICAO_A 7 10 Climb MaxClimb ZERO 10 000 A330-343 ICAO_B 1 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_B 1 2 Climb MaxTakeoff 1+F 1 000 A330-343 ICAO_B 1 3 Accelerate MaxTakeoff 1+F 1 273,5 174,9 A330-343 ICAO_B 1 4 Accelerate MaxTakeoff 1 1 384,8 213,9 A330-343 ICAO_B 1 5 Climb MaxClimb ZERO 3 000 A330-343 ICAO_B 1 6 Accelerate MaxClimb ZERO 1 268,1 250 A330-343 ICAO_B 1 7 Climb MaxClimb ZERO 5 500 A330-343 ICAO_B 1 8 Climb MaxClimb ZERO 7 5001.7.2015 EN Official Journal of the European Union L 168/505 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-343 ICAO_B 1 9 Climb MaxClimb ZERO 10 000 A330-343 ICAO_B 2 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_B 2 2 Climb MaxTakeoff 1+F 1 000 A330-343 ICAO_B 2 3 Accelerate MaxTakeoff 1+F 1 218,9 177,7 A330-343 ICAO_B 2 4 Accelerate MaxTakeoff 1 1 340,4 215 A330-343 ICAO_B 2 5 Climb MaxClimb ZERO 3 000 A330-343 ICAO_B 2 6 Accelerate MaxClimb ZERO 1 223,6 250 A330-343 ICAO_B 2 7 Climb MaxClimb ZERO 5 500 A330-343 ICAO_B 2 8 Climb MaxClimb ZERO 7 500 A330-343 ICAO_B 2 9 Climb MaxClimb ZERO 10 000 A330-343 ICAO_B 3 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_B 3 2 Climb MaxTakeoff 1+F 1 000 A330-343 ICAO_B 3 3 Accelerate MaxTakeoff 1+F 1 181,2 180,4 A330-343 ICAO_B 3 4 Accelerate MaxTakeoff 1 1 296,6 216,1 A330-343 ICAO_B 3 5 Climb MaxClimb ZERO 3 000 A330-343 ICAO_B 3 6 Accelerate MaxClimb ZERO 1 180 250 A330-343 ICAO_B 3 7 Climb MaxClimb ZERO 5 500 A330-343 ICAO_B 3 8 Climb MaxClimb ZERO 7 500 A330-343 ICAO_B 3 9 Climb MaxClimb ZERO 10 000 A330-343 ICAO_B 4 1 Takeoff MaxTakeoff 1+FL 168/506 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-343 ICAO_B 4 2 Climb MaxTakeoff 1+F 1 000 A330-343 ICAO_B 4 3 Accelerate MaxTakeoff 1+F 1 115,2 185,2 A330-343 ICAO_B 4 4 Accelerate MaxTakeoff 1 1 224,1 218,3 A330-343 ICAO_B 4 5 Climb MaxClimb ZERO 3 000 A330-343 ICAO_B 4 6 Accelerate MaxClimb ZERO 1 108,4 250 A330-343 ICAO_B 4 7 Climb MaxClimb ZERO 5 500 A330-343 ICAO_B 4 8 Climb MaxClimb ZERO 7 500 A330-343 ICAO_B 4 9 Climb MaxClimb ZERO 10 000 A330-343 ICAO_B 5 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_B 5 2 Climb MaxTakeoff 1+F 1 000 A330-343 ICAO_B 5 3 Accelerate MaxTakeoff 1+F 1 038,3 191,3 A330-343 ICAO_B 5 4 Accelerate MaxTakeoff 1 1 139,2 221,4 A330-343 ICAO_B 5 5 Climb MaxClimb ZERO 3 000 A330-343 ICAO_B 5 6 Accelerate MaxClimb ZERO 1 025,2 250 A330-343 ICAO_B 5 7 Climb MaxClimb ZERO 5 500 A330-343 ICAO_B 5 8 Climb MaxClimb ZERO 7 500 A330-343 ICAO_B 5 9 Climb MaxClimb ZERO 10 000 A330-343 ICAO_B 6 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_B 6 2 Climb MaxTakeoff 1+F 1 000 A330-343 ICAO_B 6 3 Accelerate MaxTakeoff 1+F 962,8 197,31.7.2015 EN Official Journal of the European Union L 168/507 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A330-343 ICAO_B 6 4 Accelerate MaxTakeoff 1 1 054,3 224,5 A330-343 ICAO_B 6 5 Climb MaxClimb ZERO 3 000 A330-343 ICAO_B 6 6 Accelerate MaxClimb ZERO 943,3 250 A330-343 ICAO_B 6 7 Climb MaxClimb ZERO 5 500 A330-343 ICAO_B 6 8 Climb MaxClimb ZERO 7 500 A330-343 ICAO_B 6 9 Climb MaxClimb ZERO 10 000 A330-343 ICAO_B 7 1 Takeoff MaxTakeoff 1+F A330-343 ICAO_B 7 2 Climb MaxTakeoff 1+F 1 000 A330-343 ICAO_B 7 3 Accelerate MaxTakeoff 1+F 869,5 200,8 A330-343 ICAO_B 7 4 Accelerate MaxTakeoff 1 948,6 225 A330-343 ICAO_B 7 5 Climb MaxClimb ZERO 3 000 A330-343 ICAO_B 7 6 Accelerate MaxClimb ZERO 842 250 A330-343 ICAO_B 7 7 Climb MaxClimb ZERO 5 500 A330-343 ICAO_B 7 8 Climb MaxClimb ZERO 7 500 A330-343 ICAO_B 7 9 Climb MaxClimb ZERO 10 000 A340-211 DEFAULT 1 1 Takeoff MaxTakeoff 1+F A340-211 DEFAULT 1 2 Climb MaxTakeoff 1+F 1 000 A340-211 DEFAULT 1 3 Accelerate MaxTakeoff 1+F 1 019,3 177,6 A340-211 DEFAULT 1 4 Accelerate MaxTakeoff 1 1 101,1 215,2 A340-211 DEFAULT 1 5 Climb MaxClimb ZERO 3 000L 168/508 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-211 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 165,6 250 A340-211 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 A340-211 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 A340-211 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 A340-211 DEFAULT 2 1 Takeoff MaxTakeoff 1+F A340-211 DEFAULT 2 2 Climb MaxTakeoff 1+F 1 000 A340-211 DEFAULT 2 3 Accelerate MaxTakeoff 1+F 973,9 180,5 A340-211 DEFAULT 2 4 Accelerate MaxTakeoff 1 1 061,1 216,3 A340-211 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 A340-211 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 120,6 250 A340-211 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 A340-211 DEFAULT 2 8 Climb MaxClimb ZERO 7 500 A340-211 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 A340-211 DEFAULT 3 1 Takeoff MaxTakeoff 1+F A340-211 DEFAULT 3 2 Climb MaxTakeoff 1+F 1 000 A340-211 DEFAULT 3 3 Accelerate MaxTakeoff 1+F 930,2 183,1 A340-211 DEFAULT 3 4 Accelerate MaxTakeoff 1 1 021,2 217,3 A340-211 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 A340-211 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 076,1 250 A340-211 DEFAULT 3 7 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/509 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-211 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 A340-211 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 A340-211 DEFAULT 4 1 Takeoff MaxTakeoff 1+F A340-211 DEFAULT 4 2 Climb MaxTakeoff 1+F 1 000 A340-211 DEFAULT 4 3 Accelerate MaxTakeoff 1+F 860,1 188,2 A340-211 DEFAULT 4 4 Accelerate MaxTakeoff 1 955,9 219,5 A340-211 DEFAULT 4 5 Climb MaxClimb ZERO 3 000 A340-211 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 003,9 250 A340-211 DEFAULT 4 7 Climb MaxClimb ZERO 5 500 A340-211 DEFAULT 4 8 Climb MaxClimb ZERO 7 500 A340-211 DEFAULT 4 9 Climb MaxClimb ZERO 10 000 A340-211 DEFAULT 5 1 Takeoff MaxTakeoff 1+F A340-211 DEFAULT 5 2 Climb MaxTakeoff 1+F 1 000 A340-211 DEFAULT 5 3 Accelerate MaxTakeoff 1+F 779,4 194,9 A340-211 DEFAULT 5 4 Accelerate MaxTakeoff 1 879,4 222,9 A340-211 DEFAULT 5 5 Climb MaxClimb ZERO 3 000 A340-211 DEFAULT 5 6 Accelerate MaxClimb ZERO 920,2 250 A340-211 DEFAULT 5 7 Climb MaxClimb ZERO 5 500 A340-211 DEFAULT 5 8 Climb MaxClimb ZERO 7 500 A340-211 DEFAULT 5 9 Climb MaxClimb ZERO 10 000L 168/510 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-211 DEFAULT 6 1 Takeoff MaxTakeoff 1+F A340-211 DEFAULT 6 2 Climb MaxTakeoff 1+F 1 000 A340-211 DEFAULT 6 3 Accelerate MaxTakeoff 1+F 705,2 199,2 A340-211 DEFAULT 6 4 Accelerate MaxTakeoff 1 802 224,4 A340-211 DEFAULT 6 5 Climb MaxClimb ZERO 3 000 A340-211 DEFAULT 6 6 Accelerate MaxClimb ZERO 836,4 250 A340-211 DEFAULT 6 7 Climb MaxClimb ZERO 5 500 A340-211 DEFAULT 6 8 Climb MaxClimb ZERO 7 500 A340-211 DEFAULT 6 9 Climb MaxClimb ZERO 10 000 A340-211 DEFAULT 7 1 Takeoff MaxTakeoff 1+F A340-211 DEFAULT 7 2 Climb MaxTakeoff 1+F 1 000 A340-211 DEFAULT 7 3 Accelerate MaxTakeoff 1+F 519,8 199,2 A340-211 DEFAULT 7 4 Accelerate MaxTakeoff 1 591,5 218,2 A340-211 DEFAULT 7 5 Accelerate MaxTakeoff 1 653,7 223,4 A340-211 DEFAULT 7 6 Climb MaxClimb ZERO 3 000 A340-211 DEFAULT 7 7 Accelerate MaxClimb ZERO 622,6 250 A340-211 DEFAULT 7 8 Climb MaxClimb ZERO 5 500 A340-211 DEFAULT 7 9 Climb MaxClimb ZERO 7 500 A340-211 DEFAULT 7 10 Climb MaxClimb ZERO 10 000 A340-211 ICAO_A 1 1 Takeoff MaxTakeoff 1+F1.7.2015 EN Official Journal of the European Union L 168/511 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-211 ICAO_A 1 2 Climb MaxTakeoff 1+F 1 500 A340-211 ICAO_A 1 3 Climb MaxClimb 1+F 3 000 A340-211 ICAO_A 1 4 Accelerate MaxClimb 1+F 832,3 177,4 A340-211 ICAO_A 1 5 Accelerate MaxClimb 1 890,6 206,8 A340-211 ICAO_A 1 6 Accelerate MaxClimb ZERO 1 039,6 227,9 A340-211 ICAO_A 1 7 Accelerate MaxClimb ZERO 1 154,4 250 A340-211 ICAO_A 1 8 Climb MaxClimb ZERO 5 500 A340-211 ICAO_A 1 9 Climb MaxClimb ZERO 7 500 A340-211 ICAO_A 1 10 Climb MaxClimb ZERO 10 000 A340-211 ICAO_A 2 1 Takeoff MaxTakeoff 1+F A340-211 ICAO_A 2 2 Climb MaxTakeoff 1+F 1 500 A340-211 ICAO_A 2 3 Climb MaxClimb 1+F 3 000 A340-211 ICAO_A 2 4 Accelerate MaxClimb 1+F 793 180,4 A340-211 ICAO_A 2 5 Accelerate MaxClimb 1 855,5 208,3 A340-211 ICAO_A 2 6 Accelerate MaxClimb ZERO 999,1 228,5 A340-211 ICAO_A 2 7 Accelerate MaxClimb ZERO 1 109,1 250 A340-211 ICAO_A 2 8 Climb MaxClimb ZERO 5 500 A340-211 ICAO_A 2 9 Climb MaxClimb ZERO 7 500 A340-211 ICAO_A 2 10 Climb MaxClimb ZERO 10 000 A340-211 ICAO_A 3 1 Takeoff MaxTakeoff 1+FL 168/512 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-211 ICAO_A 3 2 Climb MaxTakeoff 1+F 1 500 A340-211 ICAO_A 3 3 Climb MaxClimb 1+F 3 000 A340-211 ICAO_A 3 4 Accelerate MaxClimb 1+F 754,7 183 A340-211 ICAO_A 3 5 Accelerate MaxClimb 1 820,5 209,4 A340-211 ICAO_A 3 6 Accelerate MaxClimb ZERO 959,1 228,8 A340-211 ICAO_A 3 7 Accelerate MaxClimb ZERO 1 064,5 250 A340-211 ICAO_A 3 8 Climb MaxClimb ZERO 5 500 A340-211 ICAO_A 3 9 Climb MaxClimb ZERO 7 500 A340-211 ICAO_A 3 10 Climb MaxClimb ZERO 10 000 A340-211 ICAO_A 4 1 Takeoff MaxTakeoff 1+F A340-211 ICAO_A 4 2 Climb MaxTakeoff 1+F 1 500 A340-211 ICAO_A 4 3 Climb MaxClimb 1+F 3 000 A340-211 ICAO_A 4 4 Accelerate MaxClimb 1+F 690,8 188,1 A340-211 ICAO_A 4 5 Accelerate MaxClimb 1 763 212,2 A340-211 ICAO_A 4 6 Accelerate MaxClimb ZERO 893,8 230 A340-211 ICAO_A 4 7 Accelerate MaxClimb ZERO 991,5 250 A340-211 ICAO_A 4 8 Climb MaxClimb ZERO 5 500 A340-211 ICAO_A 4 9 Climb MaxClimb ZERO 7 500 A340-211 ICAO_A 4 10 Climb MaxClimb ZERO 10 000 A340-211 ICAO_A 5 1 Takeoff MaxTakeoff 1+F1.7.2015 EN Official Journal of the European Union L 168/513 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-211 ICAO_A 5 2 Climb MaxTakeoff 1+F 1 500 A340-211 ICAO_A 5 3 Climb MaxClimb 1+F 3 000 A340-211 ICAO_A 5 4 Accelerate MaxClimb 1+F 621,5 194,8 A340-211 ICAO_A 5 5 Accelerate MaxClimb 1 695,5 216,1 A340-211 ICAO_A 5 6 Accelerate MaxClimb ZERO 818,3 232,2 A340-211 ICAO_A 5 7 Accelerate MaxClimb ZERO 906,8 250 A340-211 ICAO_A 5 8 Climb MaxClimb ZERO 5 500 A340-211 ICAO_A 5 9 Climb MaxClimb ZERO 7 500 A340-211 ICAO_A 5 10 Climb MaxClimb ZERO 10 000 A340-211 ICAO_A 6 1 Takeoff MaxTakeoff 1+F A340-211 ICAO_A 6 2 Climb MaxTakeoff 1+F 1 500 A340-211 ICAO_A 6 3 Climb MaxClimb 1+F 3 000 A340-211 ICAO_A 6 4 Accelerate MaxClimb 1+F 555,3 199,2 A340-211 ICAO_A 6 5 Accelerate MaxClimb 1 627,4 218,1 A340-211 ICAO_A 6 6 Accelerate MaxClimb ZERO 742,5 232,6 A340-211 ICAO_A 6 7 Accelerate MaxClimb ZERO 824,1 250 A340-211 ICAO_A 6 8 Climb MaxClimb ZERO 5 500 A340-211 ICAO_A 6 9 Climb MaxClimb ZERO 7 500 A340-211 ICAO_A 6 10 Climb MaxClimb ZERO 10 000 A340-211 ICAO_A 7 1 Takeoff MaxTakeoff 1+FL 168/514 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-211 ICAO_A 7 2 Climb MaxTakeoff 1+F 1 500 A340-211 ICAO_A 7 3 Climb MaxClimb 1+F 3 000 A340-211 ICAO_A 7 4 Accelerate MaxClimb 1+F 388,7 199,2 A340-211 ICAO_A 7 5 Accelerate MaxClimb 1 444,2 212,8 A340-211 ICAO_A 7 6 Accelerate MaxClimb 1 500,7 224,8 A340-211 ICAO_A 7 7 Accelerate MaxClimb ZERO 555,6 235,4 A340-211 ICAO_A 7 8 Accelerate MaxClimb ZERO 623 250 A340-211 ICAO_A 7 9 Climb MaxClimb ZERO 5 500 A340-211 ICAO_A 7 10 Climb MaxClimb ZERO 7 500 A340-211 ICAO_A 7 11 Climb MaxClimb ZERO 10 000 A340-211 ICAO_B 1 1 Takeoff MaxTakeoff 1+F A340-211 ICAO_B 1 2 Climb MaxTakeoff 1+F 1 000 A340-211 ICAO_B 1 3 Accelerate MaxTakeoff 1+F 1 019,3 177,6 A340-211 ICAO_B 1 4 Accelerate MaxTakeoff 1 1 101,1 215,2 A340-211 ICAO_B 1 5 Climb MaxClimb ZERO 3 000 A340-211 ICAO_B 1 6 Accelerate MaxClimb ZERO 1 165,6 250 A340-211 ICAO_B 1 7 Climb MaxClimb ZERO 5 500 A340-211 ICAO_B 1 8 Climb MaxClimb ZERO 7 500 A340-211 ICAO_B 1 9 Climb MaxClimb ZERO 10 000 A340-211 ICAO_B 2 1 Takeoff MaxTakeoff 1+F1.7.2015 EN Official Journal of the European Union L 168/515 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-211 ICAO_B 2 2 Climb MaxTakeoff 1+F 1 000 A340-211 ICAO_B 2 3 Accelerate MaxTakeoff 1+F 973,9 180,5 A340-211 ICAO_B 2 4 Accelerate MaxTakeoff 1 1 061,1 216,3 A340-211 ICAO_B 2 5 Climb MaxClimb ZERO 3 000 A340-211 ICAO_B 2 6 Accelerate MaxClimb ZERO 1 120,6 250 A340-211 ICAO_B 2 7 Climb MaxClimb ZERO 5 500 A340-211 ICAO_B 2 8 Climb MaxClimb ZERO 7 500 A340-211 ICAO_B 2 9 Climb MaxClimb ZERO 10 000 A340-211 ICAO_B 3 1 Takeoff MaxTakeoff 1+F A340-211 ICAO_B 3 2 Climb MaxTakeoff 1+F 1 000 A340-211 ICAO_B 3 3 Accelerate MaxTakeoff 1+F 930,2 183,1 A340-211 ICAO_B 3 4 Accelerate MaxTakeoff 1 1 021,2 217,3 A340-211 ICAO_B 3 5 Climb MaxClimb ZERO 3 000 A340-211 ICAO_B 3 6 Accelerate MaxClimb ZERO 1 076,1 250 A340-211 ICAO_B 3 7 Climb MaxClimb ZERO 5 500 A340-211 ICAO_B 3 8 Climb MaxClimb ZERO 7 500 A340-211 ICAO_B 3 9 Climb MaxClimb ZERO 10 000 A340-211 ICAO_B 4 1 Takeoff MaxTakeoff 1+F A340-211 ICAO_B 4 2 Climb MaxTakeoff 1+F 1 000 A340-211 ICAO_B 4 3 Accelerate MaxTakeoff 1+F 860,1 188,2L 168/516 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-211 ICAO_B 4 4 Accelerate MaxTakeoff 1 955,9 219,5 A340-211 ICAO_B 4 5 Climb MaxClimb ZERO 3 000 A340-211 ICAO_B 4 6 Accelerate MaxClimb ZERO 1 003,9 250 A340-211 ICAO_B 4 7 Climb MaxClimb ZERO 5 500 A340-211 ICAO_B 4 8 Climb MaxClimb ZERO 7 500 A340-211 ICAO_B 4 9 Climb MaxClimb ZERO 10 000 A340-211 ICAO_B 5 1 Takeoff MaxTakeoff 1+F A340-211 ICAO_B 5 2 Climb MaxTakeoff 1+F 1 000 A340-211 ICAO_B 5 3 Accelerate MaxTakeoff 1+F 779,4 194,9 A340-211 ICAO_B 5 4 Accelerate MaxTakeoff 1 879,4 222,9 A340-211 ICAO_B 5 5 Climb MaxClimb ZERO 3 000 A340-211 ICAO_B 5 6 Accelerate MaxClimb ZERO 920,2 250 A340-211 ICAO_B 5 7 Climb MaxClimb ZERO 5 500 A340-211 ICAO_B 5 8 Climb MaxClimb ZERO 7 500 A340-211 ICAO_B 5 9 Climb MaxClimb ZERO 10 000 A340-211 ICAO_B 6 1 Takeoff MaxTakeoff 1+F A340-211 ICAO_B 6 2 Climb MaxTakeoff 1+F 1 000 A340-211 ICAO_B 6 3 Accelerate MaxTakeoff 1+F 705,2 199,2 A340-211 ICAO_B 6 4 Accelerate MaxTakeoff 1 802 224,4 A340-211 ICAO_B 6 5 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/517 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-211 ICAO_B 6 6 Accelerate MaxClimb ZERO 836,4 250 A340-211 ICAO_B 6 7 Climb MaxClimb ZERO 5 500 A340-211 ICAO_B 6 8 Climb MaxClimb ZERO 7 500 A340-211 ICAO_B 6 9 Climb MaxClimb ZERO 10 000 A340-211 ICAO_B 7 1 Takeoff MaxTakeoff 1+F A340-211 ICAO_B 7 2 Climb MaxTakeoff 1+F 1 000 A340-211 ICAO_B 7 3 Accelerate MaxTakeoff 1+F 519,8 199,2 A340-211 ICAO_B 7 4 Accelerate MaxTakeoff 1 591,5 218,2 A340-211 ICAO_B 7 5 Accelerate MaxTakeoff 1 653,7 223,4 A340-211 ICAO_B 7 6 Climb MaxClimb ZERO 3 000 A340-211 ICAO_B 7 7 Accelerate MaxClimb ZERO 622,6 250 A340-211 ICAO_B 7 8 Climb MaxClimb ZERO 5 500 A340-211 ICAO_B 7 9 Climb MaxClimb ZERO 7 500 A340-211 ICAO_B 7 10 Climb MaxClimb ZERO 10 000 A340-642 DEFAULT 1 1 Takeoff MaxTakeoff 1+F A340-642 DEFAULT 1 2 Accelerate MaxTakeoff 1+F 1 518,1 178,9 A340-642 DEFAULT 1 3 Climb MaxTakeoff 1+F 1 000 A340-642 DEFAULT 1 4 Accelerate MaxTakeoff 1+F 1 534,7 191,5 A340-642 DEFAULT 1 5 Accelerate MaxTakeoff 1 1 638,4 240,3 A340-642 DEFAULT 1 6 Climb MaxClimb ZERO 3 000L 168/518 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-642 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 461,4 250 A340-642 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 A340-642 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 A340-642 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 A340-642 DEFAULT 2 1 Takeoff MaxTakeoff 1+F A340-642 DEFAULT 2 2 Accelerate MaxTakeoff 1+F 1 481 178,3 A340-642 DEFAULT 2 3 Climb MaxTakeoff 1+F 1 000 A340-642 DEFAULT 2 4 Accelerate MaxTakeoff 1+F 1 452,6 194,6 A340-642 DEFAULT 2 5 Accelerate MaxTakeoff 1 1 595,8 241,6 A340-642 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 A340-642 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 415 250 A340-642 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 A340-642 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 A340-642 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 A340-642 DEFAULT 3 1 Takeoff MaxTakeoff 1+F A340-642 DEFAULT 3 2 Accelerate MaxTakeoff 1+F 1 444,1 177,7 A340-642 DEFAULT 3 3 Climb MaxTakeoff 1+F 1 000 A340-642 DEFAULT 3 4 Accelerate MaxTakeoff 1+F 1 382,6 197,7 A340-642 DEFAULT 3 5 Accelerate MaxTakeoff 1 1 554,9 243 A340-642 DEFAULT 3 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/519 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-642 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 374,5 250 A340-642 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 A340-642 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 A340-642 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 A340-642 DEFAULT 4 1 Takeoff MaxTakeoff 1+F A340-642 DEFAULT 4 2 Accelerate MaxTakeoff 1+F 1 383,2 176,9 A340-642 DEFAULT 4 3 Climb MaxTakeoff 1+F 1 000 A340-642 DEFAULT 4 4 Accelerate MaxTakeoff 1+F 1 292 203 A340-642 DEFAULT 4 5 Accelerate MaxTakeoff 1 1 478,5 245,2 A340-642 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 A340-642 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 320,3 250 A340-642 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 A340-642 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 A340-642 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 A340-642 DEFAULT 5 1 Takeoff MaxTakeoff 1+F A340-642 DEFAULT 5 2 Accelerate MaxTakeoff 1+F 1 327,9 180,6 A340-642 DEFAULT 5 3 Climb MaxTakeoff 1+F 1 000 A340-642 DEFAULT 5 4 Accelerate MaxTakeoff 1+F 1 209,7 210,1 A340-642 DEFAULT 5 5 Accelerate MaxTakeoff 1 1 373,5 248,4 A340-642 DEFAULT 5 6 Climb MaxClimb ZERO 3 000L 168/520 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-642 DEFAULT 5 7 Accelerate MaxClimb ZERO 1 410,4 250 A340-642 DEFAULT 5 8 Climb MaxClimb ZERO 5 500 A340-642 DEFAULT 5 9 Climb MaxClimb ZERO 7 500 A340-642 DEFAULT 5 10 Climb MaxClimb ZERO 10 000 A340-642 DEFAULT 6 1 Takeoff MaxTakeoff 1+F A340-642 DEFAULT 6 2 Accelerate MaxTakeoff 1+F 1 185 185,4 A340-642 DEFAULT 6 3 Climb MaxTakeoff 1+F 1 000 A340-642 DEFAULT 6 4 Accelerate MaxTakeoff 1+F 1 126,6 214,9 A340-642 DEFAULT 6 5 Accelerate MaxTakeoff 1 1 268,8 249,8 A340-642 DEFAULT 6 6 Climb MaxClimb ZERO 3 000 A340-642 DEFAULT 6 7 Accelerate MaxClimb ZERO 2 048,9 250 A340-642 DEFAULT 6 8 Climb MaxClimb ZERO 5 500 A340-642 DEFAULT 6 9 Climb MaxClimb ZERO 7 500 A340-642 DEFAULT 6 10 Climb MaxClimb ZERO 10 000 A340-642 DEFAULT 7 1 Takeoff MaxTakeoff 1+F A340-642 DEFAULT 7 2 Climb MaxTakeoff 1+F 1 000 A340-642 DEFAULT 7 3 Accelerate MaxTakeoff 1+F 868,2 214,9 A340-642 DEFAULT 7 4 Accelerate MaxTakeoff 1 929,6 241,1 A340-642 DEFAULT 7 5 Climb MaxClimb ZERO 3 000 A340-642 DEFAULT 7 6 Accelerate MaxClimb ZERO 748,4 2501.7.2015 EN Official Journal of the European Union L 168/521 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-642 DEFAULT 7 7 Climb MaxClimb ZERO 5 500 A340-642 DEFAULT 7 8 Climb MaxClimb ZERO 7 500 A340-642 DEFAULT 7 9 Climb MaxClimb ZERO 10 000 A340-642 ICAO_A 1 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_A 1 2 Accelerate MaxTakeoff 1+F 1 518,1 178,9 A340-642 ICAO_A 1 3 Climb MaxTakeoff 1+F 1 500 A340-642 ICAO_A 1 4 Climb MaxClimb 1+F 3 000 A340-642 ICAO_A 1 5 Accelerate MaxClimb 1+F 1 110,7 191,6 A340-642 ICAO_A 1 6 Accelerate MaxClimb 1 1 176,6 225,9 A340-642 ICAO_A 1 7 Accelerate MaxClimb 1 1 342,4 250 A340-642 ICAO_A 1 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_A 1 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_A 1 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_A 2 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_A 2 2 Accelerate MaxTakeoff 1+F 1 481 178,3 A340-642 ICAO_A 2 3 Climb MaxTakeoff 1+F 1 500 A340-642 ICAO_A 2 4 Climb MaxClimb 1+F 3 000 A340-642 ICAO_A 2 5 Accelerate MaxClimb 1+F 1 053,1 194,6 A340-642 ICAO_A 2 6 Accelerate MaxClimb 1 1 135,6 227,4 A340-642 ICAO_A 2 7 Accelerate MaxClimb 1 1 292,5 250L 168/522 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-642 ICAO_A 2 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_A 2 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_A 2 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_A 3 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_A 3 2 Accelerate MaxTakeoff 1+F 1 444,1 177,7 A340-642 ICAO_A 3 3 Climb MaxTakeoff 1+F 1 500 A340-642 ICAO_A 3 4 Climb MaxClimb 1+F 3 000 A340-642 ICAO_A 3 5 Accelerate MaxClimb 1+F 1 002,2 197,7 A340-642 ICAO_A 3 6 Accelerate MaxClimb 1 1 095,6 228,9 A340-642 ICAO_A 3 7 Accelerate MaxClimb 1 1 243,9 250 A340-642 ICAO_A 3 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_A 3 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_A 3 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_A 4 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_A 4 2 Accelerate MaxTakeoff 1+F 1 383,2 176,9 A340-642 ICAO_A 4 3 Climb MaxTakeoff 1+F 1 500 A340-642 ICAO_A 4 4 Climb MaxClimb 1+F 3 000 A340-642 ICAO_A 4 5 Accelerate MaxClimb 1+F 925,2 203,3 A340-642 ICAO_A 4 6 Accelerate MaxClimb 1 1 029,9 232 A340-642 ICAO_A 4 7 Accelerate MaxClimb 1 1 164 2501.7.2015 EN Official Journal of the European Union L 168/523 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-642 ICAO_A 4 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_A 4 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_A 4 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_A 5 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_A 5 2 Accelerate MaxTakeoff 1+F 1 327,9 180,6 A340-642 ICAO_A 5 3 Climb MaxTakeoff 1+F 1 500 A340-642 ICAO_A 5 4 Climb MaxClimb 1+F 3 000 A340-642 ICAO_A 5 5 Accelerate MaxClimb 1+F 848,8 210,8 A340-642 ICAO_A 5 6 Accelerate MaxClimb 1 950,4 236,5 A340-642 ICAO_A 5 7 Accelerate MaxClimb 1 1 067,5 250 A340-642 ICAO_A 5 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_A 5 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_A 5 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_A 6 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_A 6 2 Accelerate MaxTakeoff 1+F 1 185 185,4 A340-642 ICAO_A 6 3 Climb MaxTakeoff 1+F 1 500 A340-642 ICAO_A 6 4 Climb MaxClimb 1+F 3 000 A340-642 ICAO_A 6 5 Accelerate MaxClimb 1+F 780,5 219 A340-642 ICAO_A 6 6 Accelerate MaxClimb 1 875,9 242 A340-642 ICAO_A 6 7 Accelerate MaxClimb 1 975,3 250L 168/524 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-642 ICAO_A 6 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_A 6 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_A 6 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_A 7 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_A 7 2 Climb MaxTakeoff 1+F 1 500 A340-642 ICAO_A 7 3 Climb MaxClimb 1+F 3 000 A340-642 ICAO_A 7 4 Accelerate MaxClimb 1+F 556,7 214,9 A340-642 ICAO_A 7 5 Accelerate MaxClimb 1 601,9 231,3 A340-642 ICAO_A 7 6 Accelerate MaxClimb ZERO 681,8 244 A340-642 ICAO_A 7 7 Accelerate MaxClimb ZERO 729,1 250 A340-642 ICAO_A 7 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_A 7 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_A 7 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_B 1 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_B 1 2 Accelerate MaxTakeoff 1+F 1 518,1 178,9 A340-642 ICAO_B 1 3 Climb MaxTakeoff 1+F 1 000 A340-642 ICAO_B 1 4 Accelerate MaxTakeoff 1+F 1 534,7 191,5 A340-642 ICAO_B 1 5 Accelerate MaxTakeoff 1 1 638,4 240,3 A340-642 ICAO_B 1 6 Climb MaxClimb ZERO 3 000 A340-642 ICAO_B 1 7 Accelerate MaxClimb ZERO 1 461,4 2501.7.2015 EN Official Journal of the European Union L 168/525 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-642 ICAO_B 1 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_B 1 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_B 1 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_B 2 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_B 2 2 Accelerate MaxTakeoff 1+F 1 481 178,3 A340-642 ICAO_B 2 3 Climb MaxTakeoff 1+F 1 000 A340-642 ICAO_B 2 4 Accelerate MaxTakeoff 1+F 1 452,6 194,6 A340-642 ICAO_B 2 5 Accelerate MaxTakeoff 1 1 595,8 241,6 A340-642 ICAO_B 2 6 Climb MaxClimb ZERO 3 000 A340-642 ICAO_B 2 7 Accelerate MaxClimb ZERO 1 415 250 A340-642 ICAO_B 2 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_B 2 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_B 2 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_B 3 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_B 3 2 Accelerate MaxTakeoff 1+F 1 444,1 177,7 A340-642 ICAO_B 3 3 Climb MaxTakeoff 1+F 1 000 A340-642 ICAO_B 3 4 Accelerate MaxTakeoff 1+F 1 382,6 197,7 A340-642 ICAO_B 3 5 Accelerate MaxTakeoff 1 1 554,9 243 A340-642 ICAO_B 3 6 Climb MaxClimb ZERO 3 000 A340-642 ICAO_B 3 7 Accelerate MaxClimb ZERO 1 374,5 250L 168/526 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-642 ICAO_B 3 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_B 3 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_B 3 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_B 4 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_B 4 2 Accelerate MaxTakeoff 1+F 1 383,2 176,9 A340-642 ICAO_B 4 3 Climb MaxTakeoff 1+F 1 000 A340-642 ICAO_B 4 4 Accelerate MaxTakeoff 1+F 1 292 203 A340-642 ICAO_B 4 5 Accelerate MaxTakeoff 1 1 478,5 245,2 A340-642 ICAO_B 4 6 Climb MaxClimb ZERO 3 000 A340-642 ICAO_B 4 7 Accelerate MaxClimb ZERO 1 320,3 250 A340-642 ICAO_B 4 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_B 4 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_B 4 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_B 5 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_B 5 2 Accelerate MaxTakeoff 1+F 1 327,9 180,6 A340-642 ICAO_B 5 3 Climb MaxTakeoff 1+F 1 000 A340-642 ICAO_B 5 4 Accelerate MaxTakeoff 1+F 1 209,7 210,1 A340-642 ICAO_B 5 5 Accelerate MaxTakeoff 1 1 373,5 248,4 A340-642 ICAO_B 5 6 Climb MaxClimb ZERO 3 000 A340-642 ICAO_B 5 7 Accelerate MaxClimb ZERO 1 410,4 2501.7.2015 EN Official Journal of the European Union L 168/527 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-642 ICAO_B 5 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_B 5 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_B 5 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_B 6 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_B 6 2 Accelerate MaxTakeoff 1+F 1 185 185,4 A340-642 ICAO_B 6 3 Climb MaxTakeoff 1+F 1 000 A340-642 ICAO_B 6 4 Accelerate MaxTakeoff 1+F 1 126,6 214,9 A340-642 ICAO_B 6 5 Accelerate MaxTakeoff 1 1 268,8 249,8 A340-642 ICAO_B 6 6 Climb MaxClimb ZERO 3 000 A340-642 ICAO_B 6 7 Accelerate MaxClimb ZERO 2 048,9 250 A340-642 ICAO_B 6 8 Climb MaxClimb ZERO 5 500 A340-642 ICAO_B 6 9 Climb MaxClimb ZERO 7 500 A340-642 ICAO_B 6 10 Climb MaxClimb ZERO 10 000 A340-642 ICAO_B 7 1 Takeoff MaxTakeoff 1+F A340-642 ICAO_B 7 2 Climb MaxTakeoff 1+F 1 000 A340-642 ICAO_B 7 3 Accelerate MaxTakeoff 1+F 868,2 214,9 A340-642 ICAO_B 7 4 Accelerate MaxTakeoff 1 929,6 241,1 A340-642 ICAO_B 7 5 Climb MaxClimb ZERO 3 000 A340-642 ICAO_B 7 6 Accelerate MaxClimb ZERO 748,4 250 A340-642 ICAO_B 7 7 Climb MaxClimb ZERO 5 500L 168/528 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A340-642 ICAO_B 7 8 Climb MaxClimb ZERO 7 500 A340-642 ICAO_B 7 9 Climb MaxClimb ZERO 10 000 A380-841 DEFAULT 1 1 Takeoff MaxTakeoff D_1+F A380-841 DEFAULT 1 2 Climb MaxTakeoff D_1+F 1 000 A380-841 DEFAULT 1 3 Accelerate MaxTakeoff D_1+F 1 085 175,1 A380-841 DEFAULT 1 4 Accelerate MaxTakeoff D_1 1 306 238,9 A380-841 DEFAULT 1 5 Climb MaxClimb D_1 3 000 A380-841 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 497,8 250 A380-841 DEFAULT 1 7 Climb MaxClimb ZERO 10 000 A380-841 DEFAULT 2 1 Takeoff MaxTakeoff D_1+F A380-841 DEFAULT 2 2 Climb MaxTakeoff D_1+F 1 000 A380-841 DEFAULT 2 3 Accelerate MaxTakeoff D_1+F 1 054 177,6 A380-841 DEFAULT 2 4 Accelerate MaxTakeoff D_1 1 262,8 238,9 A380-841 DEFAULT 2 5 Climb MaxClimb D_1 3 000 A380-841 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 444,8 250 A380-841 DEFAULT 2 7 Climb MaxClimb ZERO 10 000 A380-841 DEFAULT 3 1 Takeoff MaxTakeoff D_1+F A380-841 DEFAULT 3 2 Climb MaxTakeoff D_1+F 1 000 A380-841 DEFAULT 3 3 Accelerate MaxTakeoff D_1+F 1 022,1 180,2 A380-841 DEFAULT 3 4 Accelerate MaxTakeoff D_1 1 220,9 239,11.7.2015 EN Official Journal of the European Union L 168/529 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-841 DEFAULT 3 5 Climb MaxClimb D_1 3 000 A380-841 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 394,3 250 A380-841 DEFAULT 3 7 Climb MaxClimb ZERO 10 000 A380-841 DEFAULT 4 1 Takeoff MaxTakeoff D_1+F A380-841 DEFAULT 4 2 Climb MaxTakeoff D_1+F 1 000 A380-841 DEFAULT 4 3 Accelerate MaxTakeoff D_1+F 975,4 184,8 A380-841 DEFAULT 4 4 Accelerate MaxTakeoff D_1 1 152,5 239,6 A380-841 DEFAULT 4 5 Climb MaxClimb D_1 3 000 A380-841 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 313,6 250 A380-841 DEFAULT 4 7 Climb MaxClimb ZERO 10 000 A380-841 DEFAULT 5 1 Takeoff MaxTakeoff D_1+F A380-841 DEFAULT 5 2 Climb MaxTakeoff D_1+F 1 000 A380-841 DEFAULT 5 3 Accelerate MaxTakeoff D_1+F 908,1 190,6 A380-841 DEFAULT 5 4 Accelerate MaxTakeoff D_1 1 072,2 240,8 A380-841 DEFAULT 5 5 Climb MaxClimb D_1 3 000 A380-841 DEFAULT 5 6 Accelerate MaxClimb ZERO 1 220,7 250 A380-841 DEFAULT 5 7 Climb MaxClimb ZERO 10 000 A380-841 DEFAULT 6 1 Takeoff MaxTakeoff D_1+F A380-841 DEFAULT 6 2 Climb MaxTakeoff D_1+F 1 000 A380-841 DEFAULT 6 3 Accelerate MaxTakeoff D_1+F 843 196,7L 168/530 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-841 DEFAULT 6 4 Accelerate MaxTakeoff D_1 994,4 242,4 A380-841 DEFAULT 6 5 Climb MaxClimb D_1 3 000 A380-841 DEFAULT 6 6 Accelerate MaxClimb ZERO 1 134,1 250 A380-841 DEFAULT 6 7 Climb MaxClimb ZERO 10 000 A380-841 DEFAULT 7 1 Takeoff MaxTakeoff D_1+F A380-841 DEFAULT 7 2 Climb MaxTakeoff D_1+F 1 000 A380-841 DEFAULT 7 3 Accelerate MaxTakeoff D_1+F 783 202,7 A380-841 DEFAULT 7 4 Accelerate MaxTakeoff D_1 925 244,4 A380-841 DEFAULT 7 5 Climb MaxClimb D_1 3 000 A380-841 DEFAULT 7 6 Accelerate MaxClimb ZERO 1 065,1 250 A380-841 DEFAULT 7 7 Climb MaxClimb ZERO 10 000 A380-841 DEFAULT 8 1 Takeoff MaxTakeoff D_1+F A380-841 DEFAULT 8 2 Climb MaxTakeoff D_1+F 1 000 A380-841 DEFAULT 8 3 Accelerate MaxTakeoff D_1+F 622,4 220 A380-841 DEFAULT 8 4 Accelerate MaxTakeoff D_1 744,8 251,7 A380-841 DEFAULT 8 5 Climb MaxClimb D_1 3 000 A380-841 DEFAULT 8 6 Climb MaxClimb ZERO 10 000 A380-841 ICAO_A 1 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_A 1 2 Climb MaxTakeoff D_1+F 1 500 A380-841 ICAO_A 1 3 Climb MaxClimb D_1+F 3 0001.7.2015 EN Official Journal of the European Union L 168/531 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-841 ICAO_A 1 4 Accelerate MaxClimb D_1 1 049,1 175,1 A380-841 ICAO_A 1 5 Accelerate MaxClimb D_1 1 257,9 233,9 A380-841 ICAO_A 1 6 Accelerate MaxClimb ZERO 1 403,3 250 A380-841 ICAO_A 1 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_A 2 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_A 2 2 Climb MaxTakeoff D_1+F 1 500 A380-841 ICAO_A 2 3 Climb MaxClimb D_1+F 3 000 A380-841 ICAO_A 2 4 Accelerate MaxClimb D_1 1 005,4 177,7 A380-841 ICAO_A 2 5 Accelerate MaxClimb D_1 1 217,2 234,1 A380-841 ICAO_A 2 6 Accelerate MaxClimb ZERO 1 355,3 250 A380-841 ICAO_A 2 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_A 3 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_A 3 2 Climb MaxTakeoff D_1+F 1 500 A380-841 ICAO_A 3 3 Climb MaxClimb D_1+F 3 000 A380-841 ICAO_A 3 4 Accelerate MaxClimb D_1 965,1 180,3 A380-841 ICAO_A 3 5 Accelerate MaxClimb D_1 1 177,8 234,5 A380-841 ICAO_A 3 6 Accelerate MaxClimb ZERO 1 308,6 250 A380-841 ICAO_A 3 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_A 4 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_A 4 2 Climb MaxTakeoff D_1+F 1 500L 168/532 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-841 ICAO_A 4 3 Climb MaxClimb D_1+F 3 000 A380-841 ICAO_A 4 4 Accelerate MaxClimb D_1 912,3 184,9 A380-841 ICAO_A 4 5 Accelerate MaxClimb D_1 1 113,9 235,4 A380-841 ICAO_A 4 6 Accelerate MaxClimb ZERO 1 231,9 250 A380-841 ICAO_A 4 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_A 5 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_A 5 2 Climb MaxTakeoff D_1+F 1 500 A380-841 ICAO_A 5 3 Climb MaxClimb D_1+F 3 000 A380-841 ICAO_A 5 4 Accelerate MaxClimb D_1 850,1 190,8 A380-841 ICAO_A 5 5 Accelerate MaxClimb D_1 1 038,8 237,1 A380-841 ICAO_A 5 6 Accelerate MaxClimb ZERO 1 141,2 250 A380-841 ICAO_A 5 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_A 6 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_A 6 2 Climb MaxTakeoff D_1+F 1 500 A380-841 ICAO_A 6 3 Climb MaxClimb D_1+F 3 000 A380-841 ICAO_A 6 4 Accelerate MaxClimb D_1 789,5 196,9 A380-841 ICAO_A 6 5 Accelerate MaxClimb D_1 965,9 239,1 A380-841 ICAO_A 6 6 Accelerate MaxClimb ZERO 1 053 250 A380-841 ICAO_A 6 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_A 7 1 Takeoff MaxTakeoff D_1+F1.7.2015 EN Official Journal of the European Union L 168/533 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-841 ICAO_A 7 2 Climb MaxTakeoff D_1+F 1 500 A380-841 ICAO_A 7 3 Climb MaxClimb D_1+F 3 000 A380-841 ICAO_A 7 4 Accelerate MaxClimb D_1 735,4 203,1 A380-841 ICAO_A 7 5 Accelerate MaxClimb D_1 900,3 241,6 A380-841 ICAO_A 7 6 Accelerate MaxClimb ZERO 973,7 250 A380-841 ICAO_A 7 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_A 8 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_A 8 2 Climb MaxTakeoff D_1+F 1 500 A380-841 ICAO_A 8 3 Climb MaxClimb D_1+F 3 000 A380-841 ICAO_A 8 4 Accelerate MaxClimb D_1 587,9 220 A380-841 ICAO_A 8 5 Accelerate MaxClimb D_1 722,8 249,2 A380-841 ICAO_A 8 6 Accelerate MaxClimb ZERO 762,6 250 A380-841 ICAO_A 8 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_B 1 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_B 1 2 Climb MaxTakeoff D_1+F 1 000 A380-841 ICAO_B 1 3 Accelerate MaxTakeoff D_1+F 1 085 175,1 A380-841 ICAO_B 1 4 Accelerate MaxTakeoff D_1 1 306 238,9 A380-841 ICAO_B 1 5 Climb MaxClimb D_1 3 000 A380-841 ICAO_B 1 6 Accelerate MaxClimb ZERO 1 497,8 250 A380-841 ICAO_B 1 7 Climb MaxClimb ZERO 10 000L 168/534 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-841 ICAO_B 2 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_B 2 2 Climb MaxTakeoff D_1+F 1 000 A380-841 ICAO_B 2 3 Accelerate MaxTakeoff D_1+F 1 054 177,6 A380-841 ICAO_B 2 4 Accelerate MaxTakeoff D_1 1 262,8 238,9 A380-841 ICAO_B 2 5 Climb MaxClimb D_1 3 000 A380-841 ICAO_B 2 6 Accelerate MaxClimb ZERO 1 444,8 250 A380-841 ICAO_B 2 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_B 3 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_B 3 2 Climb MaxTakeoff D_1+F 1 000 A380-841 ICAO_B 3 3 Accelerate MaxTakeoff D_1+F 1 022,1 180,2 A380-841 ICAO_B 3 4 Accelerate MaxTakeoff D_1 1 220,9 239,1 A380-841 ICAO_B 3 5 Climb MaxClimb D_1 3 000 A380-841 ICAO_B 3 6 Accelerate MaxClimb ZERO 1 394,3 250 A380-841 ICAO_B 3 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_B 4 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_B 4 2 Climb MaxTakeoff D_1+F 1 000 A380-841 ICAO_B 4 3 Accelerate MaxTakeoff D_1+F 975,4 184,8 A380-841 ICAO_B 4 4 Accelerate MaxTakeoff D_1 1 152,5 239,6 A380-841 ICAO_B 4 5 Climb MaxClimb D_1 3 000 A380-841 ICAO_B 4 6 Accelerate MaxClimb ZERO 1 313,6 2501.7.2015 EN Official Journal of the European Union L 168/535 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-841 ICAO_B 4 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_B 5 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_B 5 2 Climb MaxTakeoff D_1+F 1 000 A380-841 ICAO_B 5 3 Accelerate MaxTakeoff D_1+F 908,1 190,6 A380-841 ICAO_B 5 4 Accelerate MaxTakeoff D_1 1 072,2 240,8 A380-841 ICAO_B 5 5 Climb MaxClimb D_1 3 000 A380-841 ICAO_B 5 6 Accelerate MaxClimb ZERO 1 220,7 250 A380-841 ICAO_B 5 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_B 6 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_B 6 2 Climb MaxTakeoff D_1+F 1 000 A380-841 ICAO_B 6 3 Accelerate MaxTakeoff D_1+F 843 196,7 A380-841 ICAO_B 6 4 Accelerate MaxTakeoff D_1 994,4 242,4 A380-841 ICAO_B 6 5 Climb MaxClimb D_1 3 000 A380-841 ICAO_B 6 6 Accelerate MaxClimb ZERO 1 134,1 250 A380-841 ICAO_B 6 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_B 7 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_B 7 2 Climb MaxTakeoff D_1+F 1 000 A380-841 ICAO_B 7 3 Accelerate MaxTakeoff D_1+F 783 202,7 A380-841 ICAO_B 7 4 Accelerate MaxTakeoff D_1 925 244,4 A380-841 ICAO_B 7 5 Climb MaxClimb D_1 3 000L 168/536 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-841 ICAO_B 7 6 Accelerate MaxClimb ZERO 1 065,1 250 A380-841 ICAO_B 7 7 Climb MaxClimb ZERO 10 000 A380-841 ICAO_B 8 1 Takeoff MaxTakeoff D_1+F A380-841 ICAO_B 8 2 Climb MaxTakeoff D_1+F 1 000 A380-841 ICAO_B 8 3 Accelerate MaxTakeoff D_1+F 622,4 220 A380-841 ICAO_B 8 4 Accelerate MaxTakeoff D_1 744,8 251,7 A380-841 ICAO_B 8 5 Climb MaxClimb D_1 3 000 A380-841 ICAO_B 8 6 Climb MaxClimb ZERO 10 000 A380-861 DEFAULT 1 1 Takeoff MaxTakeoff D_1+F A380-861 DEFAULT 1 2 Climb MaxTakeoff D_1+F 1 000 A380-861 DEFAULT 1 3 Accelerate MaxTakeoff D_1+F 1 086 175,1 A380-861 DEFAULT 1 4 Accelerate MaxTakeoff D_1 1 312,2 239,2 A380-861 DEFAULT 1 5 Climb MaxClimb D_1 3 000 A380-861 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 499,1 250 A380-861 DEFAULT 1 7 Climb MaxClimb ZERO 10 000 A380-861 DEFAULT 2 1 Takeoff MaxTakeoff D_1+F A380-861 DEFAULT 2 2 Climb MaxTakeoff D_1+F 1 000 A380-861 DEFAULT 2 3 Accelerate MaxTakeoff D_1+F 1 056 177,6 A380-861 DEFAULT 2 4 Accelerate MaxTakeoff D_1 1 269 239,2 A380-861 DEFAULT 2 5 Climb MaxClimb D_1 3 0001.7.2015 EN Official Journal of the European Union L 168/537 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-861 DEFAULT 2 6 Accelerate MaxClimb ZERO 1 446,4 250 A380-861 DEFAULT 2 7 Climb MaxClimb ZERO 10 000 A380-861 DEFAULT 3 1 Takeoff MaxTakeoff D_1+F A380-861 DEFAULT 3 2 Climb MaxTakeoff D_1+F 1 000 A380-861 DEFAULT 3 3 Accelerate MaxTakeoff D_1+F 1 024,4 180,2 A380-861 DEFAULT 3 4 Accelerate MaxTakeoff D_1 1 226,4 239,2 A380-861 DEFAULT 3 5 Climb MaxClimb D_1 3 000 A380-861 DEFAULT 3 6 Accelerate MaxClimb ZERO 1 394,9 250 A380-861 DEFAULT 3 7 Climb MaxClimb ZERO 10 000 A380-861 DEFAULT 4 1 Takeoff MaxTakeoff D_1+F A380-861 DEFAULT 4 2 Climb MaxTakeoff D_1+F 1 000 A380-861 DEFAULT 4 3 Accelerate MaxTakeoff D_1+F 972,5 184,7 A380-861 DEFAULT 4 4 Accelerate MaxTakeoff D_1 1 158,3 239,8 A380-861 DEFAULT 4 5 Climb MaxClimb D_1 3 000 A380-861 DEFAULT 4 6 Accelerate MaxClimb ZERO 1 315,9 250 A380-861 DEFAULT 4 7 Climb MaxClimb ZERO 10 000 A380-861 DEFAULT 5 1 Takeoff MaxTakeoff D_1+F A380-861 DEFAULT 5 2 Climb MaxTakeoff D_1+F 1 000 A380-861 DEFAULT 5 3 Accelerate MaxTakeoff D_1+F 906,2 190,4 A380-861 DEFAULT 5 4 Accelerate MaxTakeoff D_1 1 080,4 240,9L 168/538 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-861 DEFAULT 5 5 Climb MaxClimb D_1 3 000 A380-861 DEFAULT 5 6 Accelerate MaxClimb ZERO 1 225,2 250 A380-861 DEFAULT 5 7 Climb MaxClimb ZERO 10 000 A380-861 DEFAULT 6 1 Takeoff MaxTakeoff D_1+F A380-861 DEFAULT 6 2 Climb MaxTakeoff D_1+F 1 000 A380-861 DEFAULT 6 3 Accelerate MaxTakeoff D_1+F 840 196,4 A380-861 DEFAULT 6 4 Accelerate MaxTakeoff D_1 1 003 242,5 A380-861 DEFAULT 6 5 Climb MaxClimb D_1 3 000 A380-861 DEFAULT 6 6 Accelerate MaxClimb ZERO 1 139 250 A380-861 DEFAULT 6 7 Climb MaxClimb ZERO 10 000 A380-861 DEFAULT 7 1 Takeoff MaxTakeoff D_1+F A380-861 DEFAULT 7 2 Climb MaxTakeoff D_1+F 1 000 A380-861 DEFAULT 7 3 Accelerate MaxTakeoff D_1+F 777,6 202,7 A380-861 DEFAULT 7 4 Accelerate MaxTakeoff D_1 930,4 244,6 A380-861 DEFAULT 7 5 Climb MaxClimb D_1 3 000 A380-861 DEFAULT 7 6 Accelerate MaxClimb ZERO 1 063,2 250 A380-861 DEFAULT 7 7 Climb MaxClimb ZERO 10 000 A380-861 DEFAULT 8 1 Takeoff MaxTakeoff D_1+F A380-861 DEFAULT 8 2 Climb MaxTakeoff D_1+F 1 000 A380-861 DEFAULT 8 3 Accelerate MaxTakeoff D_1+F 618,5 2201.7.2015 EN Official Journal of the European Union L 168/539 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-861 DEFAULT 8 4 Accelerate MaxTakeoff D_1 746,6 251,8 A380-861 DEFAULT 8 5 Climb MaxClimb D_1 3 000 A380-861 DEFAULT 8 6 Climb MaxClimb ZERO 10 000 A380-861 ICAO_A 1 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_A 1 2 Climb MaxTakeoff D_1+F 1 500 A380-861 ICAO_A 1 3 Climb MaxClimb D_1+F 3 000 A380-861 ICAO_A 1 4 Accelerate MaxClimb D_1 1 057,7 175,1 A380-861 ICAO_A 1 5 Accelerate MaxClimb D_1 1 257,2 233,9 A380-861 ICAO_A 1 6 Accelerate MaxClimb ZERO 1 386,8 250 A380-861 ICAO_A 1 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_A 2 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_A 2 2 Climb MaxTakeoff D_1+F 1 500 A380-861 ICAO_A 2 3 Climb MaxClimb D_1+F 3 000 A380-861 ICAO_A 2 4 Accelerate MaxClimb D_1 1 012,5 177,6 A380-861 ICAO_A 2 5 Accelerate MaxClimb D_1 1 208,1 233,8 A380-861 ICAO_A 2 6 Accelerate MaxClimb ZERO 1 339,4 250 A380-861 ICAO_A 2 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_A 3 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_A 3 2 Climb MaxTakeoff D_1+F 1 500 A380-861 ICAO_A 3 3 Climb MaxClimb D_1+F 3 000L 168/540 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-861 ICAO_A 3 4 Accelerate MaxClimb D_1 970 180,2 A380-861 ICAO_A 3 5 Accelerate MaxClimb D_1 1 168,2 234,1 A380-861 ICAO_A 3 6 Accelerate MaxClimb ZERO 1 293 250 A380-861 ICAO_A 3 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_A 4 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_A 4 2 Climb MaxTakeoff D_1+F 1 500 A380-861 ICAO_A 4 3 Climb MaxClimb D_1+F 3 000 A380-861 ICAO_A 4 4 Accelerate MaxClimb D_1 908,4 184,8 A380-861 ICAO_A 4 5 Accelerate MaxClimb D_1 1 103,5 235 A380-861 ICAO_A 4 6 Accelerate MaxClimb ZERO 1 216,8 250 A380-861 ICAO_A 4 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_A 5 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_A 5 2 Climb MaxTakeoff D_1+F 1 500 A380-861 ICAO_A 5 3 Climb MaxClimb D_1+F 3 000 A380-861 ICAO_A 5 4 Accelerate MaxClimb D_1 847,3 190,5 A380-861 ICAO_A 5 5 Accelerate MaxClimb D_1 1 029,6 236,5 A380-861 ICAO_A 5 6 Accelerate MaxClimb ZERO 1 129,4 250 A380-861 ICAO_A 5 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_A 6 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_A 6 2 Climb MaxTakeoff D_1+F 1 5001.7.2015 EN Official Journal of the European Union L 168/541 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-861 ICAO_A 6 3 Climb MaxClimb D_1+F 3 000 A380-861 ICAO_A 6 4 Accelerate MaxClimb D_1 786 196,7 A380-861 ICAO_A 6 5 Accelerate MaxClimb D_1 955,7 238,5 A380-861 ICAO_A 6 6 Accelerate MaxClimb ZERO 1 041,8 250 A380-861 ICAO_A 6 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_A 7 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_A 7 2 Climb MaxTakeoff D_1+F 1 500 A380-861 ICAO_A 7 3 Climb MaxClimb D_1+F 3 000 A380-861 ICAO_A 7 4 Accelerate MaxClimb D_1 728,1 203,1 A380-861 ICAO_A 7 5 Accelerate MaxClimb D_1 886,1 241,1 A380-861 ICAO_A 7 6 Accelerate MaxClimb ZERO 959,3 250 A380-861 ICAO_A 7 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_A 8 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_A 8 2 Climb MaxTakeoff D_1+F 1 500 A380-861 ICAO_A 8 3 Climb MaxClimb D_1+F 3 000 A380-861 ICAO_A 8 4 Accelerate MaxClimb D_1 577,2 220 A380-861 ICAO_A 8 5 Accelerate MaxClimb D_1 705,6 248,6 A380-861 ICAO_A 8 6 Accelerate MaxClimb ZERO 749,1 250 A380-861 ICAO_A 8 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_B 1 1 Takeoff MaxTakeoff D_1+FL 168/542 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-861 ICAO_B 1 2 Climb MaxTakeoff D_1+F 1 000 A380-861 ICAO_B 1 3 Accelerate MaxTakeoff D_1+F 1 086 175,1 A380-861 ICAO_B 1 4 Accelerate MaxTakeoff D_1 1 312,2 239,2 A380-861 ICAO_B 1 5 Climb MaxClimb D_1 3 000 A380-861 ICAO_B 1 6 Accelerate MaxClimb ZERO 1 499,1 250 A380-861 ICAO_B 1 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_B 2 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_B 2 2 Climb MaxTakeoff D_1+F 1 000 A380-861 ICAO_B 2 3 Accelerate MaxTakeoff D_1+F 1 056 177,6 A380-861 ICAO_B 2 4 Accelerate MaxTakeoff D_1 1 269 239,2 A380-861 ICAO_B 2 5 Climb MaxClimb D_1 3 000 A380-861 ICAO_B 2 6 Accelerate MaxClimb ZERO 1 446,4 250 A380-861 ICAO_B 2 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_B 3 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_B 3 2 Climb MaxTakeoff D_1+F 1 000 A380-861 ICAO_B 3 3 Accelerate MaxTakeoff D_1+F 1 024,4 180,2 A380-861 ICAO_B 3 4 Accelerate MaxTakeoff D_1 1 226,4 239,2 A380-861 ICAO_B 3 5 Climb MaxClimb D_1 3 000 A380-861 ICAO_B 3 6 Accelerate MaxClimb ZERO 1 394,9 250 A380-861 ICAO_B 3 7 Climb MaxClimb ZERO 10 0001.7.2015 EN Official Journal of the European Union L 168/543 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-861 ICAO_B 4 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_B 4 2 Climb MaxTakeoff D_1+F 1 000 A380-861 ICAO_B 4 3 Accelerate MaxTakeoff D_1+F 972,5 184,7 A380-861 ICAO_B 4 4 Accelerate MaxTakeoff D_1 1 158,3 239,8 A380-861 ICAO_B 4 5 Climb MaxClimb D_1 3 000 A380-861 ICAO_B 4 6 Accelerate MaxClimb ZERO 1 315,9 250 A380-861 ICAO_B 4 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_B 5 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_B 5 2 Climb MaxTakeoff D_1+F 1 000 A380-861 ICAO_B 5 3 Accelerate MaxTakeoff D_1+F 906,2 190,4 A380-861 ICAO_B 5 4 Accelerate MaxTakeoff D_1 1 080,4 240,9 A380-861 ICAO_B 5 5 Climb MaxClimb D_1 3 000 A380-861 ICAO_B 5 6 Accelerate MaxClimb ZERO 1 225,2 250 A380-861 ICAO_B 5 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_B 6 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_B 6 2 Climb MaxTakeoff D_1+F 1 000 A380-861 ICAO_B 6 3 Accelerate MaxTakeoff D_1+F 840 196,4 A380-861 ICAO_B 6 4 Accelerate MaxTakeoff D_1 1 003 242,5 A380-861 ICAO_B 6 5 Climb MaxClimb D_1 3 000 A380-861 ICAO_B 6 6 Accelerate MaxClimb ZERO 1 139 250L 168/544 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) A380-861 ICAO_B 6 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_B 7 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_B 7 2 Climb MaxTakeoff D_1+F 1 000 A380-861 ICAO_B 7 3 Accelerate MaxTakeoff D_1+F 777,6 202,7 A380-861 ICAO_B 7 4 Accelerate MaxTakeoff D_1 930,4 244,6 A380-861 ICAO_B 7 5 Climb MaxClimb D_1 3 000 A380-861 ICAO_B 7 6 Accelerate MaxClimb ZERO 1 063,2 250 A380-861 ICAO_B 7 7 Climb MaxClimb ZERO 10 000 A380-861 ICAO_B 8 1 Takeoff MaxTakeoff D_1+F A380-861 ICAO_B 8 2 Climb MaxTakeoff D_1+F 1 000 A380-861 ICAO_B 8 3 Accelerate MaxTakeoff D_1+F 618,5 220 A380-861 ICAO_B 8 4 Accelerate MaxTakeoff D_1 746,6 251,8 A380-861 ICAO_B 8 5 Climb MaxClimb D_1 3 000 A380-861 ICAO_B 8 6 Climb MaxClimb ZERO 10 000 BAC111 DEFAULT 1 1 Takeoff MaxTakeoff 8 BAC111 DEFAULT 1 2 Climb MaxTakeoff 8 1 000 BAC111 DEFAULT 1 3 Accelerate MaxTakeoff 8 1 942 158 BAC111 DEFAULT 1 4 Accelerate MaxTakeoff INT1 1 457 178 BAC111 DEFAULT 1 5 Accelerate MaxClimb INT1 1 000 198 BAC111 DEFAULT 1 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/545 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) BAC111 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 BAC111 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 BAC111 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 BAC111 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 BAC111 DEFAULT 2 1 Takeoff MaxTakeoff 8 BAC111 DEFAULT 2 2 Climb MaxTakeoff 8 1 000 BAC111 DEFAULT 2 3 Accelerate MaxTakeoff 8 1 809 163 BAC111 DEFAULT 2 4 Accelerate MaxTakeoff INT1 1 357 183 BAC111 DEFAULT 2 5 Accelerate MaxClimb INT1 1 000 203 BAC111 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 BAC111 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 BAC111 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 BAC111 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 BAC111 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 BAC111 DEFAULT 3 1 Takeoff MaxTakeoff 8 BAC111 DEFAULT 3 2 Climb MaxTakeoff 8 1 000 BAC111 DEFAULT 3 3 Accelerate MaxTakeoff 8 1 665 169 BAC111 DEFAULT 3 4 Accelerate MaxTakeoff INT1 1 249 189 BAC111 DEFAULT 3 5 Accelerate MaxClimb INT1 1 000 209 BAC111 DEFAULT 3 6 Climb MaxClimb ZERO 3 000L 168/546 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) BAC111 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 BAC111 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 BAC111 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 BAC111 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 BAE146 DEFAULT 1 1 Takeoff MaxTakeoff 18 BAE146 DEFAULT 1 2 Climb MaxTakeoff 18 1 000 BAE146 DEFAULT 1 3 Accelerate MaxTakeoff 18 970 171 BAE146 DEFAULT 1 4 Accelerate MaxClimb ZERO 900 201 BAE146 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 BAE146 DEFAULT 1 6 Accelerate MaxClimb ZERO 900 250 BAE146 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 BAE146 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 BAE146 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 BAE146 DEFAULT 2 1 Takeoff MaxTakeoff 18 BAE146 DEFAULT 2 2 Climb MaxTakeoff 18 1 000 BAE146 DEFAULT 2 3 Accelerate MaxTakeoff 18 801 178 BAE146 DEFAULT 2 4 Accelerate MaxClimb ZERO 750 208 BAE146 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 BAE146 DEFAULT 2 6 Accelerate MaxClimb ZERO 750 250 BAE146 DEFAULT 2 7 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/547 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) BAE146 DEFAULT 2 8 Climb MaxClimb ZERO 7 500 BAE146 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 BAE146 DEFAULT 3 1 Takeoff MaxTakeoff 18 BAE146 DEFAULT 3 2 Climb MaxTakeoff 18 1 000 BAE146 DEFAULT 3 3 Accelerate MaxTakeoff 18 671 184 BAE146 DEFAULT 3 4 Accelerate MaxClimb ZERO 500 214 BAE146 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 BAE146 DEFAULT 3 6 Accelerate MaxClimb ZERO 500 250 BAE146 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 BAE146 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 BAE146 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 BAE300 DEFAULT 1 1 Takeoff MaxTakeoff 18 BAE300 DEFAULT 1 2 Climb MaxTakeoff 18 1 000 BAE300 DEFAULT 1 3 Accelerate MaxTakeoff 18 920 176 BAE300 DEFAULT 1 4 Accelerate MaxClimb ZERO 900 206 BAE300 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 BAE300 DEFAULT 1 6 Accelerate MaxClimb ZERO 900 250 BAE300 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 BAE300 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 BAE300 DEFAULT 1 9 Climb MaxClimb ZERO 10 000L 168/548 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) BAE300 DEFAULT 2 1 Takeoff MaxTakeoff 18 BAE300 DEFAULT 2 2 Climb MaxTakeoff 18 1 000 BAE300 DEFAULT 2 3 Accelerate MaxTakeoff 18 762 183 BAE300 DEFAULT 2 4 Accelerate MaxClimb ZERO 750 213 BAE300 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 BAE300 DEFAULT 2 6 Accelerate MaxClimb ZERO 750 250 BAE300 DEFAULT 2 7 Climb MaxClimb ZERO 5 500 BAE300 DEFAULT 2 8 Climb MaxClimb ZERO 7 500 BAE300 DEFAULT 2 9 Climb MaxClimb ZERO 10 000 BAE300 DEFAULT 3 1 Takeoff MaxTakeoff 18 BAE300 DEFAULT 3 2 Climb MaxTakeoff 18 1 000 BAE300 DEFAULT 3 3 Accelerate MaxTakeoff 18 622 189 BAE300 DEFAULT 3 4 Accelerate MaxClimb ZERO 500 219 BAE300 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 BAE300 DEFAULT 3 6 Accelerate MaxClimb ZERO 500 250 BAE300 DEFAULT 3 7 Climb MaxClimb ZERO 5 500 BAE300 DEFAULT 3 8 Climb MaxClimb ZERO 7 500 BAE300 DEFAULT 3 9 Climb MaxClimb ZERO 10 000 BEC58P DEFAULT 1 1 Takeoff MaxTakeoff TO BEC58P DEFAULT 1 2 Accelerate MaxTakeoff TO 1 040 1151.7.2015 EN Official Journal of the European Union L 168/549 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) BEC58P DEFAULT 1 3 Climb MaxTakeoff TO 1 000 BEC58P DEFAULT 1 4 Accelerate MaxTakeoff TO 1 040 130 BEC58P DEFAULT 1 5 Climb MaxClimb ZERO 3 000 BEC58P DEFAULT 1 6 Climb MaxClimb ZERO 5 500 BEC58P DEFAULT 1 7 Climb MaxClimb ZERO 7 500 BEC58P DEFAULT 1 8 Climb MaxClimb ZERO 10 000 CIT3 DEFAULT 1 1 Takeoff MaxTakeoff 20 CIT3 DEFAULT 1 2 Accelerate MaxTakeoff 20 1 146 149 CIT3 DEFAULT 1 3 Climb MaxTakeoff 20 1 500 CIT3 DEFAULT 1 4 Accelerate MaxTakeoff 10 1 146 174 CIT3 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 CIT3 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 503 250 CIT3 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 CIT3 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 CIT3 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 CL600 DEFAULT 1 1 Takeoff MaxTakeoff 20 CL600 DEFAULT 1 2 Accelerate MaxTakeoff 20 1 554 163 CL600 DEFAULT 1 3 Climb MaxTakeoff 20 1 500 CL600 DEFAULT 1 4 Accelerate MaxTakeoff 10 1 554 200 CL600 DEFAULT 1 5 Climb MaxClimb ZERO 3 000L 168/550 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CL600 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 771 250 CL600 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 CL600 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 CL600 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 CL601 DEFAULT 1 1 Takeoff MaxTakeoff 20 CL601 DEFAULT 1 2 Accelerate MaxTakeoff 20 1 673 177 CL601 DEFAULT 1 3 Climb MaxTakeoff 20 1 500 CL601 DEFAULT 1 4 Accelerate MaxTakeoff 10 1 673 200 CL601 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 CL601 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 724 250 CL601 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 CL601 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 CL601 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 CNA172 DEFAULT 1 1 Takeoff MaxTakeoff ZERO-C CNA172 DEFAULT 1 2 Accelerate MaxTakeoff ZERO-C 500 75 CNA172 DEFAULT 1 3 Climb MaxTakeoff ZERO-C 1 000 CNA172 DEFAULT 1 4 Accelerate MaxTakeoff ZERO-C 500 80 CNA172 DEFAULT 1 5 Climb MaxClimb ZERO-C 3 000 CNA172 DEFAULT 1 6 Climb MaxClimb ZERO-C 5 000 CNA172 DEFAULT 1 7 Climb MaxClimb ZERO-C 8 0001.7.2015 EN Official Journal of the European Union L 168/551 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CNA182 DEFAULT 1 1 Takeoff MaxTakeoff F-20D CNA182 DEFAULT 1 2 Accelerate MaxTakeoff F-20D 500 80 CNA182 DEFAULT 1 3 Climb MaxTakeoff ZERO 1 000 CNA182 DEFAULT 1 4 Accelerate MaxTakeoff ZERO 500 85 CNA182 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 CNA182 DEFAULT 1 6 Climb MaxClimb ZERO 5 000 CNA182 DEFAULT 1 7 Climb MaxClimb ZERO 8 000 CNA182 DEFAULT 1 8 Climb MaxClimb ZERO 10 000 CNA208 DEFAULT 1 1 Takeoff MaxTakeoff F-20D CNA208 DEFAULT 1 2 Accelerate MaxTakeoff F-20D 915 104 CNA208 DEFAULT 1 3 Climb MaxTakeoff ZERO 1 000 CNA208 DEFAULT 1 4 Accelerate MaxClimb ZERO 846 115 CNA208 DEFAULT 1 5 Climb MaxClimb ZERO 2 000 CNA208 DEFAULT 1 6 Climb MaxClimb ZERO 4 000 CNA208 DEFAULT 1 7 Climb MaxClimb ZERO 6 000 CNA208 DEFAULT 1 8 Climb MaxClimb ZERO 8 000 CNA208 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 CNA441 DEFAULT 1 1 Takeoff MaxTakeoff TO CNA441 DEFAULT 1 2 Accelerate MaxTakeoff TO 1 216 120 CNA441 DEFAULT 1 3 Accelerate MaxTakeoff ZERO 1 216 140L 168/552 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CNA441 DEFAULT 1 4 Climb MaxTakeoff ZERO 3 000 CNA441 DEFAULT 1 5 Climb MaxClimb ZERO 5 500 CNA441 DEFAULT 1 6 Climb MaxClimb ZERO 7 500 CNA441 DEFAULT 1 7 Climb MaxClimb ZERO 10 000 CNA500 DEFAULT 1 1 Takeoff MaxTakeoff 12 CNA500 DEFAULT 1 2 Accelerate MaxTakeoff 12 997 131 CNA500 DEFAULT 1 3 Climb MaxTakeoff 12 1 500 CNA500 DEFAULT 1 4 Accelerate MaxTakeoff 1 997 200 CNA500 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 CNA500 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 459 250 CNA500 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 CNA500 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 CNA500 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 CNA510 DEFAULT 1 1 Takeoff MaxTakeoff D_15 CNA510 DEFAULT 1 2 Climb MaxTakeoff D_15 535 CNA510 DEFAULT 1 3 Accelerate MaxTakeoff D_15 1 500 138,3 CNA510 DEFAULT 1 4 Climb MaxTakeoff D_15 1 500 CNA510 DEFAULT 1 5 Accelerate MaxClimb ZERO_C 1 500 171 CNA510 DEFAULT 1 6 Climb MaxClimb ZERO_C 3 000 CNA510 DEFAULT 1 7 Accelerate MaxClimb ZERO_C 1 000 2501.7.2015 EN Official Journal of the European Union L 168/553 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CNA510 DEFAULT 1 8 Climb MaxClimb ZERO_C 5 500 CNA510 DEFAULT 1 9 Climb MaxClimb ZERO_C 7 500 CNA510 DEFAULT 1 10 Climb MaxClimb ZERO_C 10 000 CNA510 FLAPS_0 1 1 Takeoff MaxTakeoff ZERO_D CNA510 FLAPS_0 1 2 Climb MaxTakeoff ZERO_D 601 CNA510 FLAPS_0 1 3 Accelerate MaxTakeoff ZERO_D 1 500 138,3 CNA510 FLAPS_0 1 4 Climb MaxTakeoff ZERO_D 1 500 CNA510 FLAPS_0 1 5 Accelerate MaxClimb ZERO_C 1 500 171 CNA510 FLAPS_0 1 6 Climb MaxClimb ZERO_C 3 000 CNA510 FLAPS_0 1 7 Accelerate MaxClimb ZERO_C 1 000 250 CNA510 FLAPS_0 1 8 Climb MaxClimb ZERO_C 5 500 CNA510 FLAPS_0 1 9 Climb MaxClimb ZERO_C 7 500 CNA510 FLAPS_0 1 10 Climb MaxClimb ZERO_C 10 000 CNA510 FLAPS_15 1 1 Takeoff MaxTakeoff D_15 CNA510 FLAPS_15 1 2 Climb MaxTakeoff D_15 535 CNA510 FLAPS_15 1 3 Accelerate MaxTakeoff D_15 1 500 138,3 CNA510 FLAPS_15 1 4 Climb MaxTakeoff D_15 1 500 CNA510 FLAPS_15 1 5 Accelerate MaxClimb ZERO_C 1 500 171 CNA510 FLAPS_15 1 6 Climb MaxClimb ZERO_C 3 000 CNA510 FLAPS_15 1 7 Accelerate MaxClimb ZERO_C 1 000 250L 168/554 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CNA510 FLAPS_15 1 8 Climb MaxClimb ZERO_C 5 500 CNA510 FLAPS_15 1 9 Climb MaxClimb ZERO_C 7 500 CNA510 FLAPS_15 1 10 Climb MaxClimb ZERO_C 10 000 CNA525C DEFAULT 1 1 Takeoff MaxTakeoff D-15 CNA525C DEFAULT 1 2 Climb MaxTakeoff D-15 482,5 CNA525C DEFAULT 1 3 Accelerate MaxTakeoff D-15 1 500 140,3 CNA525C DEFAULT 1 4 Climb MaxTakeoff D-15 1 500 CNA525C DEFAULT 1 5 Accelerate MaxClimb ZERO_C 1 500 171 CNA525C DEFAULT 1 6 Climb MaxClimb ZERO_C 3 000 CNA525C DEFAULT 1 7 Accelerate MaxClimb ZERO_C 1 000 250 CNA525C DEFAULT 1 8 Climb MaxClimb ZERO_C 5 500 CNA525C DEFAULT 1 9 Climb MaxClimb ZERO_C 7 500 CNA525C DEFAULT 1 10 Climb MaxClimb ZERO_C 10 000 CNA55B DEFAULT 1 1 Takeoff MaxTakeoff D_15 CNA55B DEFAULT 1 2 Climb MaxTakeoff D_15 379 CNA55B DEFAULT 1 3 Accelerate MaxTakeoff D_15 1 500 146,5 CNA55B DEFAULT 1 4 Climb MaxTakeoff D_15 1 500 CNA55B DEFAULT 1 5 Accelerate MaxClimb ZERO_C 1 500 171,5 CNA55B DEFAULT 1 6 Climb MaxClimb ZERO_C 3 000 CNA55B DEFAULT 1 7 Accelerate MaxClimb ZERO_C 1 000 2501.7.2015 EN Official Journal of the European Union L 168/555 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CNA55B DEFAULT 1 8 Climb MaxClimb ZERO_C 5 500 CNA55B DEFAULT 1 9 Climb MaxClimb ZERO_C 7 500 CNA55B DEFAULT 1 10 Climb MaxClimb ZERO_C 10 000 CNA55B FLAPS_0 1 1 Takeoff MaxTakeoff ZERO_D CNA55B FLAPS_0 1 2 Climb MaxTakeoff ZERO_D 420 CNA55B FLAPS_0 1 3 Accelerate MaxTakeoff ZERO_D 1 500 156 CNA55B FLAPS_0 1 4 Climb MaxTakeoff ZERO_D 1 500 CNA55B FLAPS_0 1 5 Accelerate MaxClimb ZERO_C 1 500 181,1 CNA55B FLAPS_0 1 6 Climb MaxClimb ZERO_C 3 000 CNA55B FLAPS_0 1 7 Accelerate MaxClimb ZERO_C 1 000 250 CNA55B FLAPS_0 1 8 Climb MaxClimb ZERO_C 5 500 CNA55B FLAPS_0 1 9 Climb MaxClimb ZERO_C 7 500 CNA55B FLAPS_0 1 10 Climb MaxClimb ZERO_C 10 000 CNA55B FLAPS_15 1 1 Takeoff MaxTakeoff D_15 CNA55B FLAPS_15 1 2 Climb MaxTakeoff D_15 379 CNA55B FLAPS_15 1 3 Accelerate MaxTakeoff D_15 1 500 146,5 CNA55B FLAPS_15 1 4 Climb MaxTakeoff D_15 1 500 CNA55B FLAPS_15 1 5 Accelerate MaxClimb ZERO_C 1 500 171,5 CNA55B FLAPS_15 1 6 Climb MaxClimb ZERO_C 3 000 CNA55B FLAPS_15 1 7 Accelerate MaxClimb ZERO_C 1 000 250L 168/556 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CNA55B FLAPS_15 1 8 Climb MaxClimb ZERO_C 5 500 CNA55B FLAPS_15 1 9 Climb MaxClimb ZERO_C 7 500 CNA55B FLAPS_15 1 10 Climb MaxClimb ZERO_C 10 000 CNA560E DEFAULT 1 1 Takeoff MaxTakeoff 15 CNA560E DEFAULT 1 2 Climb MaxTakeoff 15 277 CNA560E DEFAULT 1 3 Accelerate MaxTakeoff 15 1 500 161,7 CNA560E DEFAULT 1 4 Climb MaxTakeoff 15 1 500 CNA560E DEFAULT 1 5 Accelerate MaxClimb 15 1 500 186,7 CNA560E DEFAULT 1 6 Climb MaxClimb ZERO 3 000 CNA560E DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 CNA560E DEFAULT 1 8 Climb MaxClimb ZERO 5 500 CNA560E DEFAULT 1 9 Climb MaxClimb ZERO 7 500 CNA560E DEFAULT 1 10 Climb MaxClimb ZERO 10 000 CNA560U DEFAULT 1 1 Takeoff MaxTakeoff 15 CNA560U DEFAULT 1 2 Accelerate MaxTakeoff 15 1 200 148 CNA560U DEFAULT 1 3 Climb MaxTakeoff 15 1 500 CNA560U DEFAULT 1 4 Accelerate MaxTakeoff ZERO 1 500 175 CNA560U DEFAULT 1 5 Climb MaxClimb ZERO 3 000 CNA560U DEFAULT 1 6 Accelerate MaxClimb ZERO 1 500 250 CNA560U DEFAULT 1 7 Climb MaxClimb ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/557 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CNA560U DEFAULT 1 8 Climb MaxClimb ZERO 7 500 CNA560U DEFAULT 1 9 Climb MaxClimb ZERO 10 000 CNA560XL DEFAULT 1 1 Takeoff MaxTakeoff 15 CNA560XL DEFAULT 1 2 Accelerate MaxTakeoff 15 1 500 158 CNA560XL DEFAULT 1 3 Climb MaxTakeoff 15 1 500 CNA560XL DEFAULT 1 4 Accelerate MaxClimb ZERO 1 500 185 CNA560XL DEFAULT 1 5 Climb MaxClimb ZERO 3 000 CNA560XL DEFAULT 1 6 Accelerate MaxClimb ZERO 1 500 250 CNA560XL DEFAULT 1 7 Climb MaxClimb ZERO 10 000 CNA680 DEFAULT 1 1 Takeoff MaxTakeoff 15 CNA680 DEFAULT 1 2 Climb MaxTakeoff 15 386 CNA680 DEFAULT 1 3 Accelerate MaxTakeoff 15 1 000 140,6 CNA680 DEFAULT 1 4 Climb MaxTakeoff 15 1 500 CNA680 DEFAULT 1 5 Accelerate MaxClimb 15 1 500 175 CNA680 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 CNA680 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 500 250 CNA680 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 CNA680 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 CNA680 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 CNA750 DEFAULT 1 1 Takeoff MaxTakeoff 15L 168/558 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CNA750 DEFAULT 1 2 Climb MaxTakeoff 15 277 CNA750 DEFAULT 1 3 Accelerate MaxTakeoff 15 1 500 161,7 CNA750 DEFAULT 1 4 Climb MaxTakeoff 15 1 500 CNA750 DEFAULT 1 5 Accelerate MaxClimb 15 1 500 186,7 CNA750 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 CNA750 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 CNA750 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 CNA750 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 CNA750 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 CNA750 FLAP_15 1 1 Takeoff MaxTakeoff 15 CNA750 FLAP_15 1 2 Climb MaxTakeoff 15 277 CNA750 FLAP_15 1 3 Accelerate MaxTakeoff 15 1 500 161,7 CNA750 FLAP_15 1 4 Climb MaxTakeoff 15 1 500 CNA750 FLAP_15 1 5 Accelerate MaxClimb 15 1 500 186,7 CNA750 FLAP_15 1 6 Climb MaxClimb ZERO 3 000 CNA750 FLAP_15 1 7 Accelerate MaxClimb ZERO 1 000 250 CNA750 FLAP_15 1 8 Climb MaxClimb ZERO 5 500 CNA750 FLAP_15 1 9 Climb MaxClimb ZERO 7 500 CNA750 FLAP_15 1 10 Climb MaxClimb ZERO 10 000 CNA750 FLAP_5 1 1 Takeoff MaxTakeoff 51.7.2015 EN Official Journal of the European Union L 168/559 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CNA750 FLAP_5 1 2 Climb MaxTakeoff 5 285 CNA750 FLAP_5 1 3 Accelerate MaxTakeoff 5 1 500 168,9 CNA750 FLAP_5 1 4 Climb MaxTakeoff 5 1 500 CNA750 FLAP_5 1 5 Accelerate MaxClimb 5 1 500 193,9 CNA750 FLAP_5 1 6 Climb MaxClimb ZERO 3 000 CNA750 FLAP_5 1 7 Accelerate MaxClimb ZERO 1 000 250 CNA750 FLAP_5 1 8 Climb MaxClimb ZERO 5 500 CNA750 FLAP_5 1 9 Climb MaxClimb ZERO 7 500 CNA750 FLAP_5 1 10 Climb MaxClimb ZERO 10 000 CRJ9-ER DEFAULT 1 1 Takeoff MaxTakeoff D-8 CRJ9-ER DEFAULT 1 2 Climb MaxTakeoff D-8 595 CRJ9-ER DEFAULT 1 3 Climb MaxTakeoff U-8 1 000 CRJ9-ER DEFAULT 1 4 Accelerate MaxClimb 0-204 500 204 CRJ9-ER DEFAULT 1 5 Climb MaxClimb ZERO 3 000 CRJ9-ER DEFAULT 1 6 Accelerate MaxClimb 0-250 500 250 CRJ9-ER DEFAULT 1 7 Climb MaxClimb ZERO 10 000 CRJ9-ER DEFAULT 2 1 Takeoff MaxTakeoff D-8 CRJ9-ER DEFAULT 2 2 Climb MaxTakeoff D-8 555 CRJ9-ER DEFAULT 2 3 Climb MaxTakeoff U-8 1 000 CRJ9-ER DEFAULT 2 4 Accelerate MaxClimb 0-204 500 204L 168/560 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CRJ9-ER DEFAULT 2 5 Climb MaxClimb ZERO 3 000 CRJ9-ER DEFAULT 2 6 Accelerate MaxClimb 0-250 500 250 CRJ9-ER DEFAULT 2 7 Climb MaxClimb ZERO 10 000 CRJ9-ER DEFAULT 3 1 Takeoff MaxTakeoff D-8 CRJ9-ER DEFAULT 3 2 Climb MaxTakeoff D-8 525 CRJ9-ER DEFAULT 3 3 Climb MaxTakeoff U-8 1 000 CRJ9-ER DEFAULT 3 4 Accelerate MaxClimb 0-204 500 204 CRJ9-ER DEFAULT 3 5 Climb MaxClimb ZERO 3 000 CRJ9-ER DEFAULT 3 6 Accelerate MaxClimb 0-250 500 250 CRJ9-ER DEFAULT 3 7 Climb MaxClimb ZERO 10 000 CRJ9-ER DEFAULT 4 1 Takeoff MaxTakeoff D-8 CRJ9-ER DEFAULT 4 2 Climb MaxTakeoff D-8 485 CRJ9-ER DEFAULT 4 3 Climb MaxTakeoff U-8 1 000 CRJ9-ER DEFAULT 4 4 Accelerate MaxClimb 0-204 500 204 CRJ9-ER DEFAULT 4 5 Climb MaxClimb ZERO 3 000 CRJ9-ER DEFAULT 4 6 Accelerate MaxClimb 0-250 500 250 CRJ9-ER DEFAULT 4 7 Climb MaxClimb ZERO 10 000 CRJ9-ER DEFAULT 5 1 Takeoff MaxTakeoff D-8 CRJ9-ER DEFAULT 5 2 Climb MaxTakeoff D-8 465 CRJ9-ER DEFAULT 5 3 Climb MaxTakeoff U-8 1 0001.7.2015 EN Official Journal of the European Union L 168/561 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CRJ9-ER DEFAULT 5 4 Accelerate MaxClimb 0-204 500 204 CRJ9-ER DEFAULT 5 5 Climb MaxClimb 0-204 3 000 CRJ9-ER DEFAULT 5 6 Accelerate MaxClimb 0-250 500 250 CRJ9-ER DEFAULT 5 7 Climb MaxClimb ZERO 10 000 CRJ9-ER ICAO_A 1 1 Takeoff MaxTakeoff D-8 CRJ9-ER ICAO_A 1 2 Climb MaxTakeoff D-8 595 CRJ9-ER ICAO_A 1 3 Climb MaxTakeoff U-8 1 500 CRJ9-ER ICAO_A 1 4 Climb MaxClimb U-8 3 000 CRJ9-ER ICAO_A 1 5 Accelerate MaxClimb 0-250 500 250 CRJ9-ER ICAO_A 1 6 Climb MaxClimb ZERO 10 000 CRJ9-ER ICAO_A 2 1 Takeoff MaxTakeoff D-8 CRJ9-ER ICAO_A 2 2 Climb MaxTakeoff D-8 555 CRJ9-ER ICAO_A 2 3 Climb MaxTakeoff U-8 1 500 CRJ9-ER ICAO_A 2 4 Climb MaxClimb U-8 3 000 CRJ9-ER ICAO_A 2 5 Accelerate MaxClimb 0-250 500 250 CRJ9-ER ICAO_A 2 6 Climb MaxClimb ZERO 10 000 CRJ9-ER ICAO_A 3 1 Takeoff MaxTakeoff D-8 CRJ9-ER ICAO_A 3 2 Climb MaxTakeoff D-8 525 CRJ9-ER ICAO_A 3 3 Climb MaxTakeoff U-8 1 500 CRJ9-ER ICAO_A 3 4 Climb MaxClimb U-8 3 000L 168/562 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CRJ9-ER ICAO_A 3 5 Accelerate MaxClimb 0-250 500 250 CRJ9-ER ICAO_A 3 6 Climb MaxClimb ZERO 10 000 CRJ9-ER ICAO_A 4 1 Takeoff MaxTakeoff D-8 CRJ9-ER ICAO_A 4 2 Climb MaxTakeoff D-8 485 CRJ9-ER ICAO_A 4 3 Climb MaxTakeoff U-8 1 500 CRJ9-ER ICAO_A 4 4 Climb MaxClimb U-8 3 000 CRJ9-ER ICAO_A 4 5 Accelerate MaxClimb 0-250 500 250 CRJ9-ER ICAO_A 4 6 Climb MaxClimb ZERO 10 000 CRJ9-ER ICAO_A 5 1 Takeoff MaxTakeoff D-8 CRJ9-ER ICAO_A 5 2 Climb MaxTakeoff D-8 465 CRJ9-ER ICAO_A 5 3 Climb MaxTakeoff U-8 1 500 CRJ9-ER ICAO_A 5 4 Climb MaxClimb U-8 3 000 CRJ9-ER ICAO_A 5 5 Accelerate MaxClimb 0-250 500 250 CRJ9-ER ICAO_A 5 6 Climb MaxClimb ZERO 10 000 CRJ9-ER ICAO_B 1 1 Takeoff MaxTakeoff D-8 CRJ9-ER ICAO_B 1 2 Climb MaxTakeoff D-8 595 CRJ9-ER ICAO_B 1 3 Climb MaxTakeoff U-8 1 000 CRJ9-ER ICAO_B 1 4 Accelerate MaxTakeoff 0-204 500 204 CRJ9-ER ICAO_B 1 5 Climb MaxClimb ZERO 3 000 CRJ9-ER ICAO_B 1 6 Accelerate MaxClimb 0-250 500 2501.7.2015 EN Official Journal of the European Union L 168/563 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CRJ9-ER ICAO_B 1 7 Climb MaxClimb ZERO 10 000 CRJ9-ER ICAO_B 2 1 Takeoff MaxTakeoff D-8 CRJ9-ER ICAO_B 2 2 Climb MaxTakeoff D-8 555 CRJ9-ER ICAO_B 2 3 Climb MaxTakeoff U-8 1 000 CRJ9-ER ICAO_B 2 4 Accelerate MaxTakeoff 0-204 500 204 CRJ9-ER ICAO_B 2 5 Climb MaxClimb ZERO 3 000 CRJ9-ER ICAO_B 2 6 Accelerate MaxClimb 0-250 500 250 CRJ9-ER ICAO_B 2 7 Climb MaxClimb ZERO 10 000 CRJ9-ER ICAO_B 3 1 Takeoff MaxTakeoff D-8 CRJ9-ER ICAO_B 3 2 Climb MaxTakeoff D-8 525 CRJ9-ER ICAO_B 3 3 Climb MaxTakeoff U-8 1 000 CRJ9-ER ICAO_B 3 4 Accelerate MaxTakeoff 0-204 500 204 CRJ9-ER ICAO_B 3 5 Climb MaxClimb ZERO 3 000 CRJ9-ER ICAO_B 3 6 Accelerate MaxClimb 0-250 500 250 CRJ9-ER ICAO_B 3 7 Climb MaxClimb ZERO 10 000 CRJ9-ER ICAO_B 4 1 Takeoff MaxTakeoff D-8 CRJ9-ER ICAO_B 4 2 Climb MaxTakeoff D-8 485 CRJ9-ER ICAO_B 4 3 Climb MaxTakeoff U-8 1 000 CRJ9-ER ICAO_B 4 4 Accelerate MaxTakeoff 0-204 500 204 CRJ9-ER ICAO_B 4 5 Climb MaxClimb ZERO 3 000L 168/564 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CRJ9-ER ICAO_B 4 6 Accelerate MaxClimb 0-250 500 250 CRJ9-ER ICAO_B 4 7 Climb MaxClimb ZERO 10 000 CRJ9-ER ICAO_B 5 1 Takeoff MaxTakeoff D-8 CRJ9-ER ICAO_B 5 2 Climb MaxTakeoff D-8 465 CRJ9-ER ICAO_B 5 3 Climb MaxTakeoff U-8 1 000 CRJ9-ER ICAO_B 5 4 Accelerate MaxTakeoff 0-204 500 204 CRJ9-ER ICAO_B 5 5 Climb MaxClimb ZERO 3 000 CRJ9-ER ICAO_B 5 6 Accelerate MaxClimb 0-250 500 250 CRJ9-ER ICAO_B 5 7 Climb MaxClimb ZERO 10 000 CRJ9-LR DEFAULT 1 1 Takeoff MaxTakeoff D-8 CRJ9-LR DEFAULT 1 2 Climb MaxTakeoff D-8 615 CRJ9-LR DEFAULT 1 3 Climb MaxTakeoff U-8 1 000 CRJ9-LR DEFAULT 1 4 Accelerate MaxClimb 0-204 500 204 CRJ9-LR DEFAULT 1 5 Climb MaxClimb ZERO 3 000 CRJ9-LR DEFAULT 1 6 Accelerate MaxClimb 0-250 500 250 CRJ9-LR DEFAULT 1 7 Climb MaxClimb ZERO 10 000 CRJ9-LR DEFAULT 2 1 Takeoff MaxTakeoff D-8 CRJ9-LR DEFAULT 2 2 Climb MaxTakeoff D-8 575 CRJ9-LR DEFAULT 2 3 Climb MaxTakeoff U-8 1 000 CRJ9-LR DEFAULT 2 4 Accelerate MaxClimb 0-204 500 2041.7.2015 EN Official Journal of the European Union L 168/565 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CRJ9-LR DEFAULT 2 5 Climb MaxClimb ZERO 3 000 CRJ9-LR DEFAULT 2 6 Accelerate MaxClimb 0-250 500 250 CRJ9-LR DEFAULT 2 7 Climb MaxClimb ZERO 10 000 CRJ9-LR DEFAULT 3 1 Takeoff MaxTakeoff D-8 CRJ9-LR DEFAULT 3 2 Climb MaxTakeoff D-8 545 CRJ9-LR DEFAULT 3 3 Climb MaxTakeoff U-8 1 000 CRJ9-LR DEFAULT 3 4 Accelerate MaxClimb 0-204 500 204 CRJ9-LR DEFAULT 3 5 Climb MaxClimb 0-204 3 000 CRJ9-LR DEFAULT 3 6 Accelerate MaxClimb 0-250 500 250 CRJ9-LR DEFAULT 3 7 Climb MaxClimb ZERO 10 000 CRJ9-LR DEFAULT 4 1 Takeoff MaxTakeoff D-8 CRJ9-LR DEFAULT 4 2 Climb MaxTakeoff D-8 505 CRJ9-LR DEFAULT 4 3 Climb MaxTakeoff U-8 1 000 CRJ9-LR DEFAULT 4 4 Accelerate MaxClimb 0-204 500 204 CRJ9-LR DEFAULT 4 5 Climb MaxClimb ZERO 3 000 CRJ9-LR DEFAULT 4 6 Accelerate MaxClimb 0-250 500 250 CRJ9-LR DEFAULT 4 7 Climb MaxClimb 0-250 10 000 CRJ9-LR DEFAULT 5 1 Takeoff MaxTakeoff D-8 CRJ9-LR DEFAULT 5 2 Climb MaxTakeoff D-8 455 CRJ9-LR DEFAULT 5 3 Climb MaxTakeoff U-8 1 000L 168/566 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CRJ9-LR DEFAULT 5 4 Accelerate MaxClimb 0-204 500 204 CRJ9-LR DEFAULT 5 5 Climb MaxClimb ZERO 3 000 CRJ9-LR DEFAULT 5 6 Accelerate MaxClimb 0-250 500 250 CRJ9-LR DEFAULT 5 7 Climb MaxClimb ZERO 10 000 CRJ9-LR ICAO_A 1 1 Takeoff MaxTakeoff D-8 CRJ9-LR ICAO_A 1 2 Climb MaxTakeoff D-8 615 CRJ9-LR ICAO_A 1 3 Climb MaxTakeoff U-8 1 500 CRJ9-LR ICAO_A 1 4 Climb MaxClimb U-8 3 000 CRJ9-LR ICAO_A 1 5 Accelerate MaxClimb 0-250 500 250 CRJ9-LR ICAO_A 1 6 Climb MaxClimb ZERO 10 000 CRJ9-LR ICAO_A 2 1 Takeoff MaxTakeoff D-8 CRJ9-LR ICAO_A 2 2 Climb MaxTakeoff D-8 575 CRJ9-LR ICAO_A 2 3 Climb MaxTakeoff U-8 1 500 CRJ9-LR ICAO_A 2 4 Climb MaxClimb U-8 3 000 CRJ9-LR ICAO_A 2 5 Accelerate MaxClimb U-8 500 250 CRJ9-LR ICAO_A 2 6 Climb MaxClimb ZERO 10 000 CRJ9-LR ICAO_A 3 1 Takeoff MaxTakeoff D-8 CRJ9-LR ICAO_A 3 2 Climb MaxTakeoff D-8 545 CRJ9-LR ICAO_A 3 3 Climb MaxTakeoff U-8 1 500 CRJ9-LR ICAO_A 3 4 Climb MaxClimb U-8 3 0001.7.2015 EN Official Journal of the European Union L 168/567 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CRJ9-LR ICAO_A 3 5 Accelerate MaxClimb U-8 500 250 CRJ9-LR ICAO_A 3 6 Climb MaxClimb ZERO 10 000 CRJ9-LR ICAO_A 4 1 Takeoff MaxTakeoff D-8 CRJ9-LR ICAO_A 4 2 Climb MaxTakeoff D-8 505 CRJ9-LR ICAO_A 4 3 Climb MaxTakeoff U-8 1 500 CRJ9-LR ICAO_A 4 4 Climb MaxClimb U-8 3 000 CRJ9-LR ICAO_A 4 5 Accelerate MaxClimb U-8 500 250 CRJ9-LR ICAO_A 4 6 Climb MaxClimb ZERO 10 000 CRJ9-LR ICAO_A 5 1 Takeoff MaxTakeoff D-8 CRJ9-LR ICAO_A 5 2 Climb MaxTakeoff D-8 455 CRJ9-LR ICAO_A 5 3 Climb MaxTakeoff U-8 1 500 CRJ9-LR ICAO_A 5 4 Climb MaxClimb U-8 3 000 CRJ9-LR ICAO_A 5 5 Accelerate MaxClimb 0-250 500 250 CRJ9-LR ICAO_A 5 6 Climb MaxClimb ZERO 10 000 CRJ9-LR ICAO_B 1 1 Takeoff MaxTakeoff D-8 CRJ9-LR ICAO_B 1 2 Climb MaxTakeoff D-8 615 CRJ9-LR ICAO_B 1 3 Climb MaxTakeoff U-8 1 000 CRJ9-LR ICAO_B 1 4 Accelerate MaxTakeoff 0-204 500 204 CRJ9-LR ICAO_B 1 5 Climb MaxClimb ZERO 3 000 CRJ9-LR ICAO_B 1 6 Accelerate MaxClimb 0-250 500 250L 168/568 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CRJ9-LR ICAO_B 1 7 Climb MaxClimb ZERO 10 000 CRJ9-LR ICAO_B 2 1 Takeoff MaxTakeoff D-8 CRJ9-LR ICAO_B 2 2 Climb MaxTakeoff D-8 575 CRJ9-LR ICAO_B 2 3 Climb MaxTakeoff U-8 1 000 CRJ9-LR ICAO_B 2 4 Accelerate MaxTakeoff 0-204 500 204 CRJ9-LR ICAO_B 2 5 Climb MaxClimb ZERO 3 000 CRJ9-LR ICAO_B 2 6 Accelerate MaxClimb 0-250 500 250 CRJ9-LR ICAO_B 2 7 Climb MaxClimb ZERO 10 000 CRJ9-LR ICAO_B 3 1 Takeoff MaxTakeoff D-8 CRJ9-LR ICAO_B 3 2 Climb MaxTakeoff D-8 545 CRJ9-LR ICAO_B 3 3 Climb MaxTakeoff U-8 1 000 CRJ9-LR ICAO_B 3 4 Accelerate MaxTakeoff 0-204 500 204 CRJ9-LR ICAO_B 3 5 Climb MaxClimb ZERO 3 000 CRJ9-LR ICAO_B 3 6 Accelerate MaxClimb 0-250 500 250 CRJ9-LR ICAO_B 3 7 Climb MaxClimb ZERO 10 000 CRJ9-LR ICAO_B 4 1 Takeoff MaxTakeoff D-8 CRJ9-LR ICAO_B 4 2 Climb MaxTakeoff D-8 505 CRJ9-LR ICAO_B 4 3 Climb MaxTakeoff U-8 1 000 CRJ9-LR ICAO_B 4 4 Accelerate MaxTakeoff 0-204 500 204 CRJ9-LR ICAO_B 4 5 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/569 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CRJ9-LR ICAO_B 4 6 Accelerate MaxClimb 0-250 500 250 CRJ9-LR ICAO_B 4 7 Climb MaxClimb ZERO 10 000 CRJ9-LR ICAO_B 5 1 Takeoff MaxTakeoff D-8 CRJ9-LR ICAO_B 5 2 Climb MaxTakeoff D-8 455 CRJ9-LR ICAO_B 5 3 Climb MaxTakeoff U-8 1 000 CRJ9-LR ICAO_B 5 4 Accelerate MaxTakeoff 0-204 500 204 CRJ9-LR ICAO_B 5 5 Climb MaxClimb ZERO 3 000 CRJ9-LR ICAO_B 5 6 Accelerate MaxClimb 0-250 500 250 CRJ9-LR ICAO_B 5 7 Climb MaxClimb ZERO 10 000 CVR580 DEFAULT 1 1 Takeoff MaxTakeoff 10 CVR580 DEFAULT 1 2 Climb MaxTakeoff 10 1 000 CVR580 DEFAULT 1 3 Accelerate MaxTakeoff 10 1 907 130 CVR580 DEFAULT 1 4 Accelerate MaxClimb INTR 1 430 150 CVR580 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 CVR580 DEFAULT 1 6 Climb MaxClimb ZERO 5 500 CVR580 DEFAULT 1 7 Climb MaxClimb ZERO 7 500 CVR580 DEFAULT 1 8 Climb MaxClimb ZERO 10 000 CVR580 DEFAULT 2 1 Takeoff MaxTakeoff 10 CVR580 DEFAULT 2 2 Climb MaxTakeoff 10 1 000 CVR580 DEFAULT 2 3 Accelerate MaxTakeoff 10 1 557 136L 168/570 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) CVR580 DEFAULT 2 4 Accelerate MaxClimb INTR 1 168 156 CVR580 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 CVR580 DEFAULT 2 6 Climb MaxClimb ZERO 5 500 CVR580 DEFAULT 2 7 Climb MaxClimb ZERO 7 500 CVR580 DEFAULT 2 8 Climb MaxClimb ZERO 10 000 CVR580 DEFAULT 3 1 Takeoff MaxTakeoff 10 CVR580 DEFAULT 3 2 Climb MaxTakeoff 10 1 000 CVR580 DEFAULT 3 3 Accelerate MaxTakeoff 10 1 321 140 CVR580 DEFAULT 3 4 Accelerate MaxClimb INTR 991 160 CVR580 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 CVR580 DEFAULT 3 6 Climb MaxClimb ZERO 5 500 CVR580 DEFAULT 3 7 Climb MaxClimb ZERO 7 500 CVR580 DEFAULT 3 8 Climb MaxClimb ZERO 10 000 DC1010 DEFAULT 1 1 Takeoff MaxTakeoff 10 DC1010 DEFAULT 1 2 Climb MaxTakeoff 10 1 000 DC1010 DEFAULT 1 3 Accelerate MaxTakeoff 10 1 904 159 DC1010 DEFAULT 1 4 Accelerate MaxTakeoff 5 1 428 174 DC1010 DEFAULT 1 5 Accelerate MaxClimb INT 1 000 189 DC1010 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 DC1010 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 2501.7.2015 EN Official Journal of the European Union L 168/571 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC1010 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC1010 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC1010 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC1010 DEFAULT 2 1 Takeoff MaxTakeoff 10 DC1010 DEFAULT 2 2 Climb MaxTakeoff 10 1 000 DC1010 DEFAULT 2 3 Accelerate MaxTakeoff 10 1 799 163 DC1010 DEFAULT 2 4 Accelerate MaxTakeoff 5 1 350 178 DC1010 DEFAULT 2 5 Accelerate MaxClimb INT 1 000 193 DC1010 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 DC1010 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC1010 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC1010 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC1010 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC1010 DEFAULT 3 1 Takeoff MaxTakeoff 10 DC1010 DEFAULT 3 2 Climb MaxTakeoff 10 1 000 DC1010 DEFAULT 3 3 Accelerate MaxTakeoff 10 1 670 167 DC1010 DEFAULT 3 4 Accelerate MaxTakeoff 5 1 253 182 DC1010 DEFAULT 3 5 Accelerate MaxClimb INT 1 000 197 DC1010 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 DC1010 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250L 168/572 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC1010 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC1010 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC1010 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DC1010 DEFAULT 4 1 Takeoff MaxTakeoff 10 DC1010 DEFAULT 4 2 Climb MaxTakeoff 10 1 000 DC1010 DEFAULT 4 3 Accelerate MaxTakeoff 10 1 494 174 DC1010 DEFAULT 4 4 Accelerate MaxTakeoff 5 1 121 189 DC1010 DEFAULT 4 5 Accelerate MaxClimb INT 1 000 204 DC1010 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 DC1010 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 DC1010 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 DC1010 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 DC1010 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 DC1010 DEFAULT 5 1 Takeoff MaxTakeoff 10 DC1010 DEFAULT 5 2 Climb MaxTakeoff 10 1 000 DC1010 DEFAULT 5 3 Accelerate MaxTakeoff 10 1 335 180 DC1010 DEFAULT 5 4 Accelerate MaxTakeoff 5 1 002 195 DC1010 DEFAULT 5 5 Accelerate MaxClimb INT 1 000 210 DC1010 DEFAULT 5 6 Climb MaxClimb ZERO 3 000 DC1010 DEFAULT 5 7 Accelerate MaxClimb ZERO 1 000 2501.7.2015 EN Official Journal of the European Union L 168/573 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC1010 DEFAULT 5 8 Climb MaxClimb ZERO 5 500 DC1010 DEFAULT 5 9 Climb MaxClimb ZERO 7 500 DC1010 DEFAULT 5 10 Climb MaxClimb ZERO 10 000 DC1010 DEFAULT 6 1 Takeoff MaxTakeoff 10 DC1010 DEFAULT 6 2 Climb MaxTakeoff 10 1 000 DC1010 DEFAULT 6 3 Accelerate MaxTakeoff 10 1 191 186 DC1010 DEFAULT 6 4 Accelerate MaxTakeoff 5 894 201 DC1010 DEFAULT 6 5 Accelerate MaxClimb INT 800 216 DC1010 DEFAULT 6 6 Climb MaxClimb ZERO 3 000 DC1010 DEFAULT 6 7 Accelerate MaxClimb ZERO 800 250 DC1010 DEFAULT 6 8 Climb MaxClimb ZERO 5 500 DC1010 DEFAULT 6 9 Climb MaxClimb ZERO 7 500 DC1010 DEFAULT 6 10 Climb MaxClimb ZERO 10 000 DC1040 DEFAULT 1 1 Takeoff MaxTakeoff 15 DC1040 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 DC1040 DEFAULT 1 3 Accelerate MaxTakeoff 15 2 255 175 DC1040 DEFAULT 1 4 Accelerate MaxTakeoff 5 1 692 190 DC1040 DEFAULT 1 5 Accelerate MaxClimb INT 1 000 205 DC1040 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 DC1040 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250L 168/574 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC1040 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC1040 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC1040 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC1040 DEFAULT 2 1 Takeoff MaxTakeoff 15 DC1040 DEFAULT 2 2 Climb MaxTakeoff 15 1 000 DC1040 DEFAULT 2 3 Accelerate MaxTakeoff 15 2 146 178 DC1040 DEFAULT 2 4 Accelerate MaxTakeoff 5 1 610 193 DC1040 DEFAULT 2 5 Accelerate MaxClimb INT 1 000 208 DC1040 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 DC1040 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC1040 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC1040 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC1040 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC1040 DEFAULT 3 1 Takeoff MaxTakeoff 15 DC1040 DEFAULT 3 2 Climb MaxTakeoff 15 1 000 DC1040 DEFAULT 3 3 Accelerate MaxTakeoff 15 2 050 181 DC1040 DEFAULT 3 4 Accelerate MaxTakeoff 5 1 538 196 DC1040 DEFAULT 3 5 Accelerate MaxClimb INT 1 000 211 DC1040 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 DC1040 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 2501.7.2015 EN Official Journal of the European Union L 168/575 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC1040 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC1040 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC1040 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DC1040 DEFAULT 4 1 Takeoff MaxTakeoff 15 DC1040 DEFAULT 4 2 Climb MaxTakeoff 15 1 000 DC1040 DEFAULT 4 3 Accelerate MaxTakeoff 15 1 859 187 DC1040 DEFAULT 4 4 Accelerate MaxTakeoff 5 1 395 202 DC1040 DEFAULT 4 5 Accelerate MaxClimb INT 1 000 217 DC1040 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 DC1040 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 DC1040 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 DC1040 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 DC1040 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 DC1040 DEFAULT 5 1 Takeoff MaxTakeoff 15 DC1040 DEFAULT 5 2 Climb MaxTakeoff 15 1 000 DC1040 DEFAULT 5 3 Accelerate MaxTakeoff 15 1 639 195 DC1040 DEFAULT 5 4 Accelerate MaxTakeoff 5 1 229 210 DC1040 DEFAULT 5 5 Accelerate MaxClimb INT 1 000 225 DC1040 DEFAULT 5 6 Climb MaxClimb ZERO 3 000 DC1040 DEFAULT 5 7 Accelerate MaxClimb ZERO 1 000 250L 168/576 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC1040 DEFAULT 5 8 Climb MaxClimb ZERO 5 500 DC1040 DEFAULT 5 9 Climb MaxClimb ZERO 7 500 DC1040 DEFAULT 5 10 Climb MaxClimb ZERO 10 000 DC1040 DEFAULT 6 1 Takeoff MaxTakeoff 15 DC1040 DEFAULT 6 2 Climb MaxTakeoff 15 1 000 DC1040 DEFAULT 6 3 Accelerate MaxTakeoff 15 1 436 203 DC1040 DEFAULT 6 4 Accelerate MaxTakeoff 5 1 077 218 DC1040 DEFAULT 6 5 Accelerate MaxClimb INT 1 000 233 DC1040 DEFAULT 6 6 Climb MaxClimb ZERO 3 000 DC1040 DEFAULT 6 7 Accelerate MaxClimb ZERO 1 000 250 DC1040 DEFAULT 6 8 Climb MaxClimb ZERO 5 500 DC1040 DEFAULT 6 9 Climb MaxClimb ZERO 7 500 DC1040 DEFAULT 6 10 Climb MaxClimb ZERO 10 000 DC1040 DEFAULT 7 1 Takeoff MaxTakeoff 15 DC1040 DEFAULT 7 2 Climb MaxTakeoff 15 1 000 DC1040 DEFAULT 7 3 Accelerate MaxTakeoff 15 1 170 211 DC1040 DEFAULT 7 4 Accelerate MaxTakeoff 5 878 226 DC1040 DEFAULT 7 5 Accelerate MaxClimb INT 800 241 DC1040 DEFAULT 7 6 Climb MaxClimb ZERO 3 000 DC1040 DEFAULT 7 7 Accelerate MaxClimb ZERO 800 2501.7.2015 EN Official Journal of the European Union L 168/577 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC1040 DEFAULT 7 8 Climb MaxClimb ZERO 5 500 DC1040 DEFAULT 7 9 Climb MaxClimb ZERO 7 500 DC1040 DEFAULT 7 10 Climb MaxClimb ZERO 10 000 DC3 DEFAULT 1 1 Takeoff MaxTakeoff TO DC3 DEFAULT 1 2 Climb MaxTakeoff TO 400 DC3 DEFAULT 1 3 Climb MaxClimb ZERO 3 000 DC3 DEFAULT 1 4 Accelerate MaxClimb ZERO 1 000 126 DC3 DEFAULT 1 5 Climb MaxClimb ZERO 5 500 DC3 DEFAULT 1 6 Climb MaxClimb ZERO 7 500 DC3 DEFAULT 1 7 Climb MaxClimb ZERO 10 000 DC3 DEFAULT 2 1 Takeoff MaxTakeoff TO DC3 DEFAULT 2 2 Climb MaxTakeoff TO 400 DC3 DEFAULT 2 3 Climb MaxClimb ZERO 3 000 DC3 DEFAULT 2 4 Accelerate MaxClimb ZERO 800 130 DC3 DEFAULT 2 5 Climb MaxClimb ZERO 5 500 DC3 DEFAULT 2 6 Climb MaxClimb ZERO 7 500 DC3 DEFAULT 2 7 Climb MaxClimb ZERO 10 000 DC3 DEFAULT 3 1 Takeoff MaxTakeoff TO DC3 DEFAULT 3 2 Climb MaxTakeoff TO 400 DC3 DEFAULT 3 3 Climb MaxClimb ZERO 3 000L 168/578 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC3 DEFAULT 3 4 Accelerate MaxClimb ZERO 633 134 DC3 DEFAULT 3 5 Climb MaxClimb ZERO 7 500 DC3 DEFAULT 3 6 Climb MaxClimb ZERO 10 000 DC6 DEFAULT 1 1 Takeoff MaxTakeoff TO DC6 DEFAULT 1 2 Climb MaxTakeoff TO 1 500 DC6 DEFAULT 1 3 Accelerate MaxTakeoff TO 818 135 DC6 DEFAULT 1 4 Climb MaxClimb ZERO 3 000 DC6 DEFAULT 1 5 Climb MaxClimb ZERO 5 500 DC6 DEFAULT 1 6 Climb MaxClimb ZERO 7 500 DC6 DEFAULT 1 7 Climb MaxClimb ZERO 10 000 DC6 DEFAULT 2 1 Takeoff MaxTakeoff TO DC6 DEFAULT 2 2 Climb MaxTakeoff TO 1 500 DC6 DEFAULT 2 3 Accelerate MaxTakeoff TO 643 143 DC6 DEFAULT 2 4 Climb MaxClimb ZERO 3 000 DC6 DEFAULT 2 5 Climb MaxClimb ZERO 5 500 DC6 DEFAULT 2 6 Climb MaxClimb ZERO 7 500 DC6 DEFAULT 2 7 Climb MaxClimb ZERO 10 000 DC6 DEFAULT 3 1 Takeoff MaxTakeoff TO DC6 DEFAULT 3 2 Climb MaxTakeoff TO 1 500 DC6 DEFAULT 3 3 Accelerate MaxTakeoff TO 498 1491.7.2015 EN Official Journal of the European Union L 168/579 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC6 DEFAULT 3 4 Climb MaxClimb ZERO 3 000 DC6 DEFAULT 3 5 Climb MaxClimb ZERO 5 500 DC6 DEFAULT 3 6 Climb MaxClimb ZERO 7 500 DC6 DEFAULT 3 7 Climb MaxClimb ZERO 10 000 DC850 DEFAULT 1 1 Takeoff MaxTakeoff 15 DC850 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 DC850 DEFAULT 1 3 Accelerate MaxTakeoff 15 2 205 149 DC850 DEFAULT 1 4 Accelerate MaxTakeoff INT 1 654 169 DC850 DEFAULT 1 5 Accelerate MaxClimb INT 1 000 189 DC850 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 DC850 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 DC850 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC850 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC850 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC850 DEFAULT 2 1 Takeoff MaxTakeoff 15 DC850 DEFAULT 2 2 Climb MaxTakeoff 15 1 000 DC850 DEFAULT 2 3 Accelerate MaxTakeoff 15 2 089 153 DC850 DEFAULT 2 4 Accelerate MaxTakeoff INT 1 567 173 DC850 DEFAULT 2 5 Accelerate MaxClimb INT 1 000 193 DC850 DEFAULT 2 6 Climb MaxClimb ZERO 3 000L 168/580 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC850 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC850 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC850 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC850 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC850 DEFAULT 3 1 Takeoff MaxTakeoff 15 DC850 DEFAULT 3 2 Climb MaxTakeoff 15 1 000 DC850 DEFAULT 3 3 Accelerate MaxTakeoff 15 1 930 158 DC850 DEFAULT 3 4 Accelerate MaxTakeoff INT 1 448 178 DC850 DEFAULT 3 5 Accelerate MaxClimb INT 1 000 198 DC850 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 DC850 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 DC850 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC850 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC850 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DC850 DEFAULT 4 1 Takeoff MaxTakeoff 15 DC850 DEFAULT 4 2 Climb MaxTakeoff 15 1 000 DC850 DEFAULT 4 3 Accelerate MaxTakeoff 15 1 743 165 DC850 DEFAULT 4 4 Accelerate MaxTakeoff INT 1 308 185 DC850 DEFAULT 4 5 Accelerate MaxClimb INT 1 000 205 DC850 DEFAULT 4 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/581 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC850 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 DC850 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 DC850 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 DC850 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 DC850 DEFAULT 5 1 Takeoff MaxTakeoff 15 DC850 DEFAULT 5 2 Climb MaxTakeoff 15 1 000 DC850 DEFAULT 5 3 Accelerate MaxTakeoff 15 1 541 173 DC850 DEFAULT 5 4 Accelerate MaxTakeoff INT 1 156 193 DC850 DEFAULT 5 5 Accelerate MaxClimb INT 1 000 213 DC850 DEFAULT 5 6 Climb MaxClimb ZERO 3 000 DC850 DEFAULT 5 7 Accelerate MaxClimb ZERO 1 000 250 DC850 DEFAULT 5 8 Climb MaxClimb ZERO 5 500 DC850 DEFAULT 5 9 Climb MaxClimb ZERO 7 500 DC850 DEFAULT 5 10 Climb MaxClimb ZERO 10 000 DC850 DEFAULT 6 1 Takeoff MaxTakeoff 15 DC850 DEFAULT 6 2 Climb MaxTakeoff 15 1 000 DC850 DEFAULT 6 3 Accelerate MaxTakeoff 15 1 397 180 DC850 DEFAULT 6 4 Accelerate MaxTakeoff INT 1 048 200 DC850 DEFAULT 6 5 Accelerate MaxClimb INT 1 000 220 DC850 DEFAULT 6 6 Climb MaxClimb ZERO 3 000L 168/582 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC850 DEFAULT 6 7 Accelerate MaxClimb ZERO 1 000 250 DC850 DEFAULT 6 8 Climb MaxClimb ZERO 5 500 DC850 DEFAULT 6 9 Climb MaxClimb ZERO 7 500 DC850 DEFAULT 6 10 Climb MaxClimb ZERO 10 000 DC860 DEFAULT 1 1 Takeoff MaxTakeoff 12 DC860 DEFAULT 1 2 Climb MaxTakeoff 12 1 000 DC860 DEFAULT 1 3 Accelerate MaxTakeoff 12 2 055 160 DC860 DEFAULT 1 4 Accelerate MaxTakeoff INT 1 541 180 DC860 DEFAULT 1 5 Accelerate MaxClimb INT 1 000 200 DC860 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 DC860 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 DC860 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC860 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC860 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC860 DEFAULT 2 1 Takeoff MaxTakeoff 12 DC860 DEFAULT 2 2 Climb MaxTakeoff 12 1 000 DC860 DEFAULT 2 3 Accelerate MaxTakeoff 12 1 959 164 DC860 DEFAULT 2 4 Accelerate MaxTakeoff INT 1 470 184 DC860 DEFAULT 2 5 Accelerate MaxClimb INT 1 000 204 DC860 DEFAULT 2 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/583 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC860 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC860 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC860 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC860 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC860 DEFAULT 3 1 Takeoff MaxTakeoff 12 DC860 DEFAULT 3 2 Climb MaxTakeoff 12 1 000 DC860 DEFAULT 3 3 Accelerate MaxTakeoff 12 1 827 168 DC860 DEFAULT 3 4 Accelerate MaxTakeoff INT 1 371 188 DC860 DEFAULT 3 5 Accelerate MaxClimb INT 1 000 208 DC860 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 DC860 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 DC860 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC860 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC860 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DC860 DEFAULT 4 1 Takeoff MaxTakeoff 12 DC860 DEFAULT 4 2 Climb MaxTakeoff 12 1 000 DC860 DEFAULT 4 3 Accelerate MaxTakeoff 12 1 668 175 DC860 DEFAULT 4 4 Accelerate MaxTakeoff INT 1 251 195 DC860 DEFAULT 4 5 Accelerate MaxClimb INT 1 000 215 DC860 DEFAULT 4 6 Climb MaxClimb ZERO 3 000L 168/584 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC860 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 DC860 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 DC860 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 DC860 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 DC860 DEFAULT 5 1 Takeoff MaxTakeoff 12 DC860 DEFAULT 5 2 Climb MaxTakeoff 12 1 000 DC860 DEFAULT 5 3 Accelerate MaxTakeoff 12 1 491 182 DC860 DEFAULT 5 4 Accelerate MaxTakeoff INT 1 118 202 DC860 DEFAULT 5 5 Accelerate MaxClimb INT 1 000 222 DC860 DEFAULT 5 6 Climb MaxClimb ZERO 3 000 DC860 DEFAULT 5 7 Accelerate MaxClimb ZERO 1 000 250 DC860 DEFAULT 5 8 Climb MaxClimb ZERO 5 500 DC860 DEFAULT 5 9 Climb MaxClimb ZERO 7 500 DC860 DEFAULT 5 10 Climb MaxClimb ZERO 10 000 DC860 DEFAULT 6 1 Takeoff MaxTakeoff 12 DC860 DEFAULT 6 2 Climb MaxTakeoff 12 1 000 DC860 DEFAULT 6 3 Accelerate MaxTakeoff 12 1 394 187 DC860 DEFAULT 6 4 Accelerate MaxTakeoff INT 1 046 207 DC860 DEFAULT 6 5 Accelerate MaxClimb INT 1 000 227 DC860 DEFAULT 6 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/585 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC860 DEFAULT 6 7 Accelerate MaxClimb ZERO 1 000 250 DC860 DEFAULT 6 8 Climb MaxClimb ZERO 5 500 DC860 DEFAULT 6 9 Climb MaxClimb ZERO 7 500 DC860 DEFAULT 6 10 Climb MaxClimb ZERO 10 000 DC860 DEFAULT 7 1 Takeoff MaxTakeoff 12 DC860 DEFAULT 7 2 Climb MaxTakeoff 12 1 000 DC860 DEFAULT 7 3 Accelerate MaxTakeoff 12 1 275 192 DC860 DEFAULT 7 4 Accelerate MaxTakeoff INT 956 212 DC860 DEFAULT 7 5 Accelerate MaxClimb INT 900 232 DC860 DEFAULT 7 6 Climb MaxClimb ZERO 3 000 DC860 DEFAULT 7 7 Accelerate MaxClimb ZERO 900 250 DC860 DEFAULT 7 8 Climb MaxClimb ZERO 5 500 DC860 DEFAULT 7 9 Climb MaxClimb ZERO 7 500 DC860 DEFAULT 7 10 Climb MaxClimb ZERO 10 000 DC870 DEFAULT 1 1 Takeoff MaxTakeoff 12 DC870 DEFAULT 1 2 Climb MaxTakeoff 12 1 000 DC870 DEFAULT 1 3 Accelerate MaxTakeoff 12 2 405 160 DC870 DEFAULT 1 4 Accelerate MaxTakeoff INT 1 804 180 DC870 DEFAULT 1 5 Accelerate MaxClimb INT 1 000 200 DC870 DEFAULT 1 6 Climb MaxClimb ZERO 3 000L 168/586 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC870 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 DC870 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC870 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC870 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC870 DEFAULT 2 1 Takeoff MaxTakeoff 12 DC870 DEFAULT 2 2 Climb MaxTakeoff 12 1 000 DC870 DEFAULT 2 3 Accelerate MaxTakeoff 12 2 289 164 DC870 DEFAULT 2 4 Accelerate MaxTakeoff INT 1 717 184 DC870 DEFAULT 2 5 Accelerate MaxClimb INT 1 000 204 DC870 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 DC870 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC870 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC870 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC870 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC870 DEFAULT 3 1 Takeoff MaxTakeoff 12 DC870 DEFAULT 3 2 Climb MaxTakeoff 12 1 000 DC870 DEFAULT 3 3 Accelerate MaxTakeoff 12 2 129 168 DC870 DEFAULT 3 4 Accelerate MaxTakeoff INT 1 597 188 DC870 DEFAULT 3 5 Accelerate MaxClimb INT 1 000 208 DC870 DEFAULT 3 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/587 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC870 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 DC870 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC870 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC870 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DC870 DEFAULT 4 1 Takeoff MaxTakeoff 12 DC870 DEFAULT 4 2 Climb MaxTakeoff 12 1 000 DC870 DEFAULT 4 3 Accelerate MaxTakeoff 12 1 938 175 DC870 DEFAULT 4 4 Accelerate MaxTakeoff INT 1 454 195 DC870 DEFAULT 4 5 Accelerate MaxClimb INT 1 000 215 DC870 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 DC870 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 DC870 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 DC870 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 DC870 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 DC870 DEFAULT 5 1 Takeoff MaxTakeoff 12 DC870 DEFAULT 5 2 Climb MaxTakeoff 12 1 000 DC870 DEFAULT 5 3 Accelerate MaxTakeoff 12 1 727 182 DC870 DEFAULT 5 4 Accelerate MaxTakeoff INT 1 295 202 DC870 DEFAULT 5 5 Accelerate MaxClimb INT 1 000 222 DC870 DEFAULT 5 6 Climb MaxClimb ZERO 3 000L 168/588 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC870 DEFAULT 5 7 Accelerate MaxClimb ZERO 1 000 250 DC870 DEFAULT 5 8 Climb MaxClimb ZERO 5 500 DC870 DEFAULT 5 9 Climb MaxClimb ZERO 7 500 DC870 DEFAULT 5 10 Climb MaxClimb ZERO 10 000 DC870 DEFAULT 6 1 Takeoff MaxTakeoff 12 DC870 DEFAULT 6 2 Climb MaxTakeoff 12 1 000 DC870 DEFAULT 6 3 Accelerate MaxTakeoff 12 1 611 187 DC870 DEFAULT 6 4 Accelerate MaxTakeoff INT 1 209 207 DC870 DEFAULT 6 5 Accelerate MaxClimb INT 1 000 227 DC870 DEFAULT 6 6 Climb MaxClimb ZERO 3 000 DC870 DEFAULT 6 7 Accelerate MaxClimb ZERO 1 000 250 DC870 DEFAULT 6 8 Climb MaxClimb ZERO 5 500 DC870 DEFAULT 6 9 Climb MaxClimb ZERO 7 500 DC870 DEFAULT 6 10 Climb MaxClimb ZERO 10 000 DC870 DEFAULT 7 1 Takeoff MaxTakeoff 12 DC870 DEFAULT 7 2 Climb MaxTakeoff 12 1 000 DC870 DEFAULT 7 3 Accelerate MaxTakeoff 12 1 470 192 DC870 DEFAULT 7 4 Accelerate MaxTakeoff INT 1 103 212 DC870 DEFAULT 7 5 Accelerate MaxClimb INT 1 000 232 DC870 DEFAULT 7 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/589 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC870 DEFAULT 7 7 Accelerate MaxClimb ZERO 1 000 250 DC870 DEFAULT 7 8 Climb MaxClimb ZERO 5 500 DC870 DEFAULT 7 9 Climb MaxClimb ZERO 7 500 DC870 DEFAULT 7 10 Climb MaxClimb ZERO 10 000 DC8QN DEFAULT 1 1 Takeoff MaxTakeoff 12 DC8QN DEFAULT 1 2 Climb MaxTakeoff 12 1 000 DC8QN DEFAULT 1 3 Accelerate MaxTakeoff 12 2 055 160 DC8QN DEFAULT 1 4 Accelerate MaxTakeoff INT 1 541 180 DC8QN DEFAULT 1 5 Accelerate MaxClimb INT 1 000 200 DC8QN DEFAULT 1 6 Climb MaxClimb ZERO 3 000 DC8QN DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 DC8QN DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC8QN DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC8QN DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC8QN DEFAULT 2 1 Takeoff MaxTakeoff 12 DC8QN DEFAULT 2 2 Climb MaxTakeoff 12 1 000 DC8QN DEFAULT 2 3 Accelerate MaxTakeoff 12 1 959 164 DC8QN DEFAULT 2 4 Accelerate MaxTakeoff INT 1 470 184 DC8QN DEFAULT 2 5 Accelerate MaxClimb INT 1 000 204 DC8QN DEFAULT 2 6 Climb MaxClimb ZERO 3 000L 168/590 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC8QN DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC8QN DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC8QN DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC8QN DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC8QN DEFAULT 3 1 Takeoff MaxTakeoff 12 DC8QN DEFAULT 3 2 Climb MaxTakeoff 12 1 000 DC8QN DEFAULT 3 3 Accelerate MaxTakeoff 12 1 827 168 DC8QN DEFAULT 3 4 Accelerate MaxTakeoff INT 1 371 188 DC8QN DEFAULT 3 5 Accelerate MaxClimb INT 1 000 208 DC8QN DEFAULT 3 6 Climb MaxClimb ZERO 3 000 DC8QN DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 DC8QN DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC8QN DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC8QN DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DC8QN DEFAULT 4 1 Takeoff MaxTakeoff 12 DC8QN DEFAULT 4 2 Climb MaxTakeoff 12 1 000 DC8QN DEFAULT 4 3 Accelerate MaxTakeoff 12 1 668 175 DC8QN DEFAULT 4 4 Accelerate MaxTakeoff INT 1 251 195 DC8QN DEFAULT 4 5 Accelerate MaxClimb INT 1 000 215 DC8QN DEFAULT 4 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/591 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC8QN DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 DC8QN DEFAULT 4 8 Climb MaxClimb ZERO 5 500 DC8QN DEFAULT 4 9 Climb MaxClimb ZERO 7 500 DC8QN DEFAULT 4 10 Climb MaxClimb ZERO 10 000 DC8QN DEFAULT 5 1 Takeoff MaxTakeoff 12 DC8QN DEFAULT 5 2 Climb MaxTakeoff 12 1 000 DC8QN DEFAULT 5 3 Accelerate MaxTakeoff 12 1 491 182 DC8QN DEFAULT 5 4 Accelerate MaxTakeoff INT 1 118 202 DC8QN DEFAULT 5 5 Accelerate MaxClimb INT 1 000 222 DC8QN DEFAULT 5 6 Climb MaxClimb ZERO 3 000 DC8QN DEFAULT 5 7 Accelerate MaxClimb ZERO 1 000 250 DC8QN DEFAULT 5 8 Climb MaxClimb ZERO 5 500 DC8QN DEFAULT 5 9 Climb MaxClimb ZERO 7 500 DC8QN DEFAULT 5 10 Climb MaxClimb ZERO 10 000 DC8QN DEFAULT 6 1 Takeoff MaxTakeoff 12 DC8QN DEFAULT 6 2 Climb MaxTakeoff 12 1 000 DC8QN DEFAULT 6 3 Accelerate MaxTakeoff 12 1 394 187 DC8QN DEFAULT 6 4 Accelerate MaxTakeoff INT 1 046 207 DC8QN DEFAULT 6 5 Accelerate MaxClimb INT 1 000 227 DC8QN DEFAULT 6 6 Climb MaxClimb ZERO 3 000L 168/592 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC8QN DEFAULT 6 7 Accelerate MaxClimb ZERO 1 000 250 DC8QN DEFAULT 6 8 Climb MaxClimb ZERO 5 500 DC8QN DEFAULT 6 9 Climb MaxClimb ZERO 7 500 DC8QN DEFAULT 6 10 Climb MaxClimb ZERO 10 000 DC8QN DEFAULT 7 1 Takeoff MaxTakeoff 12 DC8QN DEFAULT 7 2 Climb MaxTakeoff 12 1 000 DC8QN DEFAULT 7 3 Accelerate MaxTakeoff 12 1 275 192 DC8QN DEFAULT 7 4 Accelerate MaxTakeoff INT 956 212 DC8QN DEFAULT 7 5 Accelerate MaxClimb INT 900 232 DC8QN DEFAULT 7 6 Climb MaxClimb ZERO 3 000 DC8QN DEFAULT 7 7 Accelerate MaxClimb ZERO 900 250 DC8QN DEFAULT 7 8 Climb MaxClimb ZERO 5 500 DC8QN DEFAULT 7 9 Climb MaxClimb ZERO 7 500 DC8QN DEFAULT 7 10 Climb MaxClimb ZERO 10 000 DC910 DEFAULT 1 1 Takeoff MaxTakeoff 15 DC910 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 DC910 DEFAULT 1 3 Accelerate MaxTakeoff 15 2 296 136 DC910 DEFAULT 1 4 Accelerate MaxTakeoff 5 1 722 146 DC910 DEFAULT 1 5 Accelerate MaxClimb INT 1 000 181 DC910 DEFAULT 1 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/593 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC910 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 DC910 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC910 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC910 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC910 DEFAULT 2 1 Takeoff MaxTakeoff 15 DC910 DEFAULT 2 2 Climb MaxTakeoff 15 1 000 DC910 DEFAULT 2 3 Accelerate MaxTakeoff 15 2 070 143 DC910 DEFAULT 2 4 Accelerate MaxTakeoff 5 1 553 153 DC910 DEFAULT 2 5 Accelerate MaxClimb INT 1 000 188 DC910 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 DC910 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC910 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC910 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC910 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC910 DEFAULT 3 1 Takeoff MaxTakeoff 15 DC910 DEFAULT 3 2 Climb MaxTakeoff 15 1 000 DC910 DEFAULT 3 3 Accelerate MaxTakeoff 15 1 901 149 DC910 DEFAULT 3 4 Accelerate MaxTakeoff 5 1 426 159 DC910 DEFAULT 3 5 Accelerate MaxClimb INT 1 000 194 DC910 DEFAULT 3 6 Climb MaxClimb ZERO 3 000L 168/594 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC910 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 DC910 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC910 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC910 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DC930 DEFAULT 1 1 Takeoff MaxTakeoff 15 DC930 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 DC930 DEFAULT 1 3 Accelerate MaxTakeoff 15 1 741 154 DC930 DEFAULT 1 4 Accelerate MaxTakeoff 5 1 306 164 DC930 DEFAULT 1 5 Accelerate MaxClimb INT 1 000 199 DC930 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 DC930 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 DC930 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC930 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC930 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC930 DEFAULT 2 1 Takeoff MaxTakeoff 15 DC930 DEFAULT 2 2 Climb MaxTakeoff 15 1 000 DC930 DEFAULT 2 3 Accelerate MaxTakeoff 15 1 559 161 DC930 DEFAULT 2 4 Accelerate MaxTakeoff 5 1 169 171 DC930 DEFAULT 2 5 Accelerate MaxClimb INT 1 000 206 DC930 DEFAULT 2 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/595 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC930 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC930 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC930 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC930 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC930 DEFAULT 3 1 Takeoff MaxTakeoff 15 DC930 DEFAULT 3 2 Climb MaxTakeoff 15 1 000 DC930 DEFAULT 3 3 Accelerate MaxTakeoff 15 1 406 168 DC930 DEFAULT 3 4 Accelerate MaxTakeoff 5 1 055 178 DC930 DEFAULT 3 5 Accelerate MaxClimb INT 1 000 213 DC930 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 DC930 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 DC930 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC930 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC930 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DC93LW DEFAULT 1 1 Takeoff MaxTakeoff 15 DC93LW DEFAULT 1 2 Climb MaxTakeoff 15 1 000 DC93LW DEFAULT 1 3 Accelerate MaxTakeoff 15 1 741 154 DC93LW DEFAULT 1 4 Accelerate MaxTakeoff 5 1 306 164 DC93LW DEFAULT 1 5 Accelerate MaxClimb INT 1 000 199 DC93LW DEFAULT 1 6 Climb MaxClimb ZERO 3 000L 168/596 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC93LW DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 DC93LW DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC93LW DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC93LW DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC93LW DEFAULT 2 1 Takeoff MaxTakeoff 15 DC93LW DEFAULT 2 2 Climb MaxTakeoff 15 1 000 DC93LW DEFAULT 2 3 Accelerate MaxTakeoff 15 1 559 161 DC93LW DEFAULT 2 4 Accelerate MaxTakeoff 5 1 169 171 DC93LW DEFAULT 2 5 Accelerate MaxClimb INT 1 000 206 DC93LW DEFAULT 2 6 Climb MaxClimb ZERO 3 000 DC93LW DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC93LW DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC93LW DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC93LW DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC93LW DEFAULT 3 1 Takeoff MaxTakeoff 15 DC93LW DEFAULT 3 2 Climb MaxTakeoff 15 1 000 DC93LW DEFAULT 3 3 Accelerate MaxTakeoff 15 1 406 168 DC93LW DEFAULT 3 4 Accelerate MaxTakeoff 5 1 055 178 DC93LW DEFAULT 3 5 Accelerate MaxClimb INT 1 000 213 DC93LW DEFAULT 3 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/597 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC93LW DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 DC93LW DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC93LW DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC93LW DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DC950 DEFAULT 1 1 Takeoff MaxTakeoff 15 DC950 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 DC950 DEFAULT 1 3 Accelerate MaxTakeoff 15 1 983 159 DC950 DEFAULT 1 4 Accelerate MaxTakeoff 5 1 487 169 DC950 DEFAULT 1 5 Accelerate MaxClimb INTR 1 000 204 DC950 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 DC950 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 DC950 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC950 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC950 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC950 DEFAULT 2 1 Takeoff MaxTakeoff 15 DC950 DEFAULT 2 2 Climb MaxTakeoff 15 1 000 DC950 DEFAULT 2 3 Accelerate MaxTakeoff 15 1 843 164 DC950 DEFAULT 2 4 Accelerate MaxTakeoff 5 1 382 174 DC950 DEFAULT 2 5 Accelerate MaxClimb INTR 1 000 209 DC950 DEFAULT 2 6 Climb MaxClimb ZERO 3 000L 168/598 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC950 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC950 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC950 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC950 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC950 DEFAULT 3 1 Takeoff MaxTakeoff 15 DC950 DEFAULT 3 2 Climb MaxTakeoff 15 1 000 DC950 DEFAULT 3 3 Accelerate MaxTakeoff 15 1 698 170 DC950 DEFAULT 3 4 Accelerate MaxTakeoff 5 1 274 180 DC950 DEFAULT 3 5 Accelerate MaxClimb INTR 1 000 215 DC950 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 DC950 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 DC950 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC950 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC950 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DC95HW DEFAULT 1 1 Takeoff MaxTakeoff 15 DC95HW DEFAULT 1 2 Climb MaxTakeoff 15 1 000 DC95HW DEFAULT 1 3 Accelerate MaxTakeoff 15 1 983 159 DC95HW DEFAULT 1 4 Accelerate MaxTakeoff 5 1 487 169 DC95HW DEFAULT 1 5 Accelerate MaxClimb INTR 1 000 204 DC95HW DEFAULT 1 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/599 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC95HW DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 DC95HW DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC95HW DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC95HW DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC95HW DEFAULT 2 1 Takeoff MaxTakeoff 15 DC95HW DEFAULT 2 2 Climb MaxTakeoff 15 1 000 DC95HW DEFAULT 2 3 Accelerate MaxTakeoff 15 1 843 164 DC95HW DEFAULT 2 4 Accelerate MaxTakeoff 5 1 382 174 DC95HW DEFAULT 2 5 Accelerate MaxClimb INTR 1 000 209 DC95HW DEFAULT 2 6 Climb MaxClimb ZERO 3 000 DC95HW DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC95HW DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC95HW DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC95HW DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC95HW DEFAULT 3 1 Takeoff MaxTakeoff 15 DC95HW DEFAULT 3 2 Climb MaxTakeoff 15 1 000 DC95HW DEFAULT 3 3 Accelerate MaxTakeoff 15 1 698 170 DC95HW DEFAULT 3 4 Accelerate MaxTakeoff 5 1 274 180 DC95HW DEFAULT 3 5 Accelerate MaxClimb INTR 1 000 215 DC95HW DEFAULT 3 6 Climb MaxClimb ZERO 3 000L 168/600 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC95HW DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 DC95HW DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC95HW DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC95HW DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DC9Q7 DEFAULT 1 1 Takeoff MaxTakeoff 15 DC9Q7 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 DC9Q7 DEFAULT 1 3 Accelerate MaxTakeoff 15 2 296 136 DC9Q7 DEFAULT 1 4 Accelerate MaxTakeoff 5 1 722 146 DC9Q7 DEFAULT 1 5 Accelerate MaxClimb INT 1 000 181 DC9Q7 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 DC9Q7 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 DC9Q7 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC9Q7 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC9Q7 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC9Q7 DEFAULT 2 1 Takeoff MaxTakeoff 15 DC9Q7 DEFAULT 2 2 Climb MaxTakeoff 15 1 000 DC9Q7 DEFAULT 2 3 Accelerate MaxTakeoff 15 2 070 143 DC9Q7 DEFAULT 2 4 Accelerate MaxTakeoff 5 1 553 153 DC9Q7 DEFAULT 2 5 Accelerate MaxClimb INT 1 000 188 DC9Q7 DEFAULT 2 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/601 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC9Q7 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC9Q7 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC9Q7 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC9Q7 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC9Q7 DEFAULT 3 1 Takeoff MaxTakeoff 15 DC9Q7 DEFAULT 3 2 Climb MaxTakeoff 15 1 000 DC9Q7 DEFAULT 3 3 Accelerate MaxTakeoff 15 1 901 149 DC9Q7 DEFAULT 3 4 Accelerate MaxTakeoff 5 1 426 159 DC9Q7 DEFAULT 3 5 Accelerate MaxClimb INT 1 000 194 DC9Q7 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 DC9Q7 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 DC9Q7 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC9Q7 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC9Q7 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DC9Q9 DEFAULT 1 1 Takeoff MaxTakeoff 15 DC9Q9 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 DC9Q9 DEFAULT 1 3 Accelerate MaxTakeoff 15 1 741 154 DC9Q9 DEFAULT 1 4 Accelerate MaxTakeoff 5 1 306 164 DC9Q9 DEFAULT 1 5 Accelerate MaxClimb INT 1 000 199 DC9Q9 DEFAULT 1 6 Climb MaxClimb ZERO 3 000L 168/602 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC9Q9 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 DC9Q9 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 DC9Q9 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 DC9Q9 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 DC9Q9 DEFAULT 2 1 Takeoff MaxTakeoff 15 DC9Q9 DEFAULT 2 2 Climb MaxTakeoff 15 1 000 DC9Q9 DEFAULT 2 3 Accelerate MaxTakeoff 15 1 559 161 DC9Q9 DEFAULT 2 4 Accelerate MaxTakeoff 5 1 169 171 DC9Q9 DEFAULT 2 5 Accelerate MaxClimb INT 1 000 206 DC9Q9 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 DC9Q9 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 DC9Q9 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 DC9Q9 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 DC9Q9 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 DC9Q9 DEFAULT 3 1 Takeoff MaxTakeoff 15 DC9Q9 DEFAULT 3 2 Climb MaxTakeoff 15 1 000 DC9Q9 DEFAULT 3 3 Accelerate MaxTakeoff 15 1 406 168 DC9Q9 DEFAULT 3 4 Accelerate MaxTakeoff 5 1 055 178 DC9Q9 DEFAULT 3 5 Accelerate MaxClimb INT 1 000 213 DC9Q9 DEFAULT 3 6 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/603 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DC9Q9 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 DC9Q9 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 DC9Q9 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 DC9Q9 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 DHC6 DEFAULT 1 1 Takeoff MaxTakeoff TO DHC6 DEFAULT 1 2 Climb MaxTakeoff TO 1 000 DHC6 DEFAULT 1 3 Accelerate MaxTakeoff TO 952 98 DHC6 DEFAULT 1 4 Climb MaxClimb ZERO 3 000 DHC6 DEFAULT 1 5 Climb MaxClimb ZERO 5 500 DHC6 DEFAULT 1 6 Climb MaxClimb ZERO 7 500 DHC6 DEFAULT 1 7 Climb MaxClimb ZERO 10 000 DHC6QP DEFAULT 1 1 Takeoff MaxTakeoff TO DHC6QP DEFAULT 1 2 Climb MaxTakeoff TO 1 000 DHC6QP DEFAULT 1 3 Accelerate MaxTakeoff TO 952 98 DHC6QP DEFAULT 1 4 Climb MaxClimb ZERO 3 000 DHC6QP DEFAULT 1 5 Climb MaxClimb ZERO 5 500 DHC6QP DEFAULT 1 6 Climb MaxClimb ZERO 7 500 DHC6QP DEFAULT 1 7 Climb MaxClimb ZERO 10 000 DHC7 DEFAULT 1 1 Takeoff MaxTakeoff 25 DHC7 DEFAULT 1 2 Climb MaxTakeoff 25 1 000L 168/604 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DHC7 DEFAULT 1 3 Accelerate MaxTakeoff 25 933 102 DHC7 DEFAULT 1 4 Accelerate MaxTakeoff 10 700 122 DHC7 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 DHC7 DEFAULT 1 6 Accelerate MaxClimb ZERO 700 160 DHC7 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 DHC7 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 DHC7 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 DHC8 DEFAULT 1 1 Takeoff MaxTakeoff 15 DHC8 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 DHC8 DEFAULT 1 3 Accelerate MaxTakeoff 15 1 491 110 DHC8 DEFAULT 1 4 Accelerate MaxClimb 5 1 119 125 DHC8 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 DHC8 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 119 165 DHC8 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 DHC8 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 DHC8 DEFAULT 1 9 Climb MaxClimb ZERO 10 0001.7.2015 EN Official Journal of the European Union L 168/605 Table I-4 (part 4) Default departures procedural steps Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DHC830 DEFAULT 1 1 Takeoff MaxTakeoff 10 DHC830 DEFAULT 1 2 Climb MaxTakeoff 10 1 000 DHC830 DEFAULT 1 3 Accelerate MaxTakeoff 10 1 280 122 DHC830 DEFAULT 1 4 Accelerate MaxClimb 5 960 137 DHC830 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 DHC830 DEFAULT 1 6 Accelerate MaxClimb ZERO 960 179 DHC830 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 DHC830 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 DHC830 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 DO228 DEFAULT 1 1 Takeoff MaxTakeoff FLAPS1 DO228 DEFAULT 1 2 Accelerate MaxTakeoff FLAPS1 1 000 101 DO228 DEFAULT 1 3 Climb MaxTakeoff ZERO 1 000 DO228 DEFAULT 1 4 Accelerate MaxClimb ZERO 1 000 122 DO228 DEFAULT 1 5 Climb MaxClimb ZERO 2 000 DO228 DEFAULT 1 6 Climb MaxClimb ZERO 4 000 DO228 DEFAULT 1 7 Climb MaxClimb ZERO 6 000 DO228 DEFAULT 1 8 Climb MaxClimb ZERO 8 000 DO228 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 DO328 DEFAULT 1 1 Takeoff MaxTakeoff F12-D DO328 DEFAULT 1 2 Accelerate MaxTakeoff F12-D 1 000 120L 168/606 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) DO328 DEFAULT 1 3 Climb MaxTakeoff ZERO 1 000 DO328 DEFAULT 1 4 Accelerate MaxTakeoff ZERO 1 000 130 DO328 DEFAULT 1 5 Climb MaxClimb ZERO 2 000 DO328 DEFAULT 1 6 Climb MaxClimb ZERO 4 000 DO328 DEFAULT 1 7 Climb MaxClimb ZERO 6 000 DO328 DEFAULT 1 8 Climb MaxClimb ZERO 8 000 DO328 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 ECLIPSE500 DEFAULT 1 1 Takeoff MaxTakeoff TO_DN ECLIPSE500 DEFAULT 1 2 Climb MaxTakeoff TO_DN 200 ECLIPSE500 DEFAULT 1 3 Climb MaxTakeoff TO_UP 400 ECLIPSE500 DEFAULT 1 4 Accelerate MaxClimb UP_UP 1 972,9 114 ECLIPSE500 DEFAULT 1 5 Accelerate MaxClimb UP_UP 2 153,3 130,7 ECLIPSE500 DEFAULT 1 6 Accelerate MaxClimb UP_UP 2 276 145,3 ECLIPSE500 DEFAULT 1 7 Accelerate MaxClimb UP_UP 2 313,3 158,2 ECLIPSE500 DEFAULT 1 8 Accelerate MaxClimb UP_UP 2 288,2 170 ECLIPSE500 DEFAULT 1 9 Climb Reduce­ UP_UP 6 000 Climb ECLIPSE500 DEFAULT 1 10 Climb Reduce­ UP_UP 8 000 Climb ECLIPSE500 DEFAULT 1 11 Climb Reduce­ UP_UP 10 000 Climb ECLIPSE500 DEFAULT 2 1 Takeoff MaxTakeoff TO_DN ECLIPSE500 DEFAULT 2 2 Climb MaxTakeoff TO_DN 2001.7.2015 EN Official Journal of the European Union L 168/607 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) ECLIPSE500 DEFAULT 2 3 Climb MaxTakeoff TO_UP 400 ECLIPSE500 DEFAULT 2 4 Accelerate MaxClimb UP_UP 1 803,3 114,8 ECLIPSE500 DEFAULT 2 5 Accelerate MaxClimb UP_UP 1 971,7 131,2 ECLIPSE500 DEFAULT 2 6 Accelerate MaxClimb UP_UP 2 087,6 145,6 ECLIPSE500 DEFAULT 2 7 Accelerate MaxClimb UP_UP 2 124,1 158,4 ECLIPSE500 DEFAULT 2 8 Accelerate MaxClimb UP_UP 2 102,8 170 ECLIPSE500 DEFAULT 2 9 Climb Reduce­ UP_UP 6 000 Climb ECLIPSE500 DEFAULT 2 10 Climb Reduce­ UP_UP 8 000 Climb ECLIPSE500 DEFAULT 2 11 Climb Reduce­ UP_UP 10 000 Climb ECLIPSE500 DEFAULT 3 1 Takeoff MaxTakeoff TO_DN ECLIPSE500 DEFAULT 3 2 Climb MaxTakeoff TO_DN 200 ECLIPSE500 DEFAULT 3 3 Climb MaxTakeoff TO_UP 400 ECLIPSE500 DEFAULT 3 4 Accelerate MaxClimb UP_UP 1 760,4 115 ECLIPSE500 DEFAULT 3 5 Accelerate MaxClimb UP_UP 1 926,2 131,4 ECLIPSE500 DEFAULT 3 6 Accelerate MaxClimb UP_UP 2 039,6 145,7 ECLIPSE500 DEFAULT 3 7 Accelerate MaxClimb UP_UP 2 075,3 158,4 ECLIPSE500 DEFAULT 3 8 Accelerate MaxClimb UP_UP 2 054,5 170 ECLIPSE500 DEFAULT 3 9 Climb Reduce­ UP_UP 6 000 Climb ECLIPSE500 DEFAULT 3 10 Climb Reduce­ UP_UP 8 000 Climb ECLIPSE500 DEFAULT 3 11 Climb Reduce­ UP_UP 10 000 ClimbL 168/608 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) ECLIPSE500 HI_ALT 1 1 Takeoff MaxTakeoff TO_DN ECLIPSE500 HI_ALT 1 2 Climb MaxTakeoff TO_DN 200 ECLIPSE500 HI_ALT 1 3 Climb MaxTakeoff TO_UP 400 ECLIPSE500 HI_ALT 1 4 Accelerate Reduce­ UP_UP 1 798,3 113,9 Climb ECLIPSE500 HI_ALT 1 5 Accelerate Reduce­ UP_UP 1 951,8 130,7 Climb ECLIPSE500 HI_ALT 1 6 Accelerate Reduce­ UP_UP 2 043,9 145,3 Climb ECLIPSE500 HI_ALT 1 7 Accelerate Reduce­ UP_UP 2 054,7 158,2 Climb ECLIPSE500 HI_ALT 1 8 Accelerate Reduce­ UP_UP 1 998,7 170 Climb ECLIPSE500 HI_ALT 1 9 Climb Reduce­ UP_UP 6 000 Climb ECLIPSE500 HI_ALT 1 10 Climb Reduce­ UP_UP 8 000 Climb ECLIPSE500 HI_ALT 1 11 Climb Reduce­ UP_UP 10 000 Climb ECLIPSE500 HI_ALT 2 1 Takeoff MaxTakeoff TO_DN ECLIPSE500 HI_ALT 2 2 Climb MaxTakeoff TO_DN 200 ECLIPSE500 HI_ALT 2 3 Climb MaxTakeoff TO_UP 400 ECLIPSE500 HI_ALT 2 4 Accelerate Reduce­ UP_UP 1 637 114,8 Climb ECLIPSE500 HI_ALT 2 5 Accelerate Reduce­ UP_UP 1 780,8 131,2 Climb ECLIPSE500 HI_ALT 2 6 Accelerate Reduce­ UP_UP 1 868,3 145,6 Climb ECLIPSE500 HI_ALT 2 7 Accelerate Reduce­ UP_UP 1 880,3 158,4 Climb ECLIPSE500 HI_ALT 2 8 Accelerate Reduce­ UP_UP 1 838,2 170 Climb ECLIPSE500 HI_ALT 2 9 Climb Reduce­ UP_UP 6 000 Climb1.7.2015 EN Official Journal of the European Union L 168/609 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) ECLIPSE500 HI_ALT 2 10 Climb Reduce­ UP_UP 8 000 Climb ECLIPSE500 HI_ALT 2 11 Climb Reduce­ UP_UP 10 000 Climb ECLIPSE500 HI_ALT 3 1 Takeoff MaxTakeoff TO_DN ECLIPSE500 HI_ALT 3 2 Climb MaxTakeoff TO_DN 200 ECLIPSE500 HI_ALT 3 3 Climb MaxTakeoff TO_UP 400 ECLIPSE500 HI_ALT 3 4 Accelerate Reduce­ UP_UP 1 595,5 115 Climb ECLIPSE500 HI_ALT 3 5 Accelerate Reduce­ UP_UP 1 736,8 131,4 Climb ECLIPSE500 HI_ALT 3 6 Accelerate Reduce­ UP_UP 1 823,1 145,6 Climb ECLIPSE500 HI_ALT 3 7 Accelerate Reduce­ UP_UP 1 835,6 158,4 Climb ECLIPSE500 HI_ALT 3 8 Accelerate Reduce­ UP_UP 1 794,8 170 Climb ECLIPSE500 HI_ALT 3 9 Climb Reduce­ UP_UP 6 000 Climb ECLIPSE500 HI_ALT 3 10 Climb Reduce­ UP_UP 8 000 Climb ECLIPSE500 HI_ALT 3 11 Climb Reduce­ UP_UP 10 000 Climb EMB120 DEFAULT 1 1 Takeoff MaxTakeoff 15 EMB120 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 EMB120 DEFAULT 1 3 Accelerate MaxTakeoff 15 460 130 EMB120 DEFAULT 1 4 Accelerate MaxTakeoff ZERO 345 135 EMB120 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 143 EMB120 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 EMB120 DEFAULT 1 7 Climb MaxClimb ZERO 5 500L 168/610 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB120 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 EMB120 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 EMB145 DEFAULT 1 1 Takeoff MaxTakeoff 9-GEAR EMB145 DEFAULT 1 2 Climb MaxTakeoff 9 1 000 EMB145 DEFAULT 1 3 Accelerate MaxClimb ZERO 1 367 220 EMB145 DEFAULT 1 4 Climb MaxClimb ZERO 3 000 EMB145 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 250 EMB145 DEFAULT 1 6 Climb MaxClimb ZERO 5 500 EMB145 DEFAULT 1 7 Climb MaxClimb ZERO 7 500 EMB145 DEFAULT 1 8 Climb MaxClimb ZERO 10 000 EMB145 DEFAULT 2 1 Takeoff MaxTakeoff 9-GEAR EMB145 DEFAULT 2 2 Climb MaxTakeoff 9 1 000 EMB145 DEFAULT 2 3 Accelerate MaxClimb ZERO 1 334 220 EMB145 DEFAULT 2 4 Climb MaxClimb ZERO 3 000 EMB145 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 250 EMB145 DEFAULT 2 6 Climb MaxClimb ZERO 5 500 EMB145 DEFAULT 2 7 Climb MaxClimb ZERO 7 500 EMB145 DEFAULT 2 8 Climb MaxClimb ZERO 10 000 EMB145 DEFAULT 3 1 Takeoff MaxTakeoff 9-GEAR EMB145 DEFAULT 3 2 Climb MaxTakeoff 9 1 0001.7.2015 EN Official Journal of the European Union L 168/611 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB145 DEFAULT 3 3 Accelerate MaxClimb ZERO 1 315 220 EMB145 DEFAULT 3 4 Climb MaxClimb ZERO 3 000 EMB145 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 250 EMB145 DEFAULT 3 6 Climb MaxClimb ZERO 5 500 EMB145 DEFAULT 3 7 Climb MaxClimb ZERO 7 500 EMB145 DEFAULT 3 8 Climb MaxClimb ZERO 10 000 EMB145 DEFAULT 4 1 Takeoff MaxTakeoff 9-GEAR EMB145 DEFAULT 4 2 Climb MaxTakeoff 9 1 000 EMB145 DEFAULT 4 3 Accelerate MaxClimb ZERO 1 293 220 EMB145 DEFAULT 4 4 Climb MaxClimb ZERO 3 200 EMB145 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 250 EMB145 DEFAULT 4 6 Climb MaxClimb ZERO 5 500 EMB145 DEFAULT 4 7 Climb MaxClimb ZERO 7 500 EMB145 DEFAULT 4 8 Climb MaxClimb ZERO 10 000 EMB14L DEFAULT 1 1 Takeoff MaxTakeoff 9-GEAR EMB14L DEFAULT 1 2 Climb MaxTakeoff 9 1 000 EMB14L DEFAULT 1 3 Accelerate MaxClimb ZERO 1 465 220 EMB14L DEFAULT 1 4 Climb MaxClimb ZERO 3 000 EMB14L DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 250 EMB14L DEFAULT 1 6 Climb MaxClimb ZERO 5 500L 168/612 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB14L DEFAULT 1 7 Climb MaxClimb ZERO 7 500 EMB14L DEFAULT 1 8 Climb MaxClimb ZERO 10 000 EMB14L DEFAULT 2 1 Takeoff MaxTakeoff 9-GEAR EMB14L DEFAULT 2 2 Climb MaxTakeoff 9 1 000 EMB14L DEFAULT 2 3 Accelerate MaxClimb ZERO 1 420 220 EMB14L DEFAULT 2 4 Climb MaxClimb ZERO 3 000 EMB14L DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 250 EMB14L DEFAULT 2 6 Climb MaxClimb ZERO 5 500 EMB14L DEFAULT 2 7 Climb MaxClimb ZERO 7 500 EMB14L DEFAULT 2 8 Climb MaxClimb ZERO 10 000 EMB14L DEFAULT 3 1 Takeoff MaxTakeoff 9-GEAR EMB14L DEFAULT 3 2 Climb MaxTakeoff 9 1 000 EMB14L DEFAULT 3 3 Accelerate MaxClimb ZERO 1 395 220 EMB14L DEFAULT 3 4 Climb MaxClimb ZERO 3 000 EMB14L DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 250 EMB14L DEFAULT 3 6 Climb MaxClimb ZERO 5 500 EMB14L DEFAULT 3 7 Climb MaxClimb ZERO 7 500 EMB14L DEFAULT 3 8 Climb MaxClimb ZERO 10 000 EMB14L DEFAULT 4 1 Takeoff MaxTakeoff 9-GEAR EMB14L DEFAULT 4 2 Climb MaxTakeoff 9 1 0001.7.2015 EN Official Journal of the European Union L 168/613 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB14L DEFAULT 4 3 Accelerate MaxClimb ZERO 1 366 220 EMB14L DEFAULT 4 4 Climb MaxClimb ZERO 3 000 EMB14L DEFAULT 4 5 Accelerate MaxClimb ZERO 1 000 250 EMB14L DEFAULT 4 6 Climb MaxClimb ZERO 5 500 EMB14L DEFAULT 4 7 Climb MaxClimb ZERO 7 500 EMB14L DEFAULT 4 8 Climb MaxClimb ZERO 10 000 EMB14L DEFAULT 5 1 Takeoff MaxTakeoff 9-GEAR EMB14L DEFAULT 5 2 Climb MaxTakeoff 9 1 000 EMB14L DEFAULT 5 3 Accelerate MaxClimb ZERO 1 335 220 EMB14L DEFAULT 5 4 Climb MaxClimb ZERO 3 000 EMB14L DEFAULT 5 5 Accelerate MaxClimb ZERO 1 000 250 EMB14L DEFAULT 5 6 Climb MaxClimb ZERO 5 500 EMB14L DEFAULT 5 7 Climb MaxClimb ZERO 7 500 EMB14L DEFAULT 5 8 Climb MaxClimb ZERO 10 000 EMB14L DEFAULT 6 1 Takeoff MaxTakeoff 9-GEAR EMB14L DEFAULT 6 2 Climb MaxTakeoff 9 1 000 EMB14L DEFAULT 6 3 Accelerate MaxClimb ZERO 1 298 220 EMB14L DEFAULT 6 4 Climb MaxClimb ZERO 3 000 EMB14L DEFAULT 6 5 Accelerate MaxClimb ZERO 1 000 250 EMB14L DEFAULT 6 6 Climb MaxClimb ZERO 5 500L 168/614 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB14L DEFAULT 6 7 Climb MaxClimb ZERO 7 500 EMB14L DEFAULT 6 8 Climb MaxClimb ZERO 10 000 EMB170 DEFAULT 1 1 Takeoff MaxTakeoff 1 EMB170 DEFAULT 1 2 Climb MaxTakeoff 1 1 000 EMB170 DEFAULT 1 3 Accelerate MaxClimb ZERO 1 936 196 EMB170 DEFAULT 1 4 Climb MaxClimb ZERO 3 000 EMB170 DEFAULT 1 5 Accelerate MaxClimb ZERO 2 339 240 EMB170 DEFAULT 1 6 Climb MaxClimb ZERO 5 500 EMB170 DEFAULT 1 7 Climb MaxClimb ZERO 7 500 EMB170 DEFAULT 1 8 Climb MaxClimb ZERO 10 000 EMB170 DEFAULT 2 1 Takeoff MaxTakeoff 1 EMB170 DEFAULT 2 2 Climb MaxTakeoff 1 1 000 EMB170 DEFAULT 2 3 Accelerate MaxClimb ZERO 1 836 197,1 EMB170 DEFAULT 2 4 Climb MaxClimb ZERO 3 000 EMB170 DEFAULT 2 5 Accelerate MaxClimb ZERO 2 228 240 EMB170 DEFAULT 2 6 Climb MaxClimb ZERO 5 500 EMB170 DEFAULT 2 7 Climb MaxClimb ZERO 7 500 EMB170 DEFAULT 2 8 Climb MaxClimb ZERO 10 000 EMB170 DEFAULT 3 1 Takeoff MaxTakeoff 1 EMB170 DEFAULT 3 2 Climb MaxTakeoff 1 1 0001.7.2015 EN Official Journal of the European Union L 168/615 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB170 DEFAULT 3 3 Accelerate MaxClimb ZERO 1 772 200,9 EMB170 DEFAULT 3 4 Climb MaxClimb ZERO 3 000 EMB170 DEFAULT 3 5 Accelerate MaxClimb ZERO 2 120 240 EMB170 DEFAULT 3 6 Climb MaxClimb ZERO 5 500 EMB170 DEFAULT 3 7 Climb MaxClimb ZERO 7 500 EMB170 DEFAULT 3 8 Climb MaxClimb ZERO 10 000 EMB170 ICAO_A 1 1 Takeoff MaxTakeoff 1 EMB170 ICAO_A 1 2 Climb MaxTakeoff 1 1 500 EMB170 ICAO_A 1 3 Climb MaxClimb 1 3 000 EMB170 ICAO_A 1 4 Accelerate MaxClimb ZERO 1 650 195 EMB170 ICAO_A 1 5 Accelerate MaxClimb ZERO 2 035 240 EMB170 ICAO_A 1 6 Climb MaxClimb ZERO 5 500 EMB170 ICAO_A 1 7 Climb MaxClimb ZERO 7 500 EMB170 ICAO_A 1 8 Climb MaxClimb ZERO 10 000 EMB170 ICAO_A 2 1 Takeoff MaxTakeoff 1 EMB170 ICAO_A 2 2 Climb MaxTakeoff 1 1 500 EMB170 ICAO_A 2 3 Climb MaxClimb 1 3 000 EMB170 ICAO_A 2 4 Accelerate MaxClimb ZERO 1 617 198,1 EMB170 ICAO_A 2 5 Accelerate MaxClimb ZERO 1 944 240 EMB170 ICAO_A 2 6 Climb MaxClimb ZERO 5 500L 168/616 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB170 ICAO_A 2 7 Climb MaxClimb ZERO 7 500 EMB170 ICAO_A 2 8 Climb MaxClimb ZERO 10 000 EMB170 ICAO_A 3 1 Takeoff MaxTakeoff 1 EMB170 ICAO_A 3 2 Climb MaxTakeoff 1 1 500 EMB170 ICAO_A 3 3 Climb MaxClimb 1 3 000 EMB170 ICAO_A 3 4 Accelerate MaxClimb ZERO 1 546 200,4 EMB170 ICAO_A 3 5 Accelerate MaxClimb ZERO 1 850 240 EMB170 ICAO_A 3 6 Climb MaxClimb ZERO 5 500 EMB170 ICAO_A 3 7 Climb MaxClimb ZERO 7 500 EMB170 ICAO_A 3 8 Climb MaxClimb ZERO 10 000 EMB170 ICAO_B 1 1 Takeoff MaxTakeoff 1 EMB170 ICAO_B 1 2 Climb MaxTakeoff 1 1 000 EMB170 ICAO_B 1 3 Accelerate MaxTakeoff ZERO 1 899 195,5 EMB170 ICAO_B 1 4 Climb MaxClimb ZERO 3 000 EMB170 ICAO_B 1 5 Accelerate MaxClimb ZERO 2 301 240 EMB170 ICAO_B 1 6 Climb MaxClimb ZERO 5 500 EMB170 ICAO_B 1 7 Climb MaxClimb ZERO 7 500 EMB170 ICAO_B 1 8 Climb MaxClimb ZERO 10 000 EMB170 ICAO_B 2 1 Takeoff MaxTakeoff 1 EMB170 ICAO_B 2 2 Climb MaxTakeoff 1 1 0001.7.2015 EN Official Journal of the European Union L 168/617 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB170 ICAO_B 2 3 Accelerate MaxTakeoff ZERO 1 823 198,2 EMB170 ICAO_B 2 4 Climb MaxClimb ZERO 3 000 EMB170 ICAO_B 2 5 Accelerate MaxClimb ZERO 2 195 240 EMB170 ICAO_B 2 6 Climb MaxClimb ZERO 5 500 EMB170 ICAO_B 2 7 Climb MaxClimb ZERO 7 500 EMB170 ICAO_B 2 8 Climb MaxClimb ZERO 10 000 EMB170 ICAO_B 3 1 Takeoff MaxTakeoff 1 EMB170 ICAO_B 3 2 Climb MaxTakeoff 1 1 000 EMB170 ICAO_B 3 3 Accelerate MaxTakeoff ZERO 1 743 201 EMB170 ICAO_B 3 4 Climb MaxClimb ZERO 3 000 EMB170 ICAO_B 3 5 Accelerate MaxClimb ZERO 2 085 240 EMB170 ICAO_B 3 6 Climb MaxClimb ZERO 5 500 EMB170 ICAO_B 3 7 Climb MaxClimb ZERO 7 500 EMB170 ICAO_B 3 8 Climb MaxClimb ZERO 10 000 EMB175 DEFAULT 1 1 Takeoff MaxTakeoff 1 EMB175 DEFAULT 1 2 Climb MaxTakeoff 1 1 000 EMB175 DEFAULT 1 3 Accelerate MaxClimb ZERO 1 900 196 EMB175 DEFAULT 1 4 Climb MaxClimb ZERO 3 000 EMB175 DEFAULT 1 5 Accelerate MaxClimb ZERO 2 308 240 EMB175 DEFAULT 1 6 Climb MaxClimb ZERO 5 500L 168/618 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB175 DEFAULT 1 7 Climb MaxClimb ZERO 7 500 EMB175 DEFAULT 1 8 Climb MaxClimb ZERO 10 000 EMB175 DEFAULT 2 1 Takeoff MaxTakeoff 1 EMB175 DEFAULT 2 2 Climb MaxTakeoff 1 1 000 EMB175 DEFAULT 2 3 Accelerate MaxClimb ZERO 1 823 198,1 EMB175 DEFAULT 2 4 Climb MaxClimb ZERO 3 000 EMB175 DEFAULT 2 5 Accelerate MaxClimb ZERO 2 190 240 EMB175 DEFAULT 2 6 Climb MaxClimb ZERO 5 500 EMB175 DEFAULT 2 7 Climb MaxClimb ZERO 7 500 EMB175 DEFAULT 2 8 Climb MaxClimb ZERO 10 000 EMB175 DEFAULT 3 1 Takeoff MaxTakeoff 1 EMB175 DEFAULT 3 2 Climb MaxTakeoff 1 1 000 EMB175 DEFAULT 3 3 Accelerate MaxClimb ZERO 1 745 200,3 EMB175 DEFAULT 3 4 Climb MaxClimb ZERO 3 000 EMB175 DEFAULT 3 5 Accelerate MaxClimb ZERO 2 086 240 EMB175 DEFAULT 3 6 Climb MaxClimb ZERO 5 500 EMB175 DEFAULT 3 7 Climb MaxClimb ZERO 7 500 EMB175 DEFAULT 3 8 Climb MaxClimb ZERO 10 000 EMB175 ICAO_A 1 1 Takeoff MaxTakeoff 1 EMB175 ICAO_A 1 2 Climb MaxTakeoff 1 1 5001.7.2015 EN Official Journal of the European Union L 168/619 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB175 ICAO_A 1 3 Climb MaxClimb 1 3 000 EMB175 ICAO_A 1 4 Accelerate MaxClimb ZERO 1 634 195 EMB175 ICAO_A 1 5 Accelerate MaxClimb ZERO 1 979 240 EMB175 ICAO_A 1 6 Climb MaxClimb ZERO 5 500 EMB175 ICAO_A 1 7 Climb MaxClimb ZERO 7 500 EMB175 ICAO_A 1 8 Climb MaxClimb ZERO 10 000 EMB175 ICAO_A 2 1 Takeoff MaxTakeoff 1 EMB175 ICAO_A 2 2 Climb MaxTakeoff 1 1 500 EMB175 ICAO_A 2 3 Climb MaxClimb 1 3 000 EMB175 ICAO_A 2 4 Accelerate MaxClimb ZERO 1 568 198,5 EMB175 ICAO_A 2 5 Accelerate MaxClimb ZERO 1 885 240 EMB175 ICAO_A 2 6 Climb MaxClimb ZERO 5 500 EMB175 ICAO_A 2 7 Climb MaxClimb ZERO 7 500 EMB175 ICAO_A 2 8 Climb MaxClimb ZERO 10 000 EMB175 ICAO_A 3 1 Takeoff MaxTakeoff 1 EMB175 ICAO_A 3 2 Climb MaxTakeoff 1 1 500 EMB175 ICAO_A 3 3 Climb MaxClimb 1 3 000 EMB175 ICAO_A 3 4 Accelerate MaxClimb ZERO 1 499 201,3 EMB175 ICAO_A 3 5 Accelerate MaxClimb ZERO 1 794 240 EMB175 ICAO_A 3 6 Climb MaxClimb ZERO 5 500L 168/620 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB175 ICAO_A 3 7 Climb MaxClimb ZERO 7 500 EMB175 ICAO_A 3 8 Climb MaxClimb ZERO 10 000 EMB175 ICAO_B 1 1 Takeoff MaxTakeoff 1 EMB175 ICAO_B 1 2 Climb MaxTakeoff 1 1 000 EMB175 ICAO_B 1 3 Accelerate MaxTakeoff ZERO 1 818 195,5 EMB175 ICAO_B 1 4 Climb MaxClimb ZERO 3 000 EMB175 ICAO_B 1 5 Accelerate MaxClimb ZERO 2 202 240 EMB175 ICAO_B 1 6 Climb MaxClimb ZERO 5 500 EMB175 ICAO_B 1 7 Climb MaxClimb ZERO 7 500 EMB175 ICAO_B 1 8 Climb MaxClimb ZERO 10 000 EMB175 ICAO_B 2 1 Takeoff MaxTakeoff 1 EMB175 ICAO_B 2 2 Climb MaxTakeoff 1 1 000 EMB175 ICAO_B 2 3 Accelerate MaxTakeoff ZERO 1 744 197,1 EMB175 ICAO_B 2 4 Climb MaxClimb ZERO 3 000 EMB175 ICAO_B 2 5 Accelerate MaxClimb ZERO 2 099 240 EMB175 ICAO_B 2 6 Climb MaxClimb ZERO 5 500 EMB175 ICAO_B 2 7 Climb MaxClimb ZERO 7 500 EMB175 ICAO_B 2 8 Climb MaxClimb ZERO 10 000 EMB175 ICAO_B 3 1 Takeoff MaxTakeoff 1 EMB175 ICAO_B 3 2 Climb MaxTakeoff 1 1 0001.7.2015 EN Official Journal of the European Union L 168/621 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB175 ICAO_B 3 3 Accelerate MaxTakeoff ZERO 1 668 200,8 EMB175 ICAO_B 3 4 Climb MaxClimb ZERO 3 000 EMB175 ICAO_B 3 5 Accelerate MaxClimb ZERO 1 996 240 EMB175 ICAO_B 3 6 Climb MaxClimb ZERO 5 500 EMB175 ICAO_B 3 7 Climb MaxClimb ZERO 7 500 EMB175 ICAO_B 3 8 Climb MaxClimb ZERO 10 000 EMB190 DEFAULT 1 1 Takeoff MaxTakeoff 1 EMB190 DEFAULT 1 2 Climb MaxTakeoff 1 1 000 EMB190 DEFAULT 1 3 Accelerate MaxClimb ZERO 1 685 194,5 EMB190 DEFAULT 1 4 Climb MaxClimb ZERO 3 000 EMB190 DEFAULT 1 5 Accelerate MaxClimb ZERO 2 041 250 EMB190 DEFAULT 1 6 Climb MaxClimb ZERO 5 500 EMB190 DEFAULT 1 7 Climb MaxClimb ZERO 7 500 EMB190 DEFAULT 1 8 Climb MaxClimb ZERO 10 000 EMB190 DEFAULT 2 1 Takeoff MaxTakeoff 1 EMB190 DEFAULT 2 2 Climb MaxTakeoff 1 1 000 EMB190 DEFAULT 2 3 Accelerate MaxClimb ZERO 1 616 197,1 EMB190 DEFAULT 2 4 Climb MaxClimb ZERO 3 000 EMB190 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 944 250 EMB190 DEFAULT 2 6 Climb MaxClimb ZERO 5 500L 168/622 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB190 DEFAULT 2 7 Climb MaxClimb ZERO 7 500 EMB190 DEFAULT 2 8 Climb MaxClimb ZERO 10 000 EMB190 DEFAULT 3 1 Takeoff MaxTakeoff 1 EMB190 DEFAULT 3 2 Climb MaxTakeoff 1 1 000 EMB190 DEFAULT 3 3 Accelerate MaxClimb ZERO 1 546 199,7 EMB190 DEFAULT 3 4 Climb MaxClimb ZERO 3 000 EMB190 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 850 250 EMB190 DEFAULT 3 6 Climb MaxClimb ZERO 5 500 EMB190 DEFAULT 3 7 Climb MaxClimb ZERO 7 500 EMB190 DEFAULT 3 8 Climb MaxClimb ZERO 10 000 EMB190 DEFAULT 4 1 Takeoff MaxTakeoff 1 EMB190 DEFAULT 4 2 Climb MaxTakeoff 1 1 000 EMB190 DEFAULT 4 3 Accelerate MaxClimb ZERO 1 416 205,2 EMB190 DEFAULT 4 4 Climb MaxClimb ZERO 3 000 EMB190 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 677 250 EMB190 DEFAULT 4 6 Climb MaxClimb ZERO 5 500 EMB190 DEFAULT 4 7 Climb MaxClimb ZERO 7 500 EMB190 DEFAULT 4 8 Climb MaxClimb ZERO 10 000 EMB190 ICAO_A 1 1 Takeoff MaxTakeoff 1 EMB190 ICAO_A 1 2 Climb MaxTakeoff 1 1 5001.7.2015 EN Official Journal of the European Union L 168/623 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB190 ICAO_A 1 3 Climb MaxClimb 1 3 000 EMB190 ICAO_A 1 4 Accelerate MaxClimb ZERO 1 652 194,1 EMB190 ICAO_A 1 5 Accelerate MaxClimb ZERO 2 012 250 EMB190 ICAO_A 1 6 Climb MaxClimb ZERO 5 500 EMB190 ICAO_A 1 7 Climb MaxClimb ZERO 7 500 EMB190 ICAO_A 1 8 Climb MaxClimb ZERO 10 000 EMB190 ICAO_A 2 1 Takeoff MaxTakeoff 1 EMB190 ICAO_A 2 2 Climb MaxTakeoff 1 1 500 EMB190 ICAO_A 2 3 Climb MaxClimb 1 3 000 EMB190 ICAO_A 2 4 Accelerate MaxClimb ZERO 1 582 196,6 EMB190 ICAO_A 2 5 Accelerate MaxClimb ZERO 1 918 250 EMB190 ICAO_A 2 6 Climb MaxClimb ZERO 5 500 EMB190 ICAO_A 2 7 Climb MaxClimb ZERO 7 500 EMB190 ICAO_A 2 8 Climb MaxClimb ZERO 10 000 EMB190 ICAO_A 3 1 Takeoff MaxTakeoff 1 EMB190 ICAO_A 3 2 Climb MaxTakeoff 1 1 500 EMB190 ICAO_A 3 3 Climb MaxClimb 1 3 000 EMB190 ICAO_A 3 4 Accelerate MaxClimb ZERO 1 513 199,4 EMB190 ICAO_A 3 5 Accelerate MaxClimb ZERO 1 826 250 EMB190 ICAO_A 3 6 Climb MaxClimb ZERO 5 500L 168/624 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB190 ICAO_A 3 7 Climb MaxClimb ZERO 7 500 EMB190 ICAO_A 3 8 Climb MaxClimb ZERO 10 000 EMB190 ICAO_A 4 1 Takeoff MaxTakeoff 1 EMB190 ICAO_A 4 2 Climb MaxTakeoff 1 1 500 EMB190 ICAO_A 4 3 Climb MaxClimb 1 3 000 EMB190 ICAO_A 4 4 Accelerate MaxClimb ZERO 1 382 204,8 EMB190 ICAO_A 4 5 Accelerate MaxClimb ZERO 1 658 250 EMB190 ICAO_A 4 6 Climb MaxClimb ZERO 7 500 EMB190 ICAO_A 4 7 Climb MaxClimb ZERO 10 000 EMB190 ICAO_B 1 1 Takeoff MaxTakeoff 1 EMB190 ICAO_B 1 2 Climb MaxTakeoff 1 1 000 EMB190 ICAO_B 1 3 Accelerate MaxTakeoff ZERO 1 899 194,4 EMB190 ICAO_B 1 4 Climb MaxClimb ZERO 3 000 EMB190 ICAO_B 1 5 Accelerate MaxClimb ZERO 2 171 250 EMB190 ICAO_B 1 6 Climb MaxClimb ZERO 5 500 EMB190 ICAO_B 1 7 Climb MaxClimb ZERO 7 500 EMB190 ICAO_B 1 8 Climb MaxClimb ZERO 10 000 EMB190 ICAO_B 2 1 Takeoff MaxTakeoff 1 EMB190 ICAO_B 2 2 Climb MaxTakeoff 1 1 000 EMB190 ICAO_B 2 3 Accelerate MaxTakeoff ZERO 1 824 1971.7.2015 EN Official Journal of the European Union L 168/625 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB190 ICAO_B 2 4 Climb MaxClimb ZERO 3 000 EMB190 ICAO_B 2 5 Accelerate MaxClimb ZERO 2 069 250 EMB190 ICAO_B 2 6 Climb MaxClimb ZERO 5 500 EMB190 ICAO_B 2 7 Climb MaxClimb ZERO 7 500 EMB190 ICAO_B 2 8 Climb MaxClimb ZERO 10 000 EMB190 ICAO_B 3 1 Takeoff MaxTakeoff 1 EMB190 ICAO_B 3 2 Climb MaxTakeoff 1 1 000 EMB190 ICAO_B 3 3 Accelerate MaxTakeoff ZERO 1 628 199,7 EMB190 ICAO_B 3 4 Climb MaxClimb ZERO 3 000 EMB190 ICAO_B 3 5 Accelerate MaxClimb ZERO 1 969 250 EMB190 ICAO_B 3 6 Climb MaxClimb ZERO 5 500 EMB190 ICAO_B 3 7 Climb MaxClimb ZERO 7 500 EMB190 ICAO_B 3 8 Climb MaxClimb ZERO 10 000 EMB190 ICAO_B 4 1 Takeoff MaxTakeoff 1 EMB190 ICAO_B 4 2 Climb MaxTakeoff 1 1 000 EMB190 ICAO_B 4 3 Accelerate MaxTakeoff ZERO 1 603 205,1 EMB190 ICAO_B 4 4 Climb MaxClimb ZERO 3 000 EMB190 ICAO_B 4 5 Accelerate MaxClimb ZERO 1 784 250 EMB190 ICAO_B 4 6 Climb MaxClimb ZERO 5 500 EMB190 ICAO_B 4 7 Climb MaxClimb ZERO 7 500L 168/626 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB190 ICAO_B 4 8 Climb MaxClimb ZERO 10 000 EMB195 DEFAULT 1 1 Takeoff MaxTakeoff 1 EMB195 DEFAULT 1 2 Climb MaxTakeoff 1 1 000 EMB195 DEFAULT 1 3 Accelerate MaxClimb ZERO 1 622 195 EMB195 DEFAULT 1 4 Climb MaxClimb ZERO 3 000 EMB195 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 965 250 EMB195 DEFAULT 1 6 Climb MaxClimb ZERO 5 500 EMB195 DEFAULT 1 7 Climb MaxClimb ZERO 7 500 EMB195 DEFAULT 1 8 Climb MaxClimb ZERO 10 000 EMB195 DEFAULT 2 1 Takeoff MaxTakeoff 1 EMB195 DEFAULT 2 2 Climb MaxTakeoff 1 1 000 EMB195 DEFAULT 2 3 Accelerate MaxClimb ZERO 1 556 197,6 EMB195 DEFAULT 2 4 Climb MaxClimb ZERO 3 000 EMB195 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 872 250 EMB195 DEFAULT 2 6 Climb MaxClimb ZERO 5 500 EMB195 DEFAULT 2 7 Climb MaxClimb ZERO 7 500 EMB195 DEFAULT 2 8 Climb MaxClimb ZERO 10 000 EMB195 DEFAULT 3 1 Takeoff MaxTakeoff 1 EMB195 DEFAULT 3 2 Climb MaxTakeoff 1 1 000 EMB195 DEFAULT 3 3 Accelerate MaxClimb ZERO 1 489 200,21.7.2015 EN Official Journal of the European Union L 168/627 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB195 DEFAULT 3 4 Climb MaxClimb ZERO 3 000 EMB195 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 781 250 EMB195 DEFAULT 3 6 Climb MaxClimb ZERO 5 500 EMB195 DEFAULT 3 7 Climb MaxClimb ZERO 7 500 EMB195 DEFAULT 3 8 Climb MaxClimb ZERO 10 000 EMB195 DEFAULT 4 1 Takeoff MaxTakeoff 1 EMB195 DEFAULT 4 2 Climb MaxTakeoff 1 1 000 EMB195 DEFAULT 4 3 Accelerate MaxClimb ZERO 1 364 205,7 EMB195 DEFAULT 4 4 Climb MaxClimb ZERO 3 000 EMB195 DEFAULT 4 5 Accelerate MaxClimb ZERO 1 615 250 EMB195 DEFAULT 4 6 Climb MaxClimb ZERO 7 500 EMB195 DEFAULT 4 7 Climb MaxClimb ZERO 10 000 EMB195 ICAO_A 1 1 Takeoff MaxTakeoff 1 EMB195 ICAO_A 1 2 Climb MaxTakeoff 1 1 500 EMB195 ICAO_A 1 3 Climb MaxClimb 1 3 000 EMB195 ICAO_A 1 4 Accelerate MaxClimb ZERO 1 605 196,5 EMB195 ICAO_A 1 5 Accelerate MaxClimb ZERO 1 930 250 EMB195 ICAO_A 1 6 Climb MaxClimb ZERO 7 500 EMB195 ICAO_A 1 7 Climb MaxClimb ZERO 10 000 EMB195 ICAO_A 2 1 Takeoff MaxTakeoff 1L 168/628 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB195 ICAO_A 2 2 Climb MaxTakeoff 1 1 500 EMB195 ICAO_A 2 3 Climb MaxClimb 1 3 000 EMB195 ICAO_A 2 4 Accelerate MaxClimb ZERO 1 538 198,1 EMB195 ICAO_A 2 5 Accelerate MaxClimb ZERO 1 871 250 EMB195 ICAO_A 2 6 Climb MaxClimb ZERO 7 500 EMB195 ICAO_A 2 7 Climb MaxClimb ZERO 10 000 EMB195 ICAO_A 3 1 Takeoff MaxTakeoff 1 EMB195 ICAO_A 3 2 Climb MaxTakeoff 1 1 500 EMB195 ICAO_A 3 3 Climb MaxClimb 1 3 000 EMB195 ICAO_A 3 4 Accelerate MaxClimb ZERO 1 467 201,3 EMB195 ICAO_A 3 5 Accelerate MaxClimb ZERO 1 768 250 EMB195 ICAO_A 3 6 Climb MaxClimb ZERO 7 500 EMB195 ICAO_A 3 7 Climb MaxClimb ZERO 10 000 EMB195 ICAO_A 4 1 Takeoff MaxTakeoff 1 EMB195 ICAO_A 4 2 Climb MaxTakeoff 1 1 500 EMB195 ICAO_A 4 3 Climb MaxClimb 1 3 000 EMB195 ICAO_A 4 4 Accelerate MaxClimb ZERO 1 336 206,2 EMB195 ICAO_A 4 5 Accelerate MaxClimb ZERO 1 607 250 EMB195 ICAO_A 4 6 Climb MaxClimb ZERO 7 500 EMB195 ICAO_A 4 7 Climb MaxClimb ZERO 10 0001.7.2015 EN Official Journal of the European Union L 168/629 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB195 ICAO_B 1 1 Takeoff MaxTakeoff 1 EMB195 ICAO_B 1 2 Climb MaxTakeoff 1 1 000 EMB195 ICAO_B 1 3 Accelerate MaxTakeoff ZERO 1 732 194,8 EMB195 ICAO_B 1 4 Climb MaxClimb ZERO 3 000 EMB195 ICAO_B 1 5 Accelerate MaxClimb ZERO 1 988 250 EMB195 ICAO_B 1 6 Climb MaxClimb ZERO 5 500 EMB195 ICAO_B 1 7 Climb MaxClimb ZERO 7 500 EMB195 ICAO_B 1 8 Climb MaxClimb ZERO 10 000 EMB195 ICAO_B 2 1 Takeoff MaxTakeoff 1 EMB195 ICAO_B 2 2 Climb MaxTakeoff 1 1 000 EMB195 ICAO_B 2 3 Accelerate MaxTakeoff ZERO 1 664 197 EMB195 ICAO_B 2 4 Climb MaxClimb ZERO 3 000 EMB195 ICAO_B 2 5 Accelerate MaxClimb ZERO 1 895 250 EMB195 ICAO_B 2 6 Climb MaxClimb ZERO 5 500 EMB195 ICAO_B 2 7 Climb MaxClimb ZERO 7 500 EMB195 ICAO_B 2 8 Climb MaxClimb ZERO 10 000 EMB195 ICAO_B 3 1 Takeoff MaxTakeoff 1 EMB195 ICAO_B 3 2 Climb MaxTakeoff 1 1 000 EMB195 ICAO_B 3 3 Accelerate MaxTakeoff ZERO 1 485 195 EMB195 ICAO_B 3 4 Climb MaxClimb ZERO 3 000L 168/630 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) EMB195 ICAO_B 3 5 Accelerate MaxClimb ZERO 1 800 250 EMB195 ICAO_B 3 6 Climb MaxClimb ZERO 5 500 EMB195 ICAO_B 3 7 Climb MaxClimb ZERO 7 500 EMB195 ICAO_B 3 8 Climb MaxClimb ZERO 10 000 EMB195 ICAO_B 4 1 Takeoff MaxTakeoff 1 EMB195 ICAO_B 4 2 Climb MaxTakeoff 1 1 000 EMB195 ICAO_B 4 3 Accelerate MaxTakeoff ZERO 1 468 205,4 EMB195 ICAO_B 4 4 Climb MaxClimb ZERO 3 000 EMB195 ICAO_B 4 5 Accelerate MaxClimb ZERO 1 631 250 EMB195 ICAO_B 4 6 Climb MaxClimb ZERO 5 500 EMB195 ICAO_B 4 7 Climb MaxClimb ZERO 7 500 EMB195 ICAO_B 4 8 Climb MaxClimb ZERO 10 000 F10062 DEFAULT 1 1 Takeoff MaxTakeoff TO F10062 DEFAULT 1 2 Climb MaxTakeoff TO 1 000 F10062 DEFAULT 1 3 Accelerate MaxTakeoff TO 2 196 154 F10062 DEFAULT 1 4 Accelerate MaxTakeoff TO 1 647 169 F10062 DEFAULT 1 5 Accelerate MaxClimb TO 1 000 184 F10062 DEFAULT 1 6 Climb MaxClimb TO 3 000 F10062 DEFAULT 1 7 Accelerate MaxClimb TO 1 000 250 F10062 DEFAULT 1 8 Climb MaxClimb TO 5 5001.7.2015 EN Official Journal of the European Union L 168/631 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) F10062 DEFAULT 1 9 Climb MaxClimb TO 7 500 F10062 DEFAULT 1 10 Climb MaxClimb TO 10 000 F10062 DEFAULT 2 1 Takeoff MaxTakeoff TO F10062 DEFAULT 2 2 Climb MaxTakeoff TO 1 000 F10062 DEFAULT 2 3 Accelerate MaxTakeoff TO 1 982 161 F10062 DEFAULT 2 4 Accelerate MaxTakeoff TO 1 487 176 F10062 DEFAULT 2 5 Accelerate MaxClimb TO 1 000 191 F10062 DEFAULT 2 6 Climb MaxClimb TO 3 000 F10062 DEFAULT 2 7 Accelerate MaxClimb TO 1 000 250 F10062 DEFAULT 2 8 Climb MaxClimb TO 5 500 F10062 DEFAULT 2 9 Climb MaxClimb TO 7 500 F10062 DEFAULT 2 10 Climb MaxClimb TO 10 000 F10062 DEFAULT 3 1 Takeoff MaxTakeoff TO F10062 DEFAULT 3 2 Climb MaxTakeoff TO 1 000 F10062 DEFAULT 3 3 Accelerate MaxTakeoff TO 1 819 167 F10062 DEFAULT 3 4 Accelerate MaxTakeoff TO 1 364 182 F10062 DEFAULT 3 5 Accelerate MaxClimb TO 1 000 197 F10062 DEFAULT 3 6 Climb MaxClimb TO 3 000 F10062 DEFAULT 3 7 Accelerate MaxClimb TO 1 000 250 F10062 DEFAULT 3 8 Climb MaxClimb TO 5 500L 168/632 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) F10062 DEFAULT 3 9 Climb MaxClimb TO 7 500 F10062 DEFAULT 3 10 Climb MaxClimb TO 10 000 F10065 DEFAULT 1 1 Takeoff MaxTakeoff TO F10065 DEFAULT 1 2 Climb MaxTakeoff TO 1 000 F10065 DEFAULT 1 3 Accelerate MaxTakeoff TO 2 446 157 F10065 DEFAULT 1 4 Accelerate MaxTakeoff TO 1 835 172 F10065 DEFAULT 1 5 Accelerate MaxClimb TO 1 000 187 F10065 DEFAULT 1 6 Climb MaxClimb TO 3 000 F10065 DEFAULT 1 7 Accelerate MaxClimb TO 1 000 250 F10065 DEFAULT 1 8 Climb MaxClimb TO 5 500 F10065 DEFAULT 1 9 Climb MaxClimb TO 7 500 F10065 DEFAULT 1 10 Climb MaxClimb TO 10 000 F10065 DEFAULT 2 1 Takeoff MaxTakeoff TO F10065 DEFAULT 2 2 Climb MaxTakeoff TO 1 000 F10065 DEFAULT 2 3 Accelerate MaxTakeoff TO 2 218 165 F10065 DEFAULT 2 4 Accelerate MaxTakeoff TO 1 664 180 F10065 DEFAULT 2 5 Accelerate MaxClimb TO 1 000 195 F10065 DEFAULT 2 6 Climb MaxClimb TO 3 000 F10065 DEFAULT 2 7 Accelerate MaxClimb TO 1 000 250 F10065 DEFAULT 2 8 Climb MaxClimb TO 5 500 F10065 DEFAULT 2 9 Climb MaxClimb TO 7 5001.7.2015 EN Official Journal of the European Union L 168/633 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) F10065 DEFAULT 2 10 Climb MaxClimb TO 10 000 F10065 DEFAULT 3 1 Takeoff MaxTakeoff TO F10065 DEFAULT 3 2 Climb MaxTakeoff TO 1 000 F10065 DEFAULT 3 3 Accelerate MaxTakeoff TO 2 021 171 F10065 DEFAULT 3 4 Accelerate MaxTakeoff TO 1 516 186 F10065 DEFAULT 3 5 Accelerate MaxClimb TO 1 000 201 F10065 DEFAULT 3 6 Climb MaxClimb TO 3 000 F10065 DEFAULT 3 7 Accelerate MaxClimb TO 1 000 250 F10065 DEFAULT 3 8 Climb MaxClimb TO 5 500 F10065 DEFAULT 3 9 Climb MaxClimb TO 7 500 F10065 DEFAULT 3 10 Climb MaxClimb TO 10 000 F28MK2 DEFAULT 1 1 Takeoff MaxTakeoff 6 F28MK2 DEFAULT 1 2 Climb MaxTakeoff 6 1 000 F28MK2 DEFAULT 1 3 Accelerate MaxTakeoff 6 2 229 155 F28MK2 DEFAULT 1 4 Accelerate MaxTakeoff ZERO 1 672 170 F28MK2 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 185 F28MK2 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 F28MK2 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 F28MK2 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 F28MK2 DEFAULT 1 9 Climb MaxClimb ZERO 7 500L 168/634 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) F28MK2 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 F28MK2 DEFAULT 2 1 Takeoff MaxTakeoff 6 F28MK2 DEFAULT 2 2 Climb MaxTakeoff 6 1 000 F28MK2 DEFAULT 2 3 Accelerate MaxTakeoff 6 2 011 162 F28MK2 DEFAULT 2 4 Accelerate MaxTakeoff ZERO 1 508 177 F28MK2 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 192 F28MK2 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 F28MK2 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 F28MK2 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 F28MK2 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 F28MK2 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 F28MK4 DEFAULT 1 1 Takeoff MaxTakeoff 6 F28MK4 DEFAULT 1 2 Climb MaxTakeoff 6 1 000 F28MK4 DEFAULT 1 3 Accelerate MaxTakeoff 6 2 103 152 F28MK4 DEFAULT 1 4 Accelerate MaxTakeoff ZERO 1 578 167 F28MK4 DEFAULT 1 5 Accelerate MaxClimb ZERO 1 000 182 F28MK4 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 F28MK4 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 F28MK4 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 F28MK4 DEFAULT 1 9 Climb MaxClimb ZERO 7 5001.7.2015 EN Official Journal of the European Union L 168/635 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) F28MK4 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 F28MK4 DEFAULT 2 1 Takeoff MaxTakeoff 6 F28MK4 DEFAULT 2 2 Climb MaxTakeoff 6 1 000 F28MK4 DEFAULT 2 3 Accelerate MaxTakeoff 6 1 941 157 F28MK4 DEFAULT 2 4 Accelerate MaxTakeoff ZERO 1 456 172 F28MK4 DEFAULT 2 5 Accelerate MaxClimb ZERO 1 000 187 F28MK4 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 F28MK4 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 F28MK4 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 F28MK4 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 F28MK4 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 F28MK4 DEFAULT 3 1 Takeoff MaxTakeoff 6 F28MK4 DEFAULT 3 2 Climb MaxTakeoff 6 1 000 F28MK4 DEFAULT 3 3 Accelerate MaxTakeoff 6 1 743 165 F28MK4 DEFAULT 3 4 Accelerate MaxTakeoff 6 1 307 180 F28MK4 DEFAULT 3 5 Accelerate MaxClimb ZERO 1 000 195 F28MK4 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 F28MK4 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 F28MK4 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 F28MK4 DEFAULT 3 9 Climb MaxClimb ZERO 7 500L 168/636 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) F28MK4 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 FAL20 DEFAULT 1 1 Takeoff MaxTakeoff 10 FAL20 DEFAULT 1 2 Accelerate MaxTakeoff 10 1 388 152 FAL20 DEFAULT 1 3 Climb MaxTakeoff 10 1 500 FAL20 DEFAULT 1 4 Accelerate MaxTakeoff 10 1 388 162 FAL20 DEFAULT 1 5 Accelerate MaxClimb INTR 1 041 177 FAL20 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 FAL20 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 432 250 FAL20 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 FAL20 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 FAL20 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 GII DEFAULT 1 1 Takeoff ReduceTake­ T-20-D off GII DEFAULT 1 2 Climb ReduceTake­ T-20-D 35 off GII DEFAULT 1 3 Accelerate ReduceTake­ T-20-D 1 500 162 off GII DEFAULT 1 4 Climb ReduceTake­ T-20-D 400 off GII DEFAULT 1 5 Climb Reduce­ T-10-U 520 Climb GII DEFAULT 1 6 Climb Reduce­ T-10-U 1 500 Climb GII DEFAULT 1 7 Climb Reduce­ T-10-U 3 000 Climb GII DEFAULT 1 8 Accelerate MaxClimb T-0-U 1 675 192 GII DEFAULT 1 9 Accelerate MaxClimb T-0-U 1 775 2501.7.2015 EN Official Journal of the European Union L 168/637 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) GII DEFAULT 1 10 Climb MaxClimb T-0-U 5 500 GII DEFAULT 1 11 Climb MaxClimb T-0-U 7 500 GII DEFAULT 1 12 Climb MaxClimb T-0-U 10 000 GII QF_FULL 1 1 Takeoff MaxTakeoff T-20-D GII QF_FULL 1 2 Climb MaxTakeoff T-20-D 35 GII QF_FULL 1 3 Accelerate MaxTakeoff T-20-D 1 500 162 GII QF_FULL 1 4 Climb MaxTakeoff T-20-D 400 GII QF_FULL 1 5 Climb Reduce­ T-10-U 520 Climb GII QF_FULL 1 6 Climb Reduce­ T-10-U 1 500 Climb GII QF_FULL 1 7 Climb Reduce­ T-10-U 3 000 Climb GII QF_FULL 1 8 Accelerate MaxClimb T-0-U 1 675 192 GII QF_FULL 1 9 Accelerate MaxClimb T-0-U 1 775 250 GII QF_FULL 1 10 Climb MaxClimb T-0-U 5 500 GII QF_FULL 1 11 Climb MaxClimb T-0-U 7 500 GII QF_FULL 1 12 Climb MaxClimb T-0-U 10 000 GIIB DEFAULT 1 1 Takeoff ReduceTake­ T-20-D off GIIB DEFAULT 1 2 Climb ReduceTake­ T-20-D 35 off GIIB DEFAULT 1 3 Accelerate ReduceTake­ T-20-D 1 500 156 off GIIB DEFAULT 1 4 Climb ReduceTake­ T-20-D 400 off GIIB DEFAULT 1 5 Climb Reduce­ T-10-U 520 ClimbL 168/638 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) GIIB DEFAULT 1 6 Climb Reduce­ T-10-U 1 500 Climb GIIB DEFAULT 1 7 Climb Reduce­ T-10-U 3 000 Climb GIIB DEFAULT 1 8 Accelerate MaxClimb T-0-U 1 675 192 GIIB DEFAULT 1 9 Accelerate MaxClimb T-0-U 1 775 250 GIIB DEFAULT 1 10 Climb MaxClimb T-0-U 5 500 GIIB DEFAULT 1 11 Climb MaxClimb T-0-U 7 500 GIIB DEFAULT 1 12 Climb MaxClimb T-0-U 10 000 GIIB QF_FULL 1 1 Takeoff MaxTakeoff T-20-D GIIB QF_FULL 1 2 Climb MaxTakeoff T-20-D 35 GIIB QF_FULL 1 3 Accelerate MaxTakeoff T-20-D 1 500 156 GIIB QF_FULL 1 4 Climb MaxTakeoff T-20-D 400 GIIB QF_FULL 1 5 Climb Reduce­ T-10-U 520 Climb GIIB QF_FULL 1 6 Climb Reduce­ T-10-U 1 500 Climb GIIB QF_FULL 1 7 Climb Reduce­ T-10-U 3 000 Climb GIIB QF_FULL 1 8 Accelerate MaxClimb T-0-U 1 675 192 GIIB QF_FULL 1 9 Accelerate MaxClimb T-0-U 1 775 250 GIIB QF_FULL 1 10 Climb MaxClimb T-0-U 5 500 GIIB QF_FULL 1 11 Climb MaxClimb T-0-U 7 500 GIIB QF_FULL 1 12 Climb MaxClimb T-0-U 10 000 GIV DEFAULT 1 1 Takeoff MaxTakeoff T-20-D1.7.2015 EN Official Journal of the European Union L 168/639 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) GIV DEFAULT 1 2 Climb MaxTakeoff T-20-D 35 GIV DEFAULT 1 3 Accelerate MaxTakeoff T-20-D 1 800 159,2 GIV DEFAULT 1 4 Climb MaxTakeoff T-20-U 400 GIV DEFAULT 1 5 Climb MaxClimb T-20-U 600 GIV DEFAULT 1 6 Climb MaxClimb T-20-U 750 GIV DEFAULT 1 7 Climb MaxClimb T-10-U 1 850 GIV DEFAULT 1 8 Climb MaxClimb T-10-U 3 000 GIV DEFAULT 1 9 Accelerate MaxClimb T-0-U 1 750 250 GIV DEFAULT 1 10 Climb MaxClimb T-0-U 5 000 GIV DEFAULT 1 11 Climb MaxClimb T-0-U 6 000 GIV DEFAULT 1 12 Climb MaxClimb T-0-U 7 000 GIV DEFAULT 1 13 Climb MaxClimb T-0-U 8 000 GIV DEFAULT 1 14 Climb MaxClimb T-0-U 9 000 GIV DEFAULT 1 15 Climb MaxClimb T-0-U 10 000 GV DEFAULT 1 1 Takeoff MaxTakeoff T-20-D GV DEFAULT 1 2 Climb MaxTakeoff T-20-D 35 GV DEFAULT 1 3 Accelerate MaxTakeoff T-20-D 1 500 165,7 GV DEFAULT 1 4 Climb MaxTakeoff T-20-U 400 GV DEFAULT 1 5 Climb MaxClimb T-20-U 600 GV DEFAULT 1 6 Climb MaxClimb T-20-U 750L 168/640 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) GV DEFAULT 1 7 Climb MaxClimb T-10-U 1 800 GV DEFAULT 1 8 Climb MaxClimb T-10-U 3 000 GV DEFAULT 1 9 Accelerate MaxClimb T-0-U 1 750 250 GV DEFAULT 1 10 Climb MaxClimb T-0-U 5 000 GV DEFAULT 1 11 Climb MaxClimb T-0-U 6 000 GV DEFAULT 1 12 Climb MaxClimb T-0-U 7 000 GV DEFAULT 1 13 Climb MaxClimb T-0-U 8 000 GV DEFAULT 1 14 Climb MaxClimb T-0-U 9 000 GV DEFAULT 1 15 Climb MaxClimb T-0-U 10 000 HS748A DEFAULT 1 1 Takeoff MaxTakeoff TO HS748A DEFAULT 1 2 Climb MaxTakeoff TO 1 000 HS748A DEFAULT 1 3 Accelerate MaxTakeoff TO 917 127 HS748A DEFAULT 1 4 Accelerate MaxClimb INTR 688 147 HS748A DEFAULT 1 5 Climb MaxClimb ZERO 3 000 HS748A DEFAULT 1 6 Climb MaxClimb ZERO 5 500 HS748A DEFAULT 1 7 Climb MaxClimb ZERO 7 500 HS748A DEFAULT 1 8 Climb MaxClimb ZERO 10 000 IA1125 DEFAULT 1 1 Takeoff MaxTakeoff 12 IA1125 DEFAULT 1 2 Accelerate MaxTakeoff 12 1 094 163 IA1125 DEFAULT 1 3 Climb MaxTakeoff 12 1 5001.7.2015 EN Official Journal of the European Union L 168/641 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) IA1125 DEFAULT 1 4 Accelerate MaxTakeoff INTR 1 094 188 IA1125 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 IA1125 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 286 250 IA1125 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 IA1125 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 IA1125 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 L1011 DEFAULT 1 1 Takeoff MaxTakeoff 10 L1011 DEFAULT 1 2 Climb MaxTakeoff 10 1 000 L1011 DEFAULT 1 3 Accelerate MaxTakeoff 10 2 145 162 L1011 DEFAULT 1 4 Accelerate MaxTakeoff INTR 1 609 182 L1011 DEFAULT 1 5 Accelerate MaxClimb INTR 1 000 202 L1011 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 L1011 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 L1011 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 L1011 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 L1011 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 L1011 DEFAULT 2 1 Takeoff MaxTakeoff 10 L1011 DEFAULT 2 2 Climb MaxTakeoff 10 1 000 L1011 DEFAULT 2 3 Accelerate MaxTakeoff 10 2 068 165 L1011 DEFAULT 2 4 Accelerate MaxTakeoff INTR 1 551 185L 168/642 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) L1011 DEFAULT 2 5 Accelerate MaxClimb INTR 1 000 205 L1011 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 L1011 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 L1011 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 L1011 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 L1011 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 L1011 DEFAULT 3 1 Takeoff MaxTakeoff 10 L1011 DEFAULT 3 2 Climb MaxTakeoff 10 1 000 L1011 DEFAULT 3 3 Accelerate MaxTakeoff 10 1 959 168 L1011 DEFAULT 3 4 Accelerate MaxTakeoff INTR 1 469 188 L1011 DEFAULT 3 5 Accelerate MaxClimb INTR 1 000 208 L1011 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 L1011 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 L1011 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 L1011 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 L1011 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 L1011 DEFAULT 4 1 Takeoff MaxTakeoff 10 L1011 DEFAULT 4 2 Climb MaxTakeoff 10 1 000 L1011 DEFAULT 4 3 Accelerate MaxTakeoff 10 1 857 171 L1011 DEFAULT 4 4 Accelerate MaxTakeoff INTR 1 393 1911.7.2015 EN Official Journal of the European Union L 168/643 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) L1011 DEFAULT 4 5 Accelerate MaxClimb INTR 1 000 211 L1011 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 L1011 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 L1011 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 L1011 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 L1011 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 L1011 DEFAULT 5 1 Takeoff MaxTakeoff 10 L1011 DEFAULT 5 2 Climb MaxTakeoff 10 1 000 L1011 DEFAULT 5 3 Accelerate MaxTakeoff 10 1 669 178 L1011 DEFAULT 5 4 Accelerate MaxTakeoff INTR 1 252 198 L1011 DEFAULT 5 5 Accelerate MaxClimb INTR 1 000 218 L1011 DEFAULT 5 6 Climb MaxClimb ZERO 3 000 L1011 DEFAULT 5 7 Accelerate MaxClimb ZERO 1 000 250 L1011 DEFAULT 5 8 Climb MaxClimb ZERO 5 500 L1011 DEFAULT 5 9 Climb MaxClimb ZERO 7 500 L1011 DEFAULT 5 10 Climb MaxClimb ZERO 10 000 L1011 DEFAULT 6 1 Takeoff MaxTakeoff 10 L1011 DEFAULT 6 2 Climb MaxTakeoff 10 1 000 L1011 DEFAULT 6 3 Accelerate MaxTakeoff 10 1 501 184 L1011 DEFAULT 6 4 Accelerate MaxTakeoff INTR 1 126 204L 168/644 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) L1011 DEFAULT 6 5 Accelerate MaxClimb INTR 1 000 224 L1011 DEFAULT 6 6 Climb MaxClimb ZERO 3 000 L1011 DEFAULT 6 7 Accelerate MaxClimb ZERO 1 000 250 L1011 DEFAULT 6 8 Climb MaxClimb ZERO 5 500 L1011 DEFAULT 6 9 Climb MaxClimb ZERO 7 500 L1011 DEFAULT 6 10 Climb MaxClimb ZERO 10 000 L10115 DEFAULT 1 1 Takeoff MaxTakeoff 10 L10115 DEFAULT 1 2 Climb MaxTakeoff 10 1 000 L10115 DEFAULT 1 3 Accelerate MaxTakeoff 10 2 632 166 L10115 DEFAULT 1 4 Accelerate MaxTakeoff INTR 1 974 186 L10115 DEFAULT 1 5 Accelerate MaxClimb INTR 1 000 206 L10115 DEFAULT 1 6 Climb MaxClimb ZERO 3 000 L10115 DEFAULT 1 7 Accelerate MaxClimb ZERO 1 000 250 L10115 DEFAULT 1 8 Climb MaxClimb ZERO 5 500 L10115 DEFAULT 1 9 Climb MaxClimb ZERO 7 500 L10115 DEFAULT 1 10 Climb MaxClimb ZERO 10 000 L10115 DEFAULT 2 1 Takeoff MaxTakeoff 10 L10115 DEFAULT 2 2 Climb MaxTakeoff 10 1 000 L10115 DEFAULT 2 3 Accelerate MaxTakeoff 10 2 547 168 L10115 DEFAULT 2 4 Accelerate MaxTakeoff INTR 1 911 1881.7.2015 EN Official Journal of the European Union L 168/645 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) L10115 DEFAULT 2 5 Accelerate MaxClimb INTR 1 000 208 L10115 DEFAULT 2 6 Climb MaxClimb ZERO 3 000 L10115 DEFAULT 2 7 Accelerate MaxClimb ZERO 1 000 250 L10115 DEFAULT 2 8 Climb MaxClimb ZERO 5 500 L10115 DEFAULT 2 9 Climb MaxClimb ZERO 7 500 L10115 DEFAULT 2 10 Climb MaxClimb ZERO 10 000 L10115 DEFAULT 3 1 Takeoff MaxTakeoff 10 L10115 DEFAULT 3 2 Climb MaxTakeoff 10 1 000 L10115 DEFAULT 3 3 Accelerate MaxTakeoff 10 2 428 171 L10115 DEFAULT 3 4 Accelerate MaxTakeoff INTR 1 821 191 L10115 DEFAULT 3 5 Accelerate MaxClimb INTR 1 000 211 L10115 DEFAULT 3 6 Climb MaxClimb ZERO 3 000 L10115 DEFAULT 3 7 Accelerate MaxClimb ZERO 1 000 250 L10115 DEFAULT 3 8 Climb MaxClimb ZERO 5 500 L10115 DEFAULT 3 9 Climb MaxClimb ZERO 7 500 L10115 DEFAULT 3 10 Climb MaxClimb ZERO 10 000 L10115 DEFAULT 4 1 Takeoff MaxTakeoff 10 L10115 DEFAULT 4 2 Climb MaxTakeoff 10 1 000 L10115 DEFAULT 4 3 Accelerate MaxTakeoff 10 2 317 175 L10115 DEFAULT 4 4 Accelerate MaxTakeoff INTR 1 738 195L 168/646 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) L10115 DEFAULT 4 5 Accelerate MaxClimb INTR 1 000 215 L10115 DEFAULT 4 6 Climb MaxClimb ZERO 3 000 L10115 DEFAULT 4 7 Accelerate MaxClimb ZERO 1 000 250 L10115 DEFAULT 4 8 Climb MaxClimb ZERO 5 500 L10115 DEFAULT 4 9 Climb MaxClimb ZERO 7 500 L10115 DEFAULT 4 10 Climb MaxClimb ZERO 10 000 L10115 DEFAULT 5 1 Takeoff MaxTakeoff 10 L10115 DEFAULT 5 2 Climb MaxTakeoff 10 1 000 L10115 DEFAULT 5 3 Accelerate MaxTakeoff 10 2 125 181 L10115 DEFAULT 5 4 Accelerate MaxTakeoff INTR 1 594 201 L10115 DEFAULT 5 5 Accelerate MaxClimb INTR 1 000 221 L10115 DEFAULT 5 6 Climb MaxClimb ZERO 3 000 L10115 DEFAULT 5 7 Accelerate MaxClimb ZERO 1 000 250 L10115 DEFAULT 5 8 Climb MaxClimb ZERO 5 500 L10115 DEFAULT 5 9 Climb MaxClimb ZERO 7 500 L10115 DEFAULT 5 10 Climb MaxClimb ZERO 10 000 L10115 DEFAULT 6 1 Takeoff MaxTakeoff 10 L10115 DEFAULT 6 2 Climb MaxTakeoff 10 1 000 L10115 DEFAULT 6 3 Accelerate MaxTakeoff 10 1 953 186 L10115 DEFAULT 6 4 Accelerate MaxTakeoff INTR 1 465 2061.7.2015 EN Official Journal of the European Union L 168/647 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) L10115 DEFAULT 6 5 Accelerate MaxClimb INTR 1 000 226 L10115 DEFAULT 6 6 Climb MaxClimb ZERO 3 000 L10115 DEFAULT 6 7 Accelerate MaxClimb ZERO 1 000 250 L10115 DEFAULT 6 8 Climb MaxClimb ZERO 5 500 L10115 DEFAULT 6 9 Climb MaxClimb ZERO 7 500 L10115 DEFAULT 6 10 Climb MaxClimb ZERO 10 000 L10115 DEFAULT 7 1 Takeoff MaxTakeoff 10 L10115 DEFAULT 7 2 Climb MaxTakeoff 10 1 000 L10115 DEFAULT 7 3 Accelerate MaxTakeoff 10 1 790 192 L10115 DEFAULT 7 4 Accelerate MaxTakeoff INTR 1 343 212 L10115 DEFAULT 7 5 Accelerate MaxClimb INTR 1 000 232 L10115 DEFAULT 7 6 Climb MaxClimb ZERO 3 000 L10115 DEFAULT 7 7 Accelerate MaxClimb ZERO 1 000 250 L10115 DEFAULT 7 8 Climb MaxClimb ZERO 5 500 L10115 DEFAULT 7 9 Climb MaxClimb ZERO 7 500 L10115 DEFAULT 7 10 Climb MaxClimb ZERO 10 000 L188 DEFAULT 1 1 Takeoff MaxTakeoff 78-% L188 DEFAULT 1 2 Climb MaxTakeoff 78-% 1 000 L188 DEFAULT 1 3 Accelerate MaxTakeoff 78-% 1 653 133 L188 DEFAULT 1 4 Accelerate MaxClimb INTR 1 240 153L 168/648 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) L188 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 L188 DEFAULT 1 6 Climb MaxClimb ZERO 5 500 L188 DEFAULT 1 7 Climb MaxClimb ZERO 7 500 L188 DEFAULT 1 8 Climb MaxClimb ZERO 10 000 L188 DEFAULT 2 1 Takeoff MaxTakeoff 78-% L188 DEFAULT 2 2 Climb MaxTakeoff 78-% 1 000 L188 DEFAULT 2 3 Accelerate MaxTakeoff 78-% 1 309 139 L188 DEFAULT 2 4 Accelerate MaxClimb INTR 982 159 L188 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 L188 DEFAULT 2 6 Climb MaxClimb ZERO 5 500 L188 DEFAULT 2 7 Climb MaxClimb ZERO 7 500 L188 DEFAULT 2 8 Climb MaxClimb ZERO 10 000 L188 DEFAULT 3 1 Takeoff MaxTakeoff 78-% L188 DEFAULT 3 2 Climb MaxTakeoff 78-% 1 000 L188 DEFAULT 3 3 Accelerate MaxTakeoff 78-% 905 147 L188 DEFAULT 3 4 Accelerate MaxClimb INTR 679 167 L188 DEFAULT 3 5 Climb MaxClimb ZERO 3 000 L188 DEFAULT 3 6 Climb MaxClimb ZERO 5 500 L188 DEFAULT 3 7 Climb MaxClimb ZERO 7 500 L188 DEFAULT 3 8 Climb MaxClimb ZERO 10 0001.7.2015 EN Official Journal of the European Union L 168/649 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) LEAR25 DEFAULT 1 1 Takeoff MaxTakeoff 20 LEAR25 DEFAULT 1 2 Accelerate MaxTakeoff 20 1 698 171 LEAR25 DEFAULT 1 3 Climb MaxTakeoff 20 1 500 LEAR25 DEFAULT 1 4 Accelerate MaxTakeoff 10 1 698 196 LEAR25 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 LEAR25 DEFAULT 1 6 Accelerate MaxClimb ZERO 2 075 250 LEAR25 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 LEAR25 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 LEAR25 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 LEAR35 DEFAULT 1 1 Takeoff MaxTakeoff 20 LEAR35 DEFAULT 1 2 Accelerate MaxTakeoff 20 1 493 158 LEAR35 DEFAULT 1 3 Climb MaxTakeoff 20 1 500 LEAR35 DEFAULT 1 4 Accelerate MaxTakeoff 10 1 493 183 LEAR35 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 LEAR35 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 706 250 LEAR35 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 LEAR35 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 LEAR35 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 MD11GE DEFAULT 1 1 Takeoff MaxTakeoff 25 MD11GE DEFAULT 1 2 Climb MaxTakeoff 25 1 000L 168/650 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD11GE DEFAULT 1 3 Accelerate MaxTakeoff 0/EXT 1 500 211 MD11GE DEFAULT 1 4 Climb MaxClimb 0/EXT 2 000 MD11GE DEFAULT 1 5 Climb MaxClimb 0/EXT 3 000 MD11GE DEFAULT 1 6 Accelerate MaxClimb 0/RET 1 500 250 MD11GE DEFAULT 1 7 Climb MaxClimb 0/RET 10 000 MD11GE DEFAULT 2 1 Takeoff MaxTakeoff 25 MD11GE DEFAULT 2 2 Climb MaxTakeoff 25 1 000 MD11GE DEFAULT 2 3 Accelerate MaxTakeoff 0/EXT 1 500 210 MD11GE DEFAULT 2 4 Climb MaxClimb 0/EXT 2 000 MD11GE DEFAULT 2 5 Climb MaxClimb 0/EXT 3 000 MD11GE DEFAULT 2 6 Accelerate MaxClimb 0/RET 1 500 250 MD11GE DEFAULT 2 7 Climb MaxClimb 0/RET 10 000 MD11GE DEFAULT 3 1 Takeoff MaxTakeoff 25 MD11GE DEFAULT 3 2 Climb MaxTakeoff 25 1 000 MD11GE DEFAULT 3 3 Accelerate MaxTakeoff 0/EXT 1 500 210 MD11GE DEFAULT 3 4 Climb MaxClimb 0/EXT 2 000 MD11GE DEFAULT 3 5 Climb MaxClimb 0/EXT 3 000 MD11GE DEFAULT 3 6 Accelerate MaxClimb 0/RET 1 500 250 MD11GE DEFAULT 3 7 Climb MaxClimb 0/RET 10 000 MD11GE DEFAULT 4 1 Takeoff MaxTakeoff 251.7.2015 EN Official Journal of the European Union L 168/651 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD11GE DEFAULT 4 2 Climb MaxTakeoff 25 1 000 MD11GE DEFAULT 4 3 Accelerate MaxTakeoff 0/EXT 1 500 209 MD11GE DEFAULT 4 4 Climb MaxClimb 0/EXT 2 000 MD11GE DEFAULT 4 5 Climb MaxClimb 0/EXT 3 000 MD11GE DEFAULT 4 6 Accelerate MaxClimb 0/RET 1 500 250 MD11GE DEFAULT 4 7 Climb MaxClimb 0/RET 10 000 MD11GE DEFAULT 5 1 Takeoff MaxTakeoff 25 MD11GE DEFAULT 5 2 Climb MaxTakeoff 25 1 000 MD11GE DEFAULT 5 3 Accelerate MaxTakeoff 0/EXT 1 500 208 MD11GE DEFAULT 5 4 Climb MaxClimb 0/EXT 2 000 MD11GE DEFAULT 5 5 Climb MaxClimb 0/EXT 3 000 MD11GE DEFAULT 5 6 Accelerate MaxClimb 0/RET 1 500 250 MD11GE DEFAULT 5 7 Climb MaxClimb 0/RET 10 000 MD11GE DEFAULT 6 1 Takeoff MaxTakeoff 25 MD11GE DEFAULT 6 2 Climb MaxTakeoff 25 1 000 MD11GE DEFAULT 6 3 Accelerate MaxTakeoff 0/EXT 1 500 208 MD11GE DEFAULT 6 4 Climb MaxClimb 0/EXT 2 000 MD11GE DEFAULT 6 5 Climb MaxClimb 0/EXT 3 000 MD11GE DEFAULT 6 6 Accelerate MaxClimb 0/RET 1 500 250 MD11GE DEFAULT 6 7 Climb MaxClimb 0/RET 10 000L 168/652 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD11GE DEFAULT 7 1 Takeoff MaxTakeoff 25 MD11GE DEFAULT 7 2 Climb MaxTakeoff 25 1 000 MD11GE DEFAULT 7 3 Accelerate MaxTakeoff 0/EXT 1 500 207 MD11GE DEFAULT 7 4 Climb MaxClimb 0/EXT 2 000 MD11GE DEFAULT 7 5 Climb MaxClimb 0/EXT 3 000 MD11GE DEFAULT 7 6 Accelerate MaxClimb 0/RET 1 500 250 MD11GE DEFAULT 7 7 Climb MaxClimb 0/RET 10 000 MD11PW DEFAULT 1 1 Takeoff MaxTakeoff 25 MD11PW DEFAULT 1 2 Climb MaxTakeoff 25 1 000 MD11PW DEFAULT 1 3 Accelerate MaxTakeoff 0/EXT 1 500 206 MD11PW DEFAULT 1 4 Climb MaxClimb 0/EXT 2 000 MD11PW DEFAULT 1 5 Climb MaxClimb 0/EXT 3 000 MD11PW DEFAULT 1 6 Accelerate MaxClimb 0/RET 1 500 250 MD11PW DEFAULT 1 7 Climb MaxClimb 0/RET 10 000 MD11PW DEFAULT 2 1 Takeoff MaxTakeoff 25 MD11PW DEFAULT 2 2 Climb MaxTakeoff 25 1 000 MD11PW DEFAULT 2 3 Accelerate MaxTakeoff 0/EXT 1 500 206 MD11PW DEFAULT 2 4 Climb MaxClimb 0/EXT 2 000 MD11PW DEFAULT 2 5 Climb MaxClimb 0/EXT 3 000 MD11PW DEFAULT 2 6 Accelerate MaxClimb 0/RET 1 500 2501.7.2015 EN Official Journal of the European Union L 168/653 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD11PW DEFAULT 2 7 Climb MaxClimb 0/RET 10 000 MD11PW DEFAULT 3 1 Takeoff MaxTakeoff 25 MD11PW DEFAULT 3 2 Climb MaxTakeoff 25 1 000 MD11PW DEFAULT 3 3 Accelerate MaxTakeoff 0/EXT 1 500 205 MD11PW DEFAULT 3 4 Climb MaxClimb 0/EXT 2 000 MD11PW DEFAULT 3 5 Climb MaxClimb 0/EXT 3 000 MD11PW DEFAULT 3 6 Accelerate MaxClimb 0/RET 1 500 250 MD11PW DEFAULT 3 7 Climb MaxClimb 0/RET 10 000 MD11PW DEFAULT 4 1 Takeoff MaxTakeoff 25 MD11PW DEFAULT 4 2 Climb MaxTakeoff 25 1 000 MD11PW DEFAULT 4 3 Accelerate MaxTakeoff 0/EXT 1 500 205 MD11PW DEFAULT 4 4 Climb MaxClimb 0/EXT 2 000 MD11PW DEFAULT 4 5 Climb MaxClimb 0/EXT 3 000 MD11PW DEFAULT 4 6 Accelerate MaxClimb 0/RET 1 500 250 MD11PW DEFAULT 4 7 Climb MaxClimb 0/RET 10 000 MD11PW DEFAULT 5 1 Takeoff MaxTakeoff 25 MD11PW DEFAULT 5 2 Climb MaxTakeoff 25 1 000 MD11PW DEFAULT 5 3 Accelerate MaxTakeoff 0/EXT 1 500 205 MD11PW DEFAULT 5 4 Climb MaxClimb 0/EXT 2 000 MD11PW DEFAULT 5 5 Climb MaxClimb 0/EXT 3 000L 168/654 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD11PW DEFAULT 5 6 Accelerate MaxClimb 0/RET 1 500 250 MD11PW DEFAULT 5 7 Climb MaxClimb 0/RET 10 000 MD11PW DEFAULT 6 1 Takeoff MaxTakeoff 25 MD11PW DEFAULT 6 2 Climb MaxTakeoff 25 1 000 MD11PW DEFAULT 6 3 Accelerate MaxTakeoff 0/EXT 1 500 206 MD11PW DEFAULT 6 4 Climb MaxClimb 0/EXT 2 000 MD11PW DEFAULT 6 5 Climb MaxClimb 0/EXT 3 000 MD11PW DEFAULT 6 6 Accelerate MaxClimb 0/RET 1 500 250 MD11PW DEFAULT 6 7 Climb MaxClimb 0/RET 10 000 MD11PW DEFAULT 7 1 Takeoff MaxTakeoff 25 MD11PW DEFAULT 7 2 Climb MaxTakeoff 25 1 000 MD11PW DEFAULT 7 3 Accelerate MaxTakeoff 0/EXT 1 500 207 MD11PW DEFAULT 7 4 Climb MaxClimb 0/EXT 2 000 MD11PW DEFAULT 7 5 Climb MaxClimb 0/EXT 3 000 MD11PW DEFAULT 7 6 Accelerate MaxClimb 0/RET 1 500 250 MD11PW DEFAULT 7 7 Climb MaxClimb 0/RET 10 000 MD81 DEFAULT 1 1 Takeoff MaxTakeoff T_15 MD81 DEFAULT 1 2 Climb MaxTakeoff T_15 1 000 MD81 DEFAULT 1 3 Accelerate MaxClimb T_INT 1 434,2 214,1 MD81 DEFAULT 1 4 Climb MaxClimb T_ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/655 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD81 DEFAULT 1 5 Accelerate MaxClimb T_ZERO 1 866,9 250 MD81 DEFAULT 1 6 Climb MaxClimb T_ZERO 5 500 MD81 DEFAULT 1 7 Climb MaxClimb T_ZERO 7 500 MD81 DEFAULT 1 8 Climb MaxClimb T_ZERO 10 000 MD81 DEFAULT 2 1 Takeoff MaxTakeoff T_15 MD81 DEFAULT 2 2 Climb MaxTakeoff T_15 1 000 MD81 DEFAULT 2 3 Accelerate MaxClimb T_INT 1 346,9 218,7 MD81 DEFAULT 2 4 Climb MaxClimb T_ZERO 3 000 MD81 DEFAULT 2 5 Accelerate MaxClimb T_ZERO 1 745 250 MD81 DEFAULT 2 6 Climb MaxClimb T_ZERO 5 500 MD81 DEFAULT 2 7 Climb MaxClimb T_ZERO 7 500 MD81 DEFAULT 2 8 Climb MaxClimb T_ZERO 10 000 MD81 DEFAULT 3 1 Takeoff MaxTakeoff T_15 MD81 DEFAULT 3 2 Climb MaxTakeoff T_15 1 000 MD81 DEFAULT 3 3 Accelerate MaxClimb T_INT 1 266 223,2 MD81 DEFAULT 3 4 Climb MaxClimb T_ZERO 3 000 MD81 DEFAULT 3 5 Accelerate MaxClimb T_ZERO 1 643,2 250 MD81 DEFAULT 3 6 Climb MaxClimb T_ZERO 5 500 MD81 DEFAULT 3 7 Climb MaxClimb T_ZERO 7 500 MD81 DEFAULT 3 8 Climb MaxClimb T_ZERO 10 000L 168/656 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD81 DEFAULT 4 1 Takeoff MaxTakeoff T_15 MD81 DEFAULT 4 2 Climb MaxTakeoff T_15 1 000 MD81 DEFAULT 4 3 Accelerate MaxClimb T_INT 1 211,7 226,3 MD81 DEFAULT 4 4 Climb MaxClimb T_ZERO 3 000 MD81 DEFAULT 4 5 Accelerate MaxClimb T_ZERO 1 577,9 250 MD81 DEFAULT 4 6 Climb MaxClimb T_ZERO 5 500 MD81 DEFAULT 4 7 Climb MaxClimb T_ZERO 7 500 MD81 DEFAULT 4 8 Climb MaxClimb T_ZERO 10 000 MD81 ICAO_A 1 1 Takeoff MaxTakeoff T_15 MD81 ICAO_A 1 2 Climb MaxTakeoff T_15 1 500 MD81 ICAO_A 1 3 Climb MaxClimb T_15 3 000 MD81 ICAO_A 1 4 Accelerate MaxClimb T_ZERO 1 169,8 250 MD81 ICAO_A 1 5 Climb MaxClimb T_ZERO 5 500 MD81 ICAO_A 1 6 Climb MaxClimb T_ZERO 7 500 MD81 ICAO_A 1 7 Climb MaxClimb T_ZERO 10 000 MD81 ICAO_A 2 1 Takeoff MaxTakeoff T_15 MD81 ICAO_A 2 2 Climb MaxTakeoff T_15 1 500 MD81 ICAO_A 2 3 Climb MaxClimb T_15 3 000 MD81 ICAO_A 2 4 Accelerate MaxClimb T_ZERO 1 089,3 250 MD81 ICAO_A 2 5 Climb MaxClimb T_ZERO 5 5001.7.2015 EN Official Journal of the European Union L 168/657 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD81 ICAO_A 2 6 Climb MaxClimb T_ZERO 7 500 MD81 ICAO_A 2 7 Climb MaxClimb T_ZERO 10 000 MD81 ICAO_A 3 1 Takeoff MaxTakeoff T_15 MD81 ICAO_A 3 2 Climb MaxTakeoff T_15 1 500 MD81 ICAO_A 3 3 Climb MaxClimb T_15 3 000 MD81 ICAO_A 3 4 Accelerate MaxClimb T_ZERO 1 049,8 250 MD81 ICAO_A 3 5 Climb MaxClimb T_ZERO 5 500 MD81 ICAO_A 3 6 Climb MaxClimb T_ZERO 7 500 MD81 ICAO_A 3 7 Climb MaxClimb T_ZERO 10 000 MD81 ICAO_A 4 1 Takeoff MaxTakeoff T_15 MD81 ICAO_A 4 2 Climb MaxTakeoff T_15 1 500 MD81 ICAO_A 4 3 Climb MaxClimb T_15 3 000 MD81 ICAO_A 4 4 Accelerate MaxClimb T_ZERO 998,8 250 MD81 ICAO_A 4 5 Climb MaxClimb T_ZERO 5 500 MD81 ICAO_A 4 6 Climb MaxClimb T_ZERO 7 500 MD81 ICAO_A 4 7 Climb MaxClimb T_ZERO 10 000 MD81 ICAO_B 1 1 Takeoff MaxTakeoff T_15 MD81 ICAO_B 1 2 Climb MaxTakeoff T_15 1 000 MD81 ICAO_B 1 3 Accelerate MaxTakeoff T_INT 1 434,8 218,8 MD81 ICAO_B 1 4 Climb MaxClimb T_ZERO 3 000L 168/658 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD81 ICAO_B 1 5 Accelerate MaxClimb T_ZERO 1 900,5 250 MD81 ICAO_B 1 6 Climb MaxClimb T_ZERO 5 500 MD81 ICAO_B 1 7 Climb MaxClimb T_ZERO 7 500 MD81 ICAO_B 1 8 Climb MaxClimb T_ZERO 10 000 MD81 ICAO_B 2 1 Takeoff MaxTakeoff T_15 MD81 ICAO_B 2 2 Climb MaxTakeoff T_15 1 000 MD81 ICAO_B 2 3 Accelerate MaxTakeoff T_INT 1 345,2 223 MD81 ICAO_B 2 4 Climb MaxClimb T_ZERO 3 000 MD81 ICAO_B 2 5 Accelerate MaxClimb T_ZERO 1 779,8 250 MD81 ICAO_B 2 6 Climb MaxClimb T_ZERO 5 500 MD81 ICAO_B 2 7 Climb MaxClimb T_ZERO 7 500 MD81 ICAO_B 2 8 Climb MaxClimb T_ZERO 10 000 MD81 ICAO_B 3 1 Takeoff MaxTakeoff T_15 MD81 ICAO_B 3 2 Climb MaxTakeoff T_15 1 000 MD81 ICAO_B 3 3 Accelerate MaxTakeoff T_INT 1 264,5 227,4 MD81 ICAO_B 3 4 Climb MaxClimb T_ZERO 3 000 MD81 ICAO_B 3 5 Accelerate MaxClimb T_ZERO 1 664,2 250 MD81 ICAO_B 3 6 Climb MaxClimb T_ZERO 5 500 MD81 ICAO_B 3 7 Climb MaxClimb T_ZERO 7 500 MD81 ICAO_B 3 8 Climb MaxClimb T_ZERO 10 0001.7.2015 EN Official Journal of the European Union L 168/659 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD81 ICAO_B 4 1 Takeoff MaxTakeoff T_15 MD81 ICAO_B 4 2 Climb MaxTakeoff T_15 1 000 MD81 ICAO_B 4 3 Accelerate MaxTakeoff T_INT 1 211,1 230,2 MD81 ICAO_B 4 4 Climb MaxClimb T_ZERO 3 000 MD81 ICAO_B 4 5 Accelerate MaxClimb T_ZERO 1 594,3 250 MD81 ICAO_B 4 6 Climb MaxClimb T_ZERO 5 500 MD81 ICAO_B 4 7 Climb MaxClimb T_ZERO 7 500 MD81 ICAO_B 4 8 Climb MaxClimb T_ZERO 10 000 MD82 DEFAULT 1 1 Takeoff MaxTakeoff T_15 MD82 DEFAULT 1 2 Climb MaxTakeoff T_15 1 000 MD82 DEFAULT 1 3 Accelerate MaxClimb INT4 1 247,7 216,4 MD82 DEFAULT 1 4 Climb MaxClimb INT3 3 000 MD82 DEFAULT 1 5 Accelerate MaxClimb T_ZERO 1 933 250 MD82 DEFAULT 1 6 Climb MaxClimb T_ZERO 5 500 MD82 DEFAULT 1 7 Climb MaxClimb T_ZERO 7 500 MD82 DEFAULT 1 8 Climb MaxClimb T_ZERO 10 000 MD82 DEFAULT 2 1 Takeoff MaxTakeoff T_15 MD82 DEFAULT 2 2 Climb MaxTakeoff T_15 1 000 MD82 DEFAULT 2 3 Accelerate MaxClimb INT4 1 169,5 220,7 MD82 DEFAULT 2 4 Climb MaxClimb INT3 3 000L 168/660 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD82 DEFAULT 2 5 Accelerate MaxClimb T_ZERO 1 805,5 250 MD82 DEFAULT 2 6 Climb MaxClimb T_ZERO 5 500 MD82 DEFAULT 2 7 Climb MaxClimb T_ZERO 7 500 MD82 DEFAULT 2 8 Climb MaxClimb T_ZERO 10 000 MD82 DEFAULT 3 1 Takeoff MaxTakeoff T_15 MD82 DEFAULT 3 2 Climb MaxTakeoff T_15 1 000 MD82 DEFAULT 3 3 Accelerate MaxClimb INT4 1 099,1 225,1 MD82 DEFAULT 3 4 Climb MaxClimb INT3 3 000 MD82 DEFAULT 3 5 Accelerate MaxClimb T_ZERO 1 710,9 250 MD82 DEFAULT 3 6 Climb MaxClimb T_ZERO 5 500 MD82 DEFAULT 3 7 Climb MaxClimb T_ZERO 7 500 MD82 DEFAULT 3 8 Climb MaxClimb T_ZERO 10 000 MD82 DEFAULT 4 1 Takeoff MaxTakeoff T_15 MD82 DEFAULT 4 2 Climb MaxTakeoff T_15 1 000 MD82 DEFAULT 4 3 Accelerate MaxClimb INT4 989,5 231,9 MD82 DEFAULT 4 4 Climb MaxClimb INT3 3 000 MD82 DEFAULT 4 5 Accelerate MaxClimb T_ZERO 1 563,6 250 MD82 DEFAULT 4 6 Climb MaxClimb T_ZERO 5 500 MD82 DEFAULT 4 7 Climb MaxClimb T_ZERO 7 500 MD82 DEFAULT 4 8 Climb MaxClimb T_ZERO 10 0001.7.2015 EN Official Journal of the European Union L 168/661 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD82 DEFAULT 5 1 Takeoff MaxTakeoff T_15 MD82 DEFAULT 5 2 Climb MaxTakeoff T_15 1 000 MD82 DEFAULT 5 3 Accelerate MaxClimb INT4 950,4 234,2 MD82 DEFAULT 5 4 Climb MaxClimb INT3 3 000 MD82 DEFAULT 5 5 Accelerate MaxClimb T_ZERO 1 518,1 250 MD82 DEFAULT 5 6 Climb MaxClimb T_ZERO 5 500 MD82 DEFAULT 5 7 Climb MaxClimb T_ZERO 7 500 MD82 DEFAULT 5 8 Climb MaxClimb T_ZERO 10 000 MD82 ICAO_A 1 1 Takeoff MaxTakeoff T_15 MD82 ICAO_A 1 2 Climb MaxTakeoff T_15 1 500 MD82 ICAO_A 1 3 Climb MaxClimb T_INT 3 000 MD82 ICAO_A 1 4 Accelerate MaxClimb T_ZERO 1 200 250 MD82 ICAO_A 1 5 Climb MaxClimb T_ZERO 5 500 MD82 ICAO_A 1 6 Climb MaxClimb T_ZERO 7 500 MD82 ICAO_A 1 7 Climb MaxClimb T_ZERO 10 000 MD82 ICAO_A 2 1 Takeoff MaxTakeoff T_15 MD82 ICAO_A 2 2 Climb MaxTakeoff T_15 1 500 MD82 ICAO_A 2 3 Climb MaxClimb T_15 3 000 MD82 ICAO_A 2 4 Accelerate MaxClimb T_ZERO 1 120,6 250 MD82 ICAO_A 2 5 Climb MaxClimb T_ZERO 5 500L 168/662 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD82 ICAO_A 2 6 Climb MaxClimb T_ZERO 7 500 MD82 ICAO_A 2 7 Climb MaxClimb T_ZERO 10 000 MD82 ICAO_A 3 1 Takeoff MaxTakeoff T_15 MD82 ICAO_A 3 2 Climb MaxTakeoff T_15 1 500 MD82 ICAO_A 3 3 Climb MaxClimb T_15 3 000 MD82 ICAO_A 3 4 Accelerate MaxClimb T_ZERO 1 051,4 250 MD82 ICAO_A 3 5 Climb MaxClimb T_ZERO 5 500 MD82 ICAO_A 3 6 Climb MaxClimb T_ZERO 7 500 MD82 ICAO_A 3 7 Climb MaxClimb T_ZERO 10 000 MD82 ICAO_A 4 1 Takeoff MaxTakeoff T_15 MD82 ICAO_A 4 2 Climb MaxTakeoff T_15 1 500 MD82 ICAO_A 4 3 Climb MaxClimb T_15 3 000 MD82 ICAO_A 4 4 Accelerate MaxClimb T_ZERO 939,4 250 MD82 ICAO_A 4 5 Climb MaxClimb T_ZERO 5 500 MD82 ICAO_A 4 6 Climb MaxClimb T_ZERO 7 500 MD82 ICAO_A 4 7 Climb MaxClimb T_ZERO 10 000 MD82 ICAO_A 5 1 Takeoff MaxTakeoff T_15 MD82 ICAO_A 5 2 Climb MaxTakeoff T_15 1 500 MD82 ICAO_A 5 3 Climb MaxClimb T_15 3 000 MD82 ICAO_A 5 4 Accelerate MaxClimb T_ZERO 900 2501.7.2015 EN Official Journal of the European Union L 168/663 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD82 ICAO_A 5 5 Climb MaxClimb T_ZERO 5 500 MD82 ICAO_A 5 6 Climb MaxClimb T_ZERO 7 500 MD82 ICAO_A 5 7 Climb MaxClimb T_ZERO 10 000 MD82 ICAO_B 1 1 Takeoff MaxTakeoff T_15 MD82 ICAO_B 1 2 Climb MaxTakeoff T_15 1 000 MD82 ICAO_B 1 3 Accelerate MaxTakeoff T_INT 1 447,7 218,7 MD82 ICAO_B 1 4 Climb MaxClimb T_ZERO 3 000 MD82 ICAO_B 1 5 Accelerate MaxClimb T_ZERO 1 952,8 250 MD82 ICAO_B 1 6 Climb MaxClimb T_ZERO 5 500 MD82 ICAO_B 1 7 Climb MaxClimb T_ZERO 7 500 MD82 ICAO_B 1 8 Climb MaxClimb T_ZERO 10 000 MD82 ICAO_B 2 1 Takeoff MaxTakeoff T_15 MD82 ICAO_B 2 2 Climb MaxTakeoff T_15 1 000 MD82 ICAO_B 2 3 Accelerate MaxTakeoff T_INT 1 360,4 222,9 MD82 ICAO_B 2 4 Climb MaxClimb T_ZERO 3 000 MD82 ICAO_B 2 5 Accelerate MaxClimb T_ZERO 1 838,2 250 MD82 ICAO_B 2 6 Climb MaxClimb T_ZERO 5 500 MD82 ICAO_B 2 7 Climb MaxClimb T_ZERO 7 500 MD82 ICAO_B 2 8 Climb MaxClimb T_ZERO 10 000 MD82 ICAO_B 3 1 Takeoff MaxTakeoff T_15L 168/664 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD82 ICAO_B 3 2 Climb MaxTakeoff T_15 1 000 MD82 ICAO_B 3 3 Accelerate MaxTakeoff T_INT 1 279,8 227,2 MD82 ICAO_B 3 4 Climb MaxClimb T_ZERO 3 000 MD82 ICAO_B 3 5 Accelerate MaxClimb T_ZERO 1 732,3 250 MD82 ICAO_B 3 6 Climb MaxClimb T_ZERO 5 500 MD82 ICAO_B 3 7 Climb MaxClimb T_ZERO 7 500 MD82 ICAO_B 3 8 Climb MaxClimb T_ZERO 10 000 MD82 ICAO_B 4 1 Takeoff MaxTakeoff T_15 MD82 ICAO_B 4 2 Climb MaxTakeoff T_15 1 000 MD82 ICAO_B 4 3 Accelerate MaxTakeoff T_INT 1 160,8 233,9 MD82 ICAO_B 4 4 Climb MaxClimb T_ZERO 3 000 MD82 ICAO_B 4 5 Accelerate MaxClimb T_ZERO 1 564,9 250 MD82 ICAO_B 4 6 Climb MaxClimb T_ZERO 5 500 MD82 ICAO_B 4 7 Climb MaxClimb T_ZERO 7 500 MD82 ICAO_B 4 8 Climb MaxClimb T_ZERO 10 000 MD82 ICAO_B 5 1 Takeoff MaxTakeoff T_15 MD82 ICAO_B 5 2 Climb MaxTakeoff T_15 1 000 MD82 ICAO_B 5 3 Accelerate MaxTakeoff T_INT 1 131,1 236,1 MD82 ICAO_B 5 4 Climb MaxClimb T_ZERO 3 000 MD82 ICAO_B 5 5 Accelerate MaxClimb T_ZERO 1 522,4 2501.7.2015 EN Official Journal of the European Union L 168/665 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD82 ICAO_B 5 6 Climb MaxClimb T_ZERO 5 500 MD82 ICAO_B 5 7 Climb MaxClimb T_ZERO 7 500 MD82 ICAO_B 5 8 Climb MaxClimb T_ZERO 10 000 MD83 DEFAULT 1 1 Takeoff MaxTakeoff T_15 MD83 DEFAULT 1 2 Climb MaxTakeoff T_15 1 000 MD83 DEFAULT 1 3 Accelerate MaxClimb T_INT 1 319 218,1 MD83 DEFAULT 1 4 Climb MaxClimb T_ZERO 3 000 MD83 DEFAULT 1 5 Accelerate MaxClimb T_ZERO 2 033,2 250 MD83 DEFAULT 1 6 Climb MaxClimb T_ZERO 5 500 MD83 DEFAULT 1 7 Climb MaxClimb T_ZERO 7 500 MD83 DEFAULT 1 8 Climb MaxClimb T_ZERO 10 000 MD83 DEFAULT 2 1 Takeoff MaxTakeoff T_15 MD83 DEFAULT 2 2 Climb MaxTakeoff T_15 1 000 MD83 DEFAULT 2 3 Accelerate MaxClimb T_INT 1 239,2 222,2 MD83 DEFAULT 2 4 Climb MaxClimb T_ZERO 3 000 MD83 DEFAULT 2 5 Accelerate MaxClimb T_ZERO 1 921,8 250 MD83 DEFAULT 2 6 Climb MaxClimb T_ZERO 5 500 MD83 DEFAULT 2 7 Climb MaxClimb T_ZERO 7 500 MD83 DEFAULT 2 8 Climb MaxClimb T_ZERO 10 000 MD83 DEFAULT 3 1 Takeoff MaxTakeoff T_15L 168/666 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD83 DEFAULT 3 2 Climb MaxTakeoff T_15 1 000 MD83 DEFAULT 3 3 Accelerate MaxClimb T_INT 1 158,7 226,6 MD83 DEFAULT 3 4 Climb MaxClimb T_ZERO 3 000 MD83 DEFAULT 3 5 Accelerate MaxClimb T_ZERO 1 810 250 MD83 DEFAULT 3 6 Climb MaxClimb T_ZERO 5 500 MD83 DEFAULT 3 7 Climb MaxClimb T_ZERO 7 500 MD83 DEFAULT 3 8 Climb MaxClimb T_ZERO 10 000 MD83 DEFAULT 4 1 Takeoff MaxTakeoff T_15 MD83 DEFAULT 4 2 Climb MaxTakeoff T_15 1 000 MD83 DEFAULT 4 3 Accelerate MaxClimb T_INT 1 049,7 233,6 MD83 DEFAULT 4 4 Climb MaxClimb T_ZERO 3 000 MD83 DEFAULT 4 5 Accelerate MaxClimb T_ZERO 1 649 250 MD83 DEFAULT 4 6 Climb MaxClimb T_ZERO 5 500 MD83 DEFAULT 4 7 Climb MaxClimb T_ZERO 7 500 MD83 DEFAULT 4 8 Climb MaxClimb T_ZERO 10 000 MD83 DEFAULT 5 1 Takeoff MaxTakeoff T_15 MD83 DEFAULT 5 2 Climb MaxTakeoff T_15 1 000 MD83 DEFAULT 5 3 Accelerate MaxClimb T_INT 929,7 241,3 MD83 DEFAULT 5 4 Climb MaxClimb T_ZERO 3 000 MD83 DEFAULT 5 5 Accelerate MaxClimb T_ZERO 1 482,4 2501.7.2015 EN Official Journal of the European Union L 168/667 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD83 DEFAULT 5 6 Climb MaxClimb T_ZERO 5 500 MD83 DEFAULT 5 7 Climb MaxClimb T_ZERO 7 500 MD83 DEFAULT 5 8 Climb MaxClimb T_ZERO 10 000 MD83 ICAO_A 1 1 Takeoff MaxTakeoff T_15 MD83 ICAO_A 1 2 Climb MaxTakeoff T_15 1 500 MD83 ICAO_A 1 3 Climb MaxClimb T_15 3 000 MD83 ICAO_A 1 4 Accelerate MaxClimb T_INT 1 269,6 250 MD83 ICAO_A 1 5 Climb MaxClimb T_ZERO 5 500 MD83 ICAO_A 1 6 Climb MaxClimb T_ZERO 7 500 MD83 ICAO_A 1 7 Climb MaxClimb T_ZERO 10 000 MD83 ICAO_A 2 1 Takeoff MaxTakeoff T_15 MD83 ICAO_A 2 2 Climb MaxTakeoff T_15 1 500 MD83 ICAO_A 2 3 Climb MaxClimb T_15 3 000 MD83 ICAO_A 2 4 Accelerate MaxClimb T_INT 1 188,7 250 MD83 ICAO_A 2 5 Climb MaxClimb T_ZERO 5 500 MD83 ICAO_A 2 6 Climb MaxClimb T_ZERO 7 500 MD83 ICAO_A 2 7 Climb MaxClimb T_ZERO 10 000 MD83 ICAO_A 3 1 Takeoff MaxTakeoff T_15 MD83 ICAO_A 3 2 Climb MaxTakeoff T_15 1 500 MD83 ICAO_A 3 3 Climb MaxClimb T_15 3 000L 168/668 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD83 ICAO_A 3 4 Accelerate MaxClimb T_INT 1 109,5 250 MD83 ICAO_A 3 5 Climb MaxClimb T_ZERO 5 500 MD83 ICAO_A 3 6 Climb MaxClimb T_ZERO 7 500 MD83 ICAO_A 3 7 Climb MaxClimb T_ZERO 10 000 MD83 ICAO_A 4 1 Takeoff MaxTakeoff T_15 MD83 ICAO_A 4 2 Climb MaxTakeoff T_15 1 500 MD83 ICAO_A 4 3 Climb MaxClimb T_15 3 000 MD83 ICAO_A 4 4 Accelerate MaxClimb T_INT 989,8 250 MD83 ICAO_A 4 5 Climb MaxClimb T_ZERO 5 500 MD83 ICAO_A 4 6 Climb MaxClimb T_ZERO 7 500 MD83 ICAO_A 4 7 Climb MaxClimb T_ZERO 10 000 MD83 ICAO_A 5 1 Takeoff MaxTakeoff T_15 MD83 ICAO_A 5 2 Climb MaxTakeoff T_15 1 500 MD83 ICAO_A 5 3 Climb MaxClimb T_15 3 000 MD83 ICAO_A 5 4 Accelerate MaxClimb T_INT 880,1 250 MD83 ICAO_A 5 5 Climb MaxClimb T_ZERO 5 500 MD83 ICAO_A 5 6 Climb MaxClimb T_ZERO 7 500 MD83 ICAO_A 5 7 Climb MaxClimb T_ZERO 10 000 MD83 ICAO_B 1 1 Takeoff MaxTakeoff T_15 MD83 ICAO_B 1 2 Climb MaxTakeoff T_15 1 0001.7.2015 EN Official Journal of the European Union L 168/669 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD83 ICAO_B 1 3 Accelerate MaxTakeoff T_INT 1 546,8 221,1 MD83 ICAO_B 1 4 Climb MaxClimb T_ZERO 3 000 MD83 ICAO_B 1 5 Accelerate MaxClimb T_ZERO 2 056,2 250 MD83 ICAO_B 1 6 Climb MaxClimb T_ZERO 5 500 MD83 ICAO_B 1 7 Climb MaxClimb T_ZERO 7 500 MD83 ICAO_B 1 8 Climb MaxClimb T_ZERO 10 000 MD83 ICAO_B 2 1 Takeoff MaxTakeoff T_15 MD83 ICAO_B 2 2 Climb MaxTakeoff T_15 1 000 MD83 ICAO_B 2 3 Accelerate MaxTakeoff T_INT 1 462 225,1 MD83 ICAO_B 2 4 Climb MaxClimb T_ZERO 3 000 MD83 ICAO_B 2 5 Accelerate MaxClimb T_ZERO 1 941,6 250 MD83 ICAO_B 2 6 Climb MaxClimb T_ZERO 5 500 MD83 ICAO_B 2 7 Climb MaxClimb T_ZERO 7 500 MD83 ICAO_B 2 8 Climb MaxClimb T_ZERO 10 000 MD83 ICAO_B 3 1 Takeoff MaxTakeoff T_15 MD83 ICAO_B 3 2 Climb MaxTakeoff T_15 1 000 MD83 ICAO_B 3 3 Accelerate MaxTakeoff T_INT 1 376,3 229,2 MD83 ICAO_B 3 4 Climb MaxClimb T_ZERO 3 000 MD83 ICAO_B 3 5 Accelerate MaxClimb T_ZERO 1 837,5 250 MD83 ICAO_B 3 6 Climb MaxClimb T_ZERO 5 500L 168/670 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD83 ICAO_B 3 7 Climb MaxClimb T_ZERO 7 500 MD83 ICAO_B 3 8 Climb MaxClimb T_ZERO 10 000 MD83 ICAO_B 4 1 Takeoff MaxTakeoff T_15 MD83 ICAO_B 4 2 Climb MaxTakeoff T_15 1 000 MD83 ICAO_B 4 3 Accelerate MaxTakeoff T_INT 1 249,5 236,1 MD83 ICAO_B 4 4 Climb MaxClimb T_ZERO 3 000 MD83 ICAO_B 4 5 Accelerate MaxClimb T_ZERO 1 671,1 250 MD83 ICAO_B 4 6 Climb MaxClimb T_ZERO 5 500 MD83 ICAO_B 4 7 Climb MaxClimb T_ZERO 7 500 MD83 ICAO_B 4 8 Climb MaxClimb T_ZERO 10 000 MD83 ICAO_B 5 1 Takeoff MaxTakeoff T_15 MD83 ICAO_B 5 2 Climb MaxTakeoff T_15 1 000 MD83 ICAO_B 5 3 Accelerate MaxTakeoff T_INT 1 130,3 243,6 MD83 ICAO_B 5 4 Climb MaxClimb T_ZERO 3 000 MD83 ICAO_B 5 5 Accelerate MaxClimb T_ZERO 1 504,9 250 MD83 ICAO_B 5 6 Climb MaxClimb T_ZERO 5 500 MD83 ICAO_B 5 7 Climb MaxClimb T_ZERO 7 500 MD83 ICAO_B 5 8 Climb MaxClimb T_ZERO 10 000 MD9025 DEFAULT 1 1 Takeoff MaxTakeoff EXT/11 MD9025 DEFAULT 1 2 Climb MaxTakeoff EXT/11 1 0001.7.2015 EN Official Journal of the European Union L 168/671 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD9025 DEFAULT 1 3 Accelerate MaxTakeoff RET/0 2 280 194 MD9025 DEFAULT 1 4 Climb MaxClimb RET/0 3 000 MD9025 DEFAULT 1 5 Accelerate MaxClimb RET/0 1 000 250 MD9025 DEFAULT 1 6 Climb MaxClimb RET/0 10 000 MD9025 DEFAULT 2 1 Takeoff MaxTakeoff EXT/11 MD9025 DEFAULT 2 2 Climb MaxTakeoff EXT/11 1 000 MD9025 DEFAULT 2 3 Accelerate MaxTakeoff RET/0 2 150 193 MD9025 DEFAULT 2 4 Climb MaxClimb RET/0 3 000 MD9025 DEFAULT 2 5 Accelerate MaxClimb RET/0 1 000 250 MD9025 DEFAULT 2 6 Climb MaxClimb RET/0 10 000 MD9025 DEFAULT 3 1 Takeoff MaxTakeoff EXT/11 MD9025 DEFAULT 3 2 Climb MaxTakeoff EXT/11 1 000 MD9025 DEFAULT 3 3 Accelerate MaxTakeoff RET/0 2 031 192 MD9025 DEFAULT 3 4 Climb MaxClimb RET/0 3 000 MD9025 DEFAULT 3 5 Accelerate MaxClimb RET/0 1 000 250 MD9025 DEFAULT 3 6 Climb MaxClimb RET/0 10 000 MD9025 DEFAULT 4 1 Takeoff MaxTakeoff EXT/11 MD9025 DEFAULT 4 2 Climb MaxTakeoff EXT/11 1 000 MD9025 DEFAULT 4 3 Accelerate MaxTakeoff RET/0 1 916 191 MD9025 DEFAULT 4 4 Climb MaxClimb RET/0 3 000L 168/672 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD9025 DEFAULT 4 5 Accelerate MaxClimb RET/0 1 000 250 MD9025 DEFAULT 4 6 Climb MaxClimb RET/0 10 000 MD9025 DEFAULT 5 1 Takeoff MaxTakeoff EXT/11 MD9025 DEFAULT 5 2 Climb MaxTakeoff EXT/11 1 000 MD9025 DEFAULT 5 3 Accelerate MaxTakeoff RET/0 1 840 190 MD9025 DEFAULT 5 4 Climb MaxClimb RET/0 3 000 MD9025 DEFAULT 5 5 Accelerate MaxClimb RET/0 1 000 250 MD9025 DEFAULT 5 6 Climb MaxClimb RET/0 10 000 MD9028 DEFAULT 1 1 Takeoff MaxTakeoff EXT/11 MD9028 DEFAULT 1 2 Climb MaxTakeoff EXT/11 1 000 MD9028 DEFAULT 1 3 Accelerate MaxTakeoff RET/0 2 666 196 MD9028 DEFAULT 1 4 Climb MaxClimb RET/0 3 000 MD9028 DEFAULT 1 5 Accelerate MaxClimb RET/0 1 000 250 MD9028 DEFAULT 1 6 Climb MaxClimb RET/0 10 000 MD9028 DEFAULT 2 1 Takeoff MaxTakeoff EXT/11 MD9028 DEFAULT 2 2 Climb MaxTakeoff EXT/11 1 000 MD9028 DEFAULT 2 3 Accelerate MaxTakeoff RET/0 2 525 194 MD9028 DEFAULT 2 4 Climb MaxClimb RET/0 3 000 MD9028 DEFAULT 2 5 Accelerate MaxClimb RET/0 1 000 250 MD9028 DEFAULT 2 6 Climb MaxClimb RET/0 10 0001.7.2015 EN Official Journal of the European Union L 168/673 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MD9028 DEFAULT 3 1 Takeoff MaxTakeoff EXT/11 MD9028 DEFAULT 3 2 Climb MaxTakeoff EXT/11 1 000 MD9028 DEFAULT 3 3 Accelerate MaxTakeoff RET/0 2 391 193 MD9028 DEFAULT 3 4 Climb MaxClimb RET/0 3 000 MD9028 DEFAULT 3 5 Accelerate MaxClimb RET/0 1 000 250 MD9028 DEFAULT 3 6 Climb MaxClimb RET/0 10 000 MD9028 DEFAULT 4 1 Takeoff MaxTakeoff EXT/11 MD9028 DEFAULT 4 2 Climb MaxTakeoff EXT/11 1 000 MD9028 DEFAULT 4 3 Accelerate MaxTakeoff RET/0 2 263 192 MD9028 DEFAULT 4 4 Climb MaxClimb RET/0 3 000 MD9028 DEFAULT 4 5 Accelerate MaxClimb RET/0 1 000 250 MD9028 DEFAULT 4 6 Climb MaxClimb RET/0 10 000 MD9028 DEFAULT 5 1 Takeoff MaxTakeoff EXT/11 MD9028 DEFAULT 5 2 Climb MaxTakeoff EXT/11 1 000 MD9028 DEFAULT 5 3 Accelerate MaxTakeoff RET/0 2 180 189 MD9028 DEFAULT 5 4 Climb MaxClimb RET/0 3 000 MD9028 DEFAULT 5 5 Accelerate MaxClimb RET/0 1 000 250 MD9028 DEFAULT 5 6 Climb MaxClimb RET/0 10 000 MU3001 DEFAULT 1 1 Takeoff MaxTakeoff 10 MU3001 DEFAULT 1 2 Accelerate MaxTakeoff 10 1 130 142L 168/674 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) MU3001 DEFAULT 1 3 Climb MaxTakeoff 1 1 500 MU3001 DEFAULT 1 4 Accelerate MaxTakeoff 1 1 130 200 MU3001 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 MU3001 DEFAULT 1 6 Accelerate MaxClimb ZERO 1 555 250 MU3001 DEFAULT 1 7 Climb MaxClimb ZERO 5 500 MU3001 DEFAULT 1 8 Climb MaxClimb ZERO 7 500 MU3001 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 PA30 DEFAULT 1 1 Takeoff MaxTakeoff 15-D PA30 DEFAULT 1 2 Accelerate MaxTakeoff 15-D 415 79 PA30 DEFAULT 1 3 Accelerate MaxTakeoff 15-D 500 113 PA30 DEFAULT 1 4 Climb MaxTakeoff ZERO-D 1 500 PA30 DEFAULT 1 5 Climb MaxTakeoff ZERO-D 3 000 PA30 DEFAULT 1 6 Climb MaxClimb ZERO-D 5 500 PA30 DEFAULT 1 7 Climb MaxClimb ZERO-D 7 500 PA30 DEFAULT 1 8 Climb MaxClimb ZERO-D 10 000 PA42 DEFAULT 1 1 Takeoff MaxTakeoff ZER-DN PA42 DEFAULT 1 2 Accelerate MaxTakeoff ZER-DN 1 000 118 PA42 DEFAULT 1 3 Climb MaxTakeoff ZER-DN 1 000 PA42 DEFAULT 1 4 Accelerate MaxClimb ZERO 1 000 154 PA42 DEFAULT 1 5 Climb MaxClimb ZERO 3 0001.7.2015 EN Official Journal of the European Union L 168/675 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) PA42 DEFAULT 1 6 Climb MaxClimb ZERO 4 000 PA42 DEFAULT 1 7 Climb MaxClimb ZERO 6 000 PA42 DEFAULT 1 8 Climb MaxClimb ZERO 8 000 PA42 DEFAULT 1 9 Climb MaxClimb ZERO 10 000 SD330 DEFAULT 1 1 Takeoff MaxTakeoff 10 SD330 DEFAULT 1 2 Climb MaxTakeoff 10 1 000 SD330 DEFAULT 1 3 Accelerate MaxTakeoff 10 971 117 SD330 DEFAULT 1 4 Accelerate MaxClimb INTR 728 137 SD330 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 SD330 DEFAULT 1 6 Climb MaxClimb ZERO 5 500 SD330 DEFAULT 1 7 Climb MaxClimb ZERO 7 500 SD330 DEFAULT 1 8 Climb MaxClimb ZERO 10 000 SF340 DEFAULT 1 1 Takeoff MaxTakeoff 15 SF340 DEFAULT 1 2 Climb MaxTakeoff 15 1 000 SF340 DEFAULT 1 3 Accelerate MaxTakeoff 15 1 821 127 SF340 DEFAULT 1 4 Accelerate MaxClimb 5 1 366 147 SF340 DEFAULT 1 5 Climb MaxClimb ZERO 3 000 SF340 DEFAULT 1 6 Climb MaxClimb ZERO 5 500 SF340 DEFAULT 1 7 Climb MaxClimb ZERO 7 500 SF340 DEFAULT 1 8 Climb MaxClimb ZERO 10 000L 168/676 EN Official Journal of the European Union 1.7.2015 Accel­ Rate Of End Stage Step End Point erate_ ACFTID Profile_ID Step Type Thrust Rating Flap_ID Climb Point Length Number Altitude (ft) Percent (ft/min) CAS (kt) (%) SF340 DEFAULT 2 1 Takeoff MaxTakeoff 15 SF340 DEFAULT 2 2 Climb MaxTakeoff 15 1 000 SF340 DEFAULT 2 3 Accelerate MaxTakeoff 15 1 450 133 SF340 DEFAULT 2 4 Accelerate MaxClimb 5 1 088 153 SF340 DEFAULT 2 5 Climb MaxClimb ZERO 3 000 SF340 DEFAULT 2 6 Climb MaxClimb ZERO 5 500 SF340 DEFAULT 2 7 Climb MaxClimb ZERO 7 500 SF340 DEFAULT 2 8 Climb MaxClimb ZERO 10 000Table I-5 Default fixed points profiles Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID 1900D Beech 1900D/PT6A67 Turbo­ 2 Large Commercial 16 950 14 940 1 696 3 367 1 PT6A67 CNT (lb) 213 109 Prop prop 707 Boeing 707-120/JT3C Jet 4 Heavy Commercial 302 400 188 900 6 682 10 120 1 JT4A CNT (lb) 208 107 Wing 707120 Boeing 707-120B/JT3D-3 Jet 4 Heavy Commercial 302 400 188 900 6 893 14 850 1 JT3D CNT (lb) 208 107 Wing 707320 Boeing 707-320B/JT3D-7 Jet 4 Heavy Commercial 334 000 247 000 5 622 19 000 1 JT3D CNT (lb) 208 107 Wing 707QN Boeing 707-320B/JT3D- Jet 4 Heavy Commercial 334 000 247 000 5 622 19 000 2 JT3DQ CNT (lb) 208 106 Wing 7QN 717200 Boeing 717-200/BR 715 Jet 2 Large Commercial 121 000 110 000 4 600 18 000 3 BR715 CNT (lb) 203 105 Fuselage 720 Boeing 720/JT3C Jet 4 Large Commercial 223 500 155 600 4 871 10 120 1 JT4A CNT (lb) 208 107 Wing 720B Boeing 720B/JT3D-3 Jet 4 Large Commercial 234 000 175 000 5 717 18 000 1 JT3D CNT (lb) 208 107 Wing 727100 Boeing 727-100/JT8D-7 Jet 3 Large Commercial 169 500 142 500 4 867 14 000 1 3JT8D CNT (lb) 201 101 Fuselage 727200 Boeing 727-200/JT8D-7 Jet 3 Large Commercial 217 600 163 300 5 571 11 895 1 3JT8D CNT (lb) 201 101 Fuselage 727D15 Boeing 727-200/JT8D-15 Jet 3 Large Commercial 208 000 169 000 4 922 15 500 1 3JT8D CNT (lb) 201 101 Fuselage 727D17 Boeing 727-200/JT8D-17 Jet 3 Large Commercial 208 000 169 000 5 444 16 000 2 3JT8DQ CNT (lb) 201 101 Fuselage 727EM1 FEDX 727-100/JT8D-7 Jet 3 Large Commercial 169 500 142 500 4 867 14 000 3 3JT8E7 CNT (lb) 201 101 Fuselage 1.7.2015 EN Official Journal of the European Union L 168/677Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID 727EM2 FEDX 727-200/JT8D-15 Jet 3 Large Commercial 208 000 169 000 4 922 15 500 3 3JT8E5 CNT (lb) 201 101 Fuselage 727Q15 Boeing 727-200/JT8D- Jet 3 Large Commercial 208 000 169 000 4 922 15 500 2 3JT8DQ CNT (lb) 201 101 Fuselage 15QN 727Q7 Boeing 727-100/JT8D- Jet 3 Large Commercial 169 500 142 500 4 867 14 000 2 3JT8DQ CNT (lb) 201 101 Fuselage 7QN 727Q9 Boeing 727-200/JT8D-9 Jet 3 Large Commercial 191 000 160 000 5 444 14 500 2 3JT8DQ CNT (lb) 201 101 Fuselage 727QF UPS 727-100 22C 25C Jet 3 Large Commercial 169 000 142 500 4 448 15 380 3 TAY651 CNT (lb) 201 101 Fuselage 737 Boeing 737/JT8D-9 Jet 2 Large Commercial 109 000 98 000 3 900 14 500 1 2JT8DW CNT (lb) 201 101 Wing 737300 Boeing 737-300/CFM56- Jet 2 Large Commercial 135 000 114 000 4 580 20 000 3 CFM563 CNT (lb) 202 102 Wing 3B-1 7373B2 Boeing 737-300/CFM56- Jet 2 Large Commercial 139 500 114 000 4 580 22 000 3 CFM563 CNT (lb) 202 102 Wing 3B-2 737400 Boeing 737-400/CFM56- Jet 2 Large Commercial 150 000 124 000 5 062 23 500 3 CFM563 CNT (lb) 202 102 Wing 3C-1 737500 Boeing 737-500/CFM56- Jet 2 Large Commercial 133 500 111 000 4 551 20 000 3 CFM563 CNT (lb) 202 102 Wing 3C-1 737700 Boeing 737-700/CFM56- Jet 2 Large Commercial 154 500 129 200 4 445 24 000 3 CF567B CNT (lb) 203 104 Wing 7B24 737800 Boeing 737-800/CFM56- Jet 2 Large Commercial 174 200 146 300 5 435 26 300 3 CF567B CNT (lb) 203 104 Wing 7B26 737D17 Boeing 737-200/JT8D-17 Jet 2 Large Commercial 124 000 107 000 4 244 16 000 2 2JT8QW CNT (lb) 201 101 Wing L 168/678 EN Official Journal of the European Union 1.7.2015Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID 737N17 Boeing 737-200/JT8D-17 Jet 2 Large Commercial 124 000 107 000 4 244 16 000 3 2JT8DN CNT (lb) 202 104 Wing Nordam B737 LGW Hushkit 737N9 Boeing 737/JT8D-9 Nor­ Jet 2 Large Commercial 109 000 98 000 3 900 14 500 3 2JT8DN CNT (lb) 202 104 Wing dam B737 LGW Hushkit 737QN Boeing 737/JT8D-9QN Jet 2 Large Commercial 109 000 98 000 3 900 14 500 2 2JT8QW CNT (lb) 201 101 Wing 747100 Boeing 747-100/JT9DBD Jet 4 Heavy Commercial 733 000 516 600 5 727 33 042 2 JT9DBD CNT (lb) 209 107 Wing 74710Q Boeing 747-100/JT9D- Jet 4 Heavy Commercial 733 000 564 000 6 200 45 500 3 JT9DFL CNT (lb) 207 107 Wing 7QN 747200 Boeing 747-200/JT9D-7 Jet 4 Heavy Commercial 775 000 564 000 6 200 45 500 3 JT9DFL CNT (lb) 207 107 Wing 74720A Boeing 747-200/JT9D- Jet 4 Heavy Commercial 785 000 564 000 6 200 46 300 3 JT9D7Q CNT (lb) 207 107 Wing 7A 74720B Boeing 747-200/JT9D- Jet 4 Heavy Commercial 800 000 630 000 6 200 53 000 3 JT9D7Q CNT (lb) 207 107 Wing 7Q 747400 Boeing 747-400/ Jet 4 Heavy Commercial 875 000 652 000 6 989 56 800 3 PW4056 CNT (lb) 207 107 Wing PW4056 7478 Boeing 747-8F/GEnx- Jet 4 Heavy Commercial 987 000 757 000 7 900 68 000 4 GENX67 CNT (lb) 205 107 Wing 2B67 747SP Boeing 747SP/JT9D-7 Jet 4 Heavy Commercial 702 000 475 000 5 911 45 500 3 JT9DFL CNT (lb) 207 107 Wing 757300 Boeing 757-300/RB211- Jet 2 Large Commercial 275 000 224 000 5 651 43 100 3 RR535E CNT (lb) 203 103 Wing 535E4B 757PW Boeing 757-200/ Jet 2 Large Commercial 255 000 210 000 4 790 38 300 3 PW2037 CNT (lb) 203 103 Wing PW2037 1.7.2015 EN Official Journal of the European Union L 168/679Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID 757RR Boeing 757-200/RB211- Jet 2 Large Commercial 255 000 210 000 4 640 40 100 3 RR535E CNT (lb) 203 103 Wing 535E4 767300 Boeing 767-300/ Jet 2 Heavy Commercial 407 000 320 000 4 710 60 000 3 2CF680 CNT (lb) 203 103 Wing PW4060 767400 Boeing 767-400ER/CF6- Jet 2 Heavy Commercial 450 000 340 000 6 000 58 685 3 CF680C CNT (lb) 205 102 Wing 80C2B(F) 767CF6 Boeing 767-200/CF6- Jet 2 Heavy Commercial 315 500 270 000 4 700 48 000 3 2CF680 CNT (lb) 203 103 Wing 80A 767JT9 Boeing 767-200/JT9D- Jet 2 Heavy Commercial 351 000 270 000 4 744 48 000 3 2CF680 CNT (lb) 203 103 Wing 7R4D 777200 Boeing 777-200/GE90- Jet 2 Heavy Commercial 656 000 470 000 4 450 90 000 3 GE90 CNT (lb) 205 105 Wing 76B 777300 Boeing 777-300/Trent Jet 2 Heavy Commercial 660 000 524 000 6 012 77 000 0 TRENT8 CNT (lb) 203 105 Wing 892 7773ER Boeing 777-300ER/ Jet 2 Heavy Commercial 775 000 554 000 5 805 115 000 3 GE9015 CNT (lb) 204 107 Wing GE90-115B-EIS 7878R Boeing 787-8/T1000-C/ Jet 2 Heavy Commercial 502 500 380 000 5 090 70 000 4 T1KBFP CNT (lb) 205 103 Wing 01 Family Plan Cert A300- Airbus A300-622R/ Jet 2 Heavy Commercial 378 533 308 647 4 735 58 000 3 PW4158 CNT (lb) 202 103 Wing 622R PW4158 A300B4- Airbus A300B4-200/ Jet 2 Heavy Commercial 364 000 295 000 5 367 52 500 3 2CF650 CNT (lb) 203 103 Wing 203 CF6-50C2 A310-304 Airbus A310-304/GE Jet 2 Heavy Commercial 346 126 273 373 4 682 53 500 3 A310 CNT (lb) 204 103 Wing CF6-80C2A2 A319-131 Airbus A319-131/ Jet 2 Large Commercial 166 449 137 789 4 364 22 000 3 V2522A CNT (lb) 205 103 Wing V2522-A5 L 168/680 EN Official Journal of the European Union 1.7.2015Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID A320-211 Airbus A320-211/ Jet 2 Large Commercial 169 756 142 198 4 753 25 000 3 CFM565 CNT (lb) 202 103 Wing CFM56-5A1 A320-232 Airbus A320-232/ Jet 2 Large Commercial 169 756 145 505 4 917 26 500 3 V2527A CNT (lb) 205 103 Wing V2527-A5 A321-232 Airbus A321-232/IAE Jet 2 Large Commercial 196 211 166 449 5 587 30 000 3 V2530 CNT (lb) 202 103 Wing V2530-A5 A330-301 Airbus A330-301/GE Jet 2 Heavy Commercial 478 400 383 604 5 966 67 500 3 CF680E CNT (lb) 202 102 Wing CF6-80 E1A2 A330-343 Airbus A330-343/RR Jet 2 Heavy Commercial 513 677 412 264 5 512 71 100 3 TRENT7 CNT (lb) 205 102 Wing Trent 772B A340-211 Airbus A340-211/ Jet 4 Heavy Commercial 573 200 399 036 5 900 31 200 3 CF565C CNT (lb) 206 107 Wing CFM56-5C2 A340-642 Airbus A340-642/RR Jet 4 Heavy Commercial 804 687 564 383 6 919 56 000 4 TRENT5 CNT (lb) 205 102 Wing Trent 556 A380-841 Airbus A380-841/RR Jet 4 Heavy Commercial 1 254 430 862 007 6 752 70 000 4 TRENT9 CNT (lb) 205 105 Wing Trent 970 A380-861 Airbus A380-861/EA Jet 4 Heavy Commercial 1 254 430 862 007 6 837 70 000 4 GP7270 CNT (lb) 206 105 Wing GP7270 BAC111 BAC 111/SPEY MK511- Jet 2 Large Commercial 89 600 82 000 4 449 11 400 2 2JT8D CNT (lb) 201 101 Fuselage 14 BAE146 BAe 146-200/ALF502R- Jet 4 Large Commercial 93 000 81 000 3 770 6 970 3 AL502R CNT (lb) 206 108 Wing 5 BAE300 BAe 146-300/ALF502R- Jet 4 Large Commercial 97 500 84 500 3 960 6 970 3 AL502R CNT (lb) 206 108 Wing 5 BEC58P Raytheon BARON 58P/ Piston 2 Small General 6 100 6 100 2 733 779 0 TSIO52 CNT (% of 215 109 Prop TS10-520-L Aviation Max Static Thrust) 1.7.2015 EN Official Journal of the European Union L 168/681Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID CIT3 Cessna Citation III/ Jet 2 Large General 20 000 17 000 2 770 3 650 3 TF7313 CNT (lb) 216 113 Fuselage TFE731-3-100S Aviation CL600 Canadair CL-600/ Jet 2 Large General 36 000 33 000 3 300 7 500 3 AL502L CNT (lb) 216 113 Fuselage ALF502L Aviation CL601 Canadair CL-601/CF34- Jet 2 Large General 43 100 36 000 3 550 9 220 3 CF34 CNT (lb) 216 113 Fuselage 3A Aviation CNA172 Cessna 172R/Lycoming Piston 1 Small General 2 450 2 450 1 695 436 0 IO360L CNT (% of 215 109 Prop IO-360-L2A Aviation Max Static Thrust) CNA182 Cessna 182H/Continental Piston 1 Small General 2 800 2 800 1 544 965 2 O470R CNT (lb) 215 113 Prop O-470-R Aviation CNA206 Cessna 206H/Lycoming Piston 1 Small General 3 600 3 600 1 880 798 0 IO540 Other 215 109 Prop IO-540-AC Aviation (RPM) CNA208 Cessna 208/PT6A-114 Turbo­ 1 Small General 8 750 8 500 1 740 2 300 3 PT6­ CNT (lb) 210 109 Prop prop Aviation A114 CNA20T Cessna T206H/Lycoming Piston 1 Small General 3 600 3 600 1 880 825 0 TIO540 Other 215 109 Prop TIO-540-AJ1A Aviation (RPM) CNA441 Cessna CONQUEST II Turbo­ 2 Small Commercial 9 900 9 400 1 939 1 535 0 TPE331 CNT (% of 210 111 Prop /TPE331-8 prop Max Static Thrust) CNA500 Cessna Citation II/JT15D- Jet 2 Large General 14 700 14 000 3 050 2 500 3 JT15D1 CNT (lb) 216 113 Fuselage 4 Aviation CNA510 Cessna Mustang Model Jet 2 Small Commercial 8 645 7 200 3 010 1 466 0 PW615F CNT (lb) 203 113 Fuselage 510/PW615F CNA525C Cessna Citation Jet 2 Small Commercial 16 950 15 500 3 010 3 600 4 FJ44-4 CNT (lb) 235 136 Fuselage CJ4 525C /FJ44-4A L 168/682 EN Official Journal of the European Union 1.7.2015Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID CNA55B Cessna 550 Citation Jet 2 Large General 14 800 13 500 3 010 2 863 0 PW530A CNT (lb) 203 113 Fuselage Bravo/PW530A Aviation CNA560E Cessna Citation Encore Jet 2 Small Commercial 16 300 13 680 3 000 3 313 3 2PW535 CNT (lb) 238 138 Fuselage 560/PW535A CNA560U Cessna Citation Ultra Jet 2 Small Commercial 16 300 13 680 2 700 3 029 3 2J155D CNT (lb) 237 113 Fuselage 560/JT15D-5D CNA560XL Cessna Citation Excel Jet 2 Small Commercial 20 000 16 830 3 000 3 824 3 PW545A CNT (lb) 238 137 Fuselage 560/PW545A CNA680 Cessna Citation Sovereign Jet 2 Small Commercial 30 000 24 390 3 010 5 749 3 PW306C CNT (lb) 236 136 Fuselage 680/PW306C CNA750 Cessna Citation X/Rolls Jet 2 Large General 35 700 31 800 3 500 6 407 3 AE300C CNT (lb) 202 105 Fuselage Royce Allison AE3007C Aviation CONCRD Concorde/OLY593 Jet 4 Heavy Commercial 400 000 245 000 10 600 38 100 0 OLY593 CNT (lb) 206 106 Wing CRJ9-ER Bombardier CL-600- Jet 2 Large Commercial 82 500 73 500 5 779 13 525 3 CF348­ CNT (lb) 216 113 Fuselage 2D15/CL-600-2D24/ C5 CF34-8C5 CRJ9-LR Bombardier CL-600- Jet 2 Large Commercial 84 500 75 100 5 680 13 525 3 CF348­ CNT (lb) 216 113 Fuselage 2D15/CL-600-2D24/ C5 CF34-8C5 CVR580 Convair CV-580/ALL Turbo­ 2 Large Commercial 58 000 52 000 4 256 8 100 0 501D13 CNT (% of 214 112 Prop 501-D15 prop Max Static Thrust) DC1010 McDonnell Douglas Jet 3 Heavy Commercial 455 000 363 000 5 820 40 000 3 CF66D CNT (lb) 203 101 Wing DC10-10/CF6-6D DC1030 McDonnell Douglas Jet 3 Heavy Commercial 572 000 403 000 5 418 53 200 3 CF66D CNT (lb) 203 101 Wing DC10-30/CF6-50C2 1.7.2015 EN Official Journal of the European Union L 168/683Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID DC1040 McDonnell Douglas Jet 3 Heavy Commercial 555 000 403 000 6 020 49 400 3 CF66D CNT (lb) 203 101 Wing DC10-40/JT9D-20 DC3 Douglas DC-3/R1820-86 Piston 2 Large Commercial 28 000 24 500 2 222 3 120 0 2R2800 CNT (% of 213 110 Prop Max Static Thrust) DC6 Douglas DC-6/R2800- Piston 4 Large Commercial 106 000 95 000 3 010 4 180 0 4R2800 CNT (% of 213 110 Prop CB17 Max Static Thrust) DC820 Douglas DC-8-20/JT4A Jet 4 Heavy Commercial 317 600 194 400 6 527 11 850 1 JT4A CNT (lb) 208 107 Wing DC850 Douglas DC-8-50/JT3D- Jet 4 Heavy Commercial 325 000 240 000 5 400 18 000 1 JT3D CNT (lb) 208 107 Wing 3B DC860 Douglas DC-8-60/JT3D-7 Jet 4 Heavy Commercial 355 000 275 000 5 310 19 000 1 JT3D CNT (lb) 208 107 Wing DC870 Douglas DC-8-70/ Jet 4 Heavy Commercial 355 000 258 000 6 500 22 000 3 CFM562 CNT (lb) 206 106 Wing CFM56-2C-5 DC8QN Douglas DC-8-60/JT8D- Jet 4 Heavy Commercial 355 000 275 000 5 310 19 000 2 JT3DQ CNT (lb) 208 106 Wing 7QN DC910 McDonnell Douglas DC- Jet 2 Large Commercial 90 700 81 700 5 030 14 000 1 2JT8D CNT (lb) 201 101 Fuselage 9-10/JT8D-7 DC930 McDonnell Douglas DC- Jet 2 Large Commercial 114 000 102 000 4 680 14 500 1 2JT8D CNT (lb) 201 101 Fuselage 9-30/JT8D-9 DC93LW McDonnell Douglas DC- Jet 2 Large Commercial 114 000 102 000 4 680 14 500 3 2JT8DL CNT (lb) 201 101 Fuselage 9-30/JT8D-9 w/ ABS Lightweight hushkit DC950 McDonnell Douglas DC- Jet 2 Large Commercial 121 000 110 000 4 880 16 000 2 2JT8DQ CNT (lb) 201 101 Fuselage 9-50/JT8D-17 L 168/684 EN Official Journal of the European Union 1.7.2015Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID DC95HW McDonnell Douglas DC- Jet 2 Large Commercial 121 000 110 000 4 880 16 000 3 2JT8DH CNT (lb) 201 101 Fuselage 9-50/JT8D17 w/ ABS Heavyweight hushkit DC9Q7 McDonnell Douglas DC- Jet 2 Large Commercial 90 700 81 700 5 030 14 000 2 2JT8DQ CNT (lb) 201 101 Fuselage 9-10/JT8D-7QN DC9Q9 McDonnell Douglas DC- Jet 2 Large Commercial 114 000 102 000 4 680 14 500 2 2JT8DQ CNT (lb) 201 101 Fuselage 9-30/JT8D-9QN DHC6 De Havilland DASH 6/ Turbo­ 2 Small Commercial 12 500 12 300 1 500 2 000 0 PT6A27 CNT (% of 210 109 Prop PT6A-27 prop Max Static Thrust) DHC6QP De Havilland DASH 6/ Turbo­ 2 Small Commercial 12 500 12 300 1 500 2 000 0 RAISQP CNT (% of 210 109 Prop PT6A-27 Raisbeck Quiet prop Max Static PropMod Thrust) DHC7 De Havilland DASH 7/ Turbo­ 4 Large Commercial 41 000 39 000 2 150 2 850 3 PT6A50 CNT (% of 213 112 Prop PT6A-50 prop Max Static Thrust) DHC8 Bombardier de Havilland Turbo­ 2 Large Commercial 34 500 33 900 3 000 4 750 3 PW120 CNT (% of 213 112 Prop DASH 8-100/PW121 prop Max Static Thrust) DHC830 Bombardier de Havilland Turbo­ 2 Large Commercial 43 000 42 000 3 500 4 918 3 PW120 CNT (% of 213 112 Prop DASH 8-300/PW123 prop Max Static Thrust) DO228 Dornier 228-202/TPE Turbo­ 2 Large Commercial 13 669 13 448 2 375 2 240 3 TPE331- CNT (lb) 216 110 Prop 311-5 prop 5 DO328 Dornier 328-100/ Turbo­ 2 Large Commercial 30 843 29 167 3 825 6 745 3 PW119C CNT (lb) 214 109 Prop PW119C prop 1.7.2015 EN Official Journal of the European Union L 168/685Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID ECLIPS­ Eclipse 500/PW610F Jet 2 Small General 6 000 5 600 2 389 1 031 3 PW610F CNT (lb) 201 103 Fuselage E500 Aviation EMB120 Embraer 120 ER/Pratt & Turbo­ 2 Large Commercial 26 433 25 794 5 571 4 000 3 EPW118 CNT (lb) 213 109 Prop Whitney PW118 prop EMB145 Embraer 145 ER/Allison Jet 2 Large Commercial 45 420 41 230 4 232 7 500 3 AE3007 CNT (lb) 216 113 Fuselage AE3007 EMB14L Embraer 145 LR/Allison Jet 2 Large Commercial 48 500 42 550 4 232 7 500 3 AE3007 CNT (lb) 216 113 Fuselage AE3007A1 EMB170 Embraer ERJ170-100 Jet 2 Large Commercial 82 012 72 312 4 029 13 800 3 CF348E CNT (lb) 216 113 Wing EMB175 Embraer ERJ170-200 Jet 2 Large Commercial 85 517 74 957 4 130 13 800 3 CF348E CNT (lb) 216 113 Wing EMB190 Embraer ERJ190-100 Jet 2 Large Commercial 114 199 97 003 4 081 18 500 3 CF3410E CNT (lb) 205 105 Wing EMB195 Embraer ERJ190-200 Jet 2 Large Commercial 115 280 100 972 4 183 18 500 3 CF3410E CNT (lb) 205 105 Wing F10062 Fokker 100/TAY 620-15 Jet 2 Large Commercial 95 000 85 500 4 560 13 900 3 TAY620 CNT (lb) 201 101 Fuselage F10065 Fokker 100/TAY 650-15 Jet 2 Large Commercial 98 000 88 000 4 704 15 100 3 TAY650 CNT (lb) 201 101 Fuselage F28MK2 Fokker F-28-2000/ Jet 2 Large Commercial 65 000 59 000 3 540 9 850 2 RB183 CNT (lb) 216 104 Fuselage RB183MK555 F28MK4 Fokker F-28-4000/ Jet 2 Large Commercial 73 000 64 000 3 546 9 900 2 RB183P CNT (lb) 216 104 Fuselage RB183MK555 FAL20 Dassault FALCON 20/ Jet 2 Large General 28 700 27 300 2 490 4 500 2 CF700 CNT (lb) 203 113 Fuselage CF700-2D-2 Aviation L 168/686 EN Official Journal of the European Union 1.7.2015Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID GII Gulfstream GII/SPEY Jet 2 Large General 64 800 58 500 3 200 11 400 2 SPEYHK CNT (lb) 216 104 Fuselage 511-8 Aviation GIIB Gulfstream GIIB/GIII — Jet 2 Large General 69 700 58 500 3 250 11 400 2 SPEYHK CNT (lb) 216 104 Fuselage SPEY 511-8 Aviation GIV Gulfstream GIV-SP/TAY Jet 2 Large General 74 600 66 000 3 190 13 850 3 TAYGIV CNT (lb) 203 113 Fuselage 611-8 Aviation GV Gulfstream GV/BR 710 Jet 2 Large General 90 500 75 300 2 760 14 750 3 BR710 CNT (lb) 205 105 Fuselage Aviation HS748A Hawker Siddeley HS-748/ Turbo­ 2 Large Commercial 46 500 43 000 3 360 5 150 2 RDA532 CNT (% of 212 110 Prop DART MK532-2 prop Max Static Thrust) IA1125 IAI-1125 ASTRA/ Jet 2 Large General 23 500 20 700 3 689 3 700 3 TF7313 CNT (lb) 216 113 Fuselage TFE731-3A Aviation L1011 Lockheed Martin L-1011/ Jet 3 Heavy Commercial 430 000 358 000 5 693 42 000 3 RB2112 CNT (lb) 203 101 Wing RB211-22B L10115 Lockheed Martin L-1011- Jet 3 Heavy Commercial 510 000 368 000 6 800 50 000 3 RB2112 CNT (lb) 203 101 Wing 500/RB211-224B L188 Lockheed L-188C/ALL Turbo­ 4 Large Commercial 116 000 98 100 4 960 8 000 0 T56A7 CNT (% of 214 112 Prop 501-D13 prop Max Static Thrust) LEAR25 Learjet 25/CJ610-8 Jet 2 Large General 15 000 13 500 2 620 2 950 2 CJ610 CNT (lb) 202 113 Fuselage Aviation LEAR35 Learjet 36/TFE731-2 Jet 2 Large General 18 300 15 300 3 076 3 500 3 TF7312 CNT (lb) 216 113 Fuselage Aviation MD11GE McDonnell Douglas MD- Jet 3 Heavy Commercial 682 400 433 300 5 131 61 500 3 2CF68D CNT (lb) 203 103 Wing 11/CF6-80C2D1F MD11PW McDonnell Douglas MD- Jet 3 Heavy Commercial 682 400 433 300 4 681 60 000 3 PW4460 CNT (lb) 203 103 Wing 11/PW 4460 1.7.2015 EN Official Journal of the European Union L 168/687Max Sea Depar­ Max Approach Lateral Engine Numb of Weight Owner MGTOW MGLW Level Noise Power Para­ ture ACFTID Description Landing NPD_ID Spectral Directivity Type Engines Class Category (lb) (lb) Static Chapter meter Spectral Dist (ft) Class ID Identifier Thrust (lb) Class ID MD81 McDonnell Douglas MD- Jet 2 Large Commercial 140 000 128 000 4 860 19 300 3 2JT8D2 CNT (lb) 204 104 Fuselage 81/JT8D-209 MD82 McDonnell Douglas MD- Jet 2 Large Commercial 149 500 130 000 4 920 20 900 3 2JT8D2 CNT (lb) 204 104 Fuselage 82/JT8D-217A MD83 McDonnell Douglas MD- Jet 2 Large Commercial 160 000 139 500 5 200 21 700 3 2JT8D2 CNT (lb) 204 104 Fuselage 83/JT8D-219 MD9025 McDonnell Douglas MD- Jet 2 Large Commercial 156 000 142 000 3 000 25 000 3 V2525 CNT (lb) 205 105 Fuselage 90/V2525-D5 MD9028 McDonnell Douglas MD- Jet 2 Large Commercial 156 000 142 000 3 000 28 000 3 V2525 CNT (lb) 205 105 Fuselage 90/V2528-D5 MU3001 Mitsubishi MU300-10 Jet 2 Large General 14 100 13 200 2 800 2 500 3 JT15D5 CNT (lb) 203 113 Fuselage Diamond II/JT15D-5 Aviation PA28 Piper Warrior PA-28- Piston 1 Small General 2 325 2 325 1 695 400 0 O320D3 Other 213 113 Prop 161/O-320-D3G Aviation (RPM) PA30 Piper Twin Comanche Piston 2 Small General 3 600 3 600 1 654 777 0 IO320B CNT (lb) 213 113 Prop PA-30/IO-320-B1A Aviation PA31 Piper Navajo Chieftain Piston 2 Small General 7 000 7 000 1 850 1 481 0 TIO542 Other 213 109 Prop PA-31-350/TIO-5 Aviation (RPM) PA42 Piper PA-42/PT6A-41 Turbo­ 2 Small General 11 200 10 330 3 300 1 800 3 PT6A41 CNT (lb) 213 109 Prop prop Aviation SABR80 NA Sabreliner 80 Jet 2 Large General 33 720 27 290 2 490 3 962 2 CF700 CNT (lb) 203 113 Fuselage Aviation SD330 Short SD3-30/PT6A- Turbo­ 2 Large Commercial 22 900 22 600 3 650 2 670 3 PT6A45 CNT (% of 211 109 Prop 45AR prop Max Static Thrust) SF340 Saab SF340B/CT7-9B Turbo­ 2 Large Commercial 27 300 26 500 3 470 4 067 3 CT75 CNT (% of 211 110 Prop prop Max Static Thrust) L 168/688 EN Official Journal of the European Union 1.7.20151.7.2015 EN Official Journal of the European Union L 168/689 Table I-6 Default weights ACFTID Stage Length Weight (lb) 1900D 1 15 500 1900D 2 16 950 707 1 175 000 707 2 185 000 707 3 200 000 707 4 220 000 707 5 245 000 707 6 257 000 707120 1 175 000 707120 2 185 000 707120 3 200 000 707120 4 220 000 707120 5 245 000 707120 6 257 000 707320 1 214 000 707320 2 228 000 707320 3 240 000 707320 4 260 000 707320 5 286 000 707320 6 312 000 707320 7 330 000 707QN 1 214 000 707QN 2 228 000 707QN 3 240 000 707QN 4 260 000 707QN 5 286 000 707QN 6 312 000 707QN 7 330 000 717200 1 94 900 717200 2 99 700 717200 3 104 900 717200 4 110 400L 168/690 EN Official Journal of the European Union 1.7.2015 ACFTID Stage Length Weight (lb) 717200 5 112 700 717200 6 121 000 720 1 145 000 720 2 155 000 720 3 165 000 720 4 180 000 720 5 190 000 720B 1 165 000 720B 2 175 000 720B 3 185 000 720B 4 200 000 720B 5 210 000 727100 1 136 000 727100 2 143 000 727100 3 150 000 727100 4 158 000 727200 1 152 000 727200 2 163 000 727200 3 174 000 727200 4 185 000 727D15 1 156 000 727D15 2 164 000 727D15 3 175 000 727D15 4 189 000 727D15 5 204 000 727D17 1 157 000 727D17 2 169 000 727D17 3 180 000 727D17 4 189 000 727EM1 1 136 000 727EM1 2 143 000 727EM1 3 150 0001.7.2015 EN Official Journal of the European Union L 168/691 ACFTID Stage Length Weight (lb) 727EM1 4 158 000 727EM2 1 156 000 727EM2 2 164 000 727EM2 3 175 000 727EM2 4 189 000 727EM2 5 204 000 727Q15 1 156 000 727Q15 2 164 000 727Q15 3 175 000 727Q15 4 189 000 727Q15 5 204 000 727Q7 1 136 000 727Q7 2 143 000 727Q7 3 150 000 727Q7 4 158 000 727Q9 1 156 000 727Q9 2 168 000 727Q9 3 180 000 727Q9 4 191 000 727QF 1 136 000 727QF 2 143 000 727QF 3 150 000 727QF 4 158 000 737 1 82 000 737 2 85 000 737 3 92 000 737 4 100 000 737300 1 108 800 737300 2 114 100 737300 3 119 900 737300 4 131 800 7373B2 1 108 800L 168/692 EN Official Journal of the European Union 1.7.2015 ACFTID Stage Length Weight (lb) 7373B2 2 114 100 7373B2 3 119 900 7373B2 4 131 800 7373B2 M 139 500 737400 1 115 800 737400 2 121 400 737400 3 127 700 737400 4 138 200 737400 M 150 000 737500 1 103 400 737500 2 108 500 737500 3 114 100 737500 4 125 700 737500 5 126 900 737500 M 128 500 737700 1 120 000 737700 2 125 000 737700 3 130 300 737700 4 141 100 737700 5 154 400 737700 6 154 500 737800 1 133 300 737800 2 139 200 737800 3 145 500 737800 4 156 700 737800 5 167 600 737800 6 172 300 737D17 1 90 000 737D17 2 95 000 737D17 3 100 000 737D17 4 105 000 737N17 1 90 0001.7.2015 EN Official Journal of the European Union L 168/693 ACFTID Stage Length Weight (lb) 737N17 2 95 000 737N17 3 100 000 737N17 4 105 000 737N9 1 82 000 737N9 2 85 000 737N9 3 92 000 737N9 4 100 000 737QN 1 82 000 737QN 2 85 000 737QN 3 92 000 737QN 4 100 000 747100 1 475 000 747100 2 495 000 747100 3 520 000 747100 4 550 000 747100 5 625 000 747100 6 635 000 74710Q 1 475 000 74710Q 2 495 000 74710Q 3 520 000 74710Q 4 550 000 74710Q 5 625 000 74710Q 6 635 000 747200 1 525 000 747200 2 545 000 747200 3 565 000 747200 4 610 000 747200 5 665 000 747200 6 725 000 747200 7 775 000 74720A 1 475 000 74720A 2 500 000L 168/694 EN Official Journal of the European Union 1.7.2015 ACFTID Stage Length Weight (lb) 74720A 3 520 000 74720A 4 560 000 74720A 5 610 000 74720A 6 675 000 74720A 7 725 000 74720B 1 525 000 74720B 2 545 000 74720B 3 565 000 74720B 4 610 000 74720B 5 665 000 74720B 6 725 000 74720B 7 775 000 747400 1 545 000 747400 2 563 800 747400 3 583 100 747400 4 621 500 747400 5 669 500 747400 6 720 900 747400 7 776 600 747400 8 836 200 747400 9 875 000 7478 1 671 100 7478 2 691 200 7478 3 713 300 7478 4 752 400 7478 5 801 000 7478 6 853 400 7478 7 909 300 7478 8 969 000 7478 9 987 000 747SP 1 400 000 747SP 2 422 0001.7.2015 EN Official Journal of the European Union L 168/695 ACFTID Stage Length Weight (lb) 747SP 3 443 000 747SP 4 475 000 747SP 5 518 000 747SP 6 560 000 747SP 7 625 000 757300 1 203 900 757300 2 212 700 757300 3 222 100 757300 4 239 100 757300 5 260 700 757300 6 269 400 757PW 1 183 200 757PW 2 190 000 757PW 3 197 500 757PW 4 212 600 757PW 5 230 900 757PW 6 243 200 757PW 7 255 000 757RR 1 183 900 757RR 2 191 200 757RR 3 199 100 757RR 4 215 200 757RR 5 234 800 757RR 6 243 200 757RR 7 255 000 767300 1 265 000 767300 2 275 500 767300 3 286 400 767300 4 305 700 767300 5 330 000 767300 6 355 900 767300 7 367 700L 168/696 EN Official Journal of the European Union 1.7.2015 ACFTID Stage Length Weight (lb) 767400 1 288 818 767400 2 299 037 767400 3 310 125 767400 4 329 861 767400 5 354 427 767400 6 380 906 767400 7 422 420 767CF6 1 227 000 767CF6 2 236 000 767CF6 3 245 300 767CF6 4 261 400 767CF6 5 281 600 767CF6 6 303 300 767CF6 7 315 500 767JT9 1 228 500 767JT9 2 237 600 767JT9 3 247 000 767JT9 4 263 600 767JT9 5 284 600 767JT9 6 306 900 767JT9 7 317 100 777200 1 429 900 777200 2 442 400 777200 3 456 100 777200 4 483 100 777200 5 516 400 777200 6 551 700 777200 7 589 400 777200 8 629 500 777200 9 656 000 777300 1 435 100 777300 2 449 7001.7.2015 EN Official Journal of the European Union L 168/697 ACFTID Stage Length Weight (lb) 777300 3 465 300 777300 4 493 100 777300 5 527 700 777300 6 564 500 777300 7 636 100 7773ER 1 503 600 7773ER 2 519 100 7773ER 3 536 100 7773ER 4 565 800 7773ER 5 602 700 7773ER 6 642 600 7773ER 7 684 500 7773ER 8 728 900 7773ER 9 775 000 7878R 1 343 400 7878R 2 353 200 7878R 3 363 900 7878R 4 382 600 7878R 5 405 700 7878R 6 430 100 7878R 7 455 900 7878R 8 483 600 7878R 9 502 500 A300-622R 1 278 700 A300-622R 2 290 300 A300-622R 3 302 400 A300-622R 4 324 100 A300-622R 5 353 300 A300-622R 6 378 500 A300B4-203 1 262 000 A300B4-203 2 280 000 A300B4-203 3 295 000L 168/698 EN Official Journal of the European Union 1.7.2015 ACFTID Stage Length Weight (lb) A300B4-203 4 324 000 A300B4-203 5 357 000 A310-304 1 243 300 A310-304 2 253 000 A310-304 3 262 900 A310-304 4 280 700 A310-304 5 304 400 A310-304 6 346 100 A319-131 1 125 900 A319-131 2 131 000 A319-131 3 136 500 A319-131 4 146 100 A319-131 5 166 400 A320-211 1 133 400 A320-211 2 139 200 A320-211 3 145 200 A320-211 4 155 900 A320-211 5 169 800 A320-232 1 132 900 A320-232 2 138 500 A320-232 3 144 200 A320-232 4 154 300 A320-232 5 172 000 A321-232 1 156 800 A321-232 2 163 300 A321-232 3 170 000 A321-232 4 182 100 A321-232 5 206 100 A330-301 1 367 000 A330-301 2 378 500 A330-301 3 390 500 A330-301 4 411 7001.7.2015 EN Official Journal of the European Union L 168/699 ACFTID Stage Length Weight (lb) A330-301 5 439 200 A330-301 6 469 100 A330-301 7 478 400 A330-343 1 369 200 A330-343 2 380 800 A330-343 3 392 900 A330-343 4 414 300 A330-343 5 441 900 A330-343 6 472 000 A330-343 7 513 700 A340-211 1 369 500 A340-211 2 381 600 A340-211 3 394 100 A340-211 4 416 600 A340-211 5 446 000 A340-211 6 477 600 A340-211 7 573 200 A340-642 1 524 100 A340-642 2 540 700 A340-642 3 557 800 A340-642 4 588 000 A340-642 5 628 600 A340-642 6 671 300 A340-642 7 811 300 A380-841 1 799 160 A380-841 2 822 921 A380-841 3 847 265 A380-841 4 890 164 A380-841 5 945 893 A380-841 6 1 006 106 A380-841 7 1 066 266 A380-841 8 1 254 430L 168/700 EN Official Journal of the European Union 1.7.2015 ACFTID Stage Length Weight (lb) A380-861 1 798 928 A380-861 2 822 613 A380-861 3 846 941 A380-861 4 889 750 A380-861 5 943 737 A380-861 6 1 003 582 A380-861 7 1 066 266 A380-861 8 1 254 430 BAC111 1 74 000 BAC111 2 79 000 BAC111 3 85 000 BAE146 1 76 000 BAE146 2 84 000 BAE146 3 91 000 BAE300 1 80 000 BAE300 2 88 000 BAE300 3 96 000 BEC58P 1 5 500 CIT3 1 20 000 CL600 1 36 000 CL601 1 43 100 CNA172 1 2 450 CNA182 1 2 800 CNA206 1 3 000 CNA206 2 3 300 CNA206 3 3 600 CNA208 1 8 750 CNA20T 1 3 000 CNA20T 2 3 300 CNA20T 3 3 600 CNA441 1 9 850 CNA500 1 14 7001.7.2015 EN Official Journal of the European Union L 168/701 ACFTID Stage Length Weight (lb) CNA510 1 8 645 CNA525C 1 16 950 CNA55B 1 14 800 CNA560E 1 16 300 CNA560U 1 16 300 CNA560XL 1 20 000 CNA680 1 30 000 CNA750 1 35 700 CONCRD 1 340 000 CONCRD 2 340 000 CONCRD 3 375 000 CONCRD 4 375 000 CONCRD 5 400 000 CONCRD 6 400 000 CRJ9-ER 1 67 500 CRJ9-ER 2 71 000 CRJ9-ER 3 75 000 CRJ9-ER 4 80 000 CRJ9-ER 5 82 500 CRJ9-LR 1 65 500 CRJ9-LR 2 69 000 CRJ9-LR 3 73 000 CRJ9-LR 4 78 000 CRJ9-LR 5 84 500 CVR580 1 49 000 CVR580 2 54 000 CVR580 3 58 000 DC1010 1 325 000 DC1010 2 340 000 DC1010 3 360 000 DC1010 4 390 000 DC1010 5 420 000L 168/702 EN Official Journal of the European Union 1.7.2015 ACFTID Stage Length Weight (lb) DC1010 6 450 000 DC1030 1 375 000 DC1030 2 390 000 DC1030 3 405 000 DC1030 4 436 000 DC1030 5 476 000 DC1030 6 517 000 DC1030 7 561 000 DC1040 1 364 000 DC1040 2 379 000 DC1040 3 393 000 DC1040 4 423 000 DC1040 5 462 000 DC1040 6 502 000 DC1040 7 544 000 DC3 1 24 000 DC3 2 26 000 DC3 3 28 000 DC6 1 85 000 DC6 2 95 000 DC6 3 105 000 DC820 1 180 000 DC820 2 190 000 DC820 3 205 000 DC820 4 225 000 DC820 5 250 000 DC820 6 270 000 DC850 1 185 000 DC850 2 195 000 DC850 3 210 000 DC850 4 230 000 DC850 5 255 0001.7.2015 EN Official Journal of the European Union L 168/703 ACFTID Stage Length Weight (lb) DC850 6 275 000 DC860 1 220 000 DC860 2 230 000 DC860 3 245 000 DC860 4 265 000 DC860 5 290 000 DC860 6 305 000 DC860 7 325 000 DC870 1 220 000 DC870 2 230 000 DC870 3 245 000 DC870 4 265 000 DC870 5 290 000 DC870 6 305 000 DC870 7 325 000 DC8QN 1 220 000 DC8QN 2 230 000 DC8QN 3 245 000 DC8QN 4 265 000 DC8QN 5 290 000 DC8QN 6 305 000 DC8QN 7 325 000 DC910 1 70 000 DC910 2 78 000 DC910 3 85 000 DC930 1 93 500 DC930 2 103 000 DC930 3 112 000 DC93LW 1 93 500 DC93LW 2 103 000 DC93LW 3 112 000 DC950 1 100 000L 168/704 EN Official Journal of the European Union 1.7.2015 ACFTID Stage Length Weight (lb) DC950 2 107 000 DC950 3 115 000 DC95HW 1 100 000 DC95HW 2 107 000 DC95HW 3 115 000 DC9Q7 1 70 000 DC9Q7 2 78 000 DC9Q7 3 85 000 DC9Q9 1 93 500 DC9Q9 2 103 000 DC9Q9 3 112 000 DHC6 1 12 500 DHC6QP 1 12 500 DHC7 1 38 950 DHC8 1 31 000 DHC830 1 38 700 DO228 1 13 669 DO328 1 30 843 ECLIPSE500 1 5 500 ECLIPSE500 2 5 891 ECLIPSE500 3 6 000 EMB120 1 22 475 EMB145 1 35 500 EMB145 2 39 500 EMB145 3 41 800 EMB145 4 44 000 EMB14L 1 35 275 EMB14L 2 39 675 EMB14L 3 41 900 EMB14L 4 44 100 EMB14L 5 46 300 EMB14L 6 48 5001.7.2015 EN Official Journal of the European Union L 168/705 ACFTID Stage Length Weight (lb) EMB170 1 63 070 EMB170 2 66 599 EMB170 3 70 484 EMB175 1 65 698 EMB175 2 69 459 EMB175 3 73 518 EMB190 1 83 520 EMB190 2 87 757 EMB190 3 92 363 EMB190 4 100 656 EMB195 1 87 096 EMB195 2 91 558 EMB195 3 96 388 EMB195 4 105 138 F10062 1 78 000 F10062 2 86 000 F10062 3 93 000 F10065 1 80 000 F10065 2 88 000 F10065 3 96 000 F28MK2 1 58 000 F28MK2 2 64 000 F28MK4 1 61 000 F28MK4 2 66 000 F28MK4 3 73 000 FAL20 1 28 660 GII 1 56 000 GIIB 1 59 245 GIV 1 63 410 GV 1 76 925 HS748A 1 46 500 IA1125 1 23 500L 168/706 EN Official Journal of the European Union 1.7.2015 ACFTID Stage Length Weight (lb) L1011 1 330 000 L1011 2 340 000 L1011 3 355 000 L1011 4 370 000 L1011 5 400 000 L1011 6 430 000 L10115 1 345 000 L10115 2 355 000 L10115 3 370 000 L10115 4 385 000 L10115 5 413 000 L10115 6 441 000 L10115 7 470 000 L188 1 93 000 L188 2 102 000 L188 3 115 000 LEAR25 1 15 000 LEAR35 1 18 300 MD11GE 1 395 000 MD11GE 2 410 000 MD11GE 3 425 000 MD11GE 4 460 000 MD11GE 5 495 000 MD11GE 6 535 000 MD11GE 7 580 000 MD11PW 1 395 000 MD11PW 2 410 000 MD11PW 3 425 000 MD11PW 4 460 000 MD11PW 5 495 000 MD11PW 6 535 000 MD11PW 7 580 0001.7.2015 EN Official Journal of the European Union L 168/707 ACFTID Stage Length Weight (lb) MD81 1 120 680 MD81 2 127 804 MD81 3 135 134 MD81 4 140 000 MD82 1 120 383 MD82 2 127 379 MD82 3 134 584 MD82 4 145 838 MD82 5 149 500 MD83 1 121 555 MD83 2 128 361 MD83 3 135 456 MD83 4 147 079 MD83 5 160 000 MD9025 1 131 021 MD9025 2 137 490 MD9025 3 144 181 MD9025 4 151 107 MD9025 5 156 000 MD9028 1 131 021 MD9028 2 137 490 MD9028 3 144 181 MD9028 4 151 107 MD9028 5 156 000 MU3001 1 14 100 PA28 1 2 325 PA30 1 3 600 PA31 1 7 000 PA42 1 11 200 SABR80 1 28 660 SD330 1 21 800 SF340 1 24 548 SF340 2 27 275L 168/708 EN Official Journal of the European Union 1.7.2015 Table I-7 Jet engine coefficients K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) 1900D MaxClimb 2 548,8 – 6,7075 – 0,014 0 – 0,72 1900D MaxTakeoff 3 374,6 – 9,6869 – 0,0046 0 – 0,504 707320 General – 25 447,4 – 6,79039 – 0,01775 0 0 33 299,8 – 5 817 707320 MaxClimb 15 943,8 – 13,9584 0,1672 5,7074E-06 0 707320 MaxTakeoff 18 044,7 – 15,7976 0,1893 6,4595E-06 0 707QN General – 25 447,4 – 6,79039 – 0,01775 0 0 33 299,8 – 5 817 707QN MaxClimb 15 943,8 – 13,9584 0,1672 5,7074E-06 0 707QN MaxTakeoff 18 044,7 – 15,7976 0,1893 6,4595E-06 0 717200 MaxClimb 15 541,5 – 17,8282 0,253495 0 0 717200 MaxClimbHi­ 22 232 – 18,025 – 0,201 0 – 218 Temp 717200 MaxTakeoff 17 542,7 – 19,588 0,234981 0 0 717200 MaxTkoffHi­ 22 280,7 – 19,819 – 0,097 0 – 154,5 Temp 720B General – 27 419,9 – 5,81791 – 0,01175 0 0 35 654,5 – 6 560,9 720B MaxClimb 14 540,1 – 13,4149 0,121548 1,78264E-06 0 720B MaxTakeoff 16 768,6 – 15,471 0,140178 2,0559E-06 0 727100 General – 14 205,5 – 4,53212 0 0 0 16 602,8 – 1 403,02 727100 MaxClimb 12 029,2 – 7,99864 – 0,05203 5,44617E-06 0 727100 MaxTakeoff 13 218,9 – 8,78972 – 0,05717 5,9848E-06 0 727D15 General – 14 773,7 – 5,09534 0 0 0 17 717,3 – 1 845,07 727D15 MaxClimb 14 249,6 – 8,103 – 0,0436 0 – 103 727D15 MaxTakeoff 14 935,3 – 7,459 0,3337 0 – 14,78 727D15 MaxTkoffHi­ 15 524,3 – 7,066 0 0 – 32,38 Temp 727D17 General – 14 773,7 – 5,09534 0 0 0 17 717,3 – 1 845,071.7.2015 EN Official Journal of the European Union L 168/709 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) 727D17 MaxClimb 13 812,7 – 7,52948 0,207702 – 0,000025939 0 727D17 MaxTakeoff 15 519,8 – 8,46009 0,233373 – 0,000029145 0 727EM1 MaxClimb 12 029,2 – 7,99864 – 0,05203 5,44617E-06 0 727EM1 MaxTakeoff 13 218,9 – 8,78972 – 0,05717 5,9848E-06 0 727EM2 General – 14 773,7 – 5,09534 0 0 0 17 717,3 – 1 845,07 727EM2 MaxClimb 14 249,6 – 8,103 – 0,0436 0 – 103 727EM2 MaxTakeoff 14 935,3 – 7,459 0,3337 0 – 14,78 727EM2 MaxTkoffHi­ 15 524,3 – 7,066 0 0 – 32,38 Temp 727Q15 General – 14 773,7 – 5,09534 0 0 0 17 717,3 – 1 845,07 727Q15 MaxClimb 14 249,6 – 8,103 – 0,0436 0 – 103 727Q15 MaxTakeoff 14 935,3 – 7,459 0,3337 0 – 14,78 727Q15 MaxTkoffHi­ 15 524,3 – 7,066 0 0 – 32,38 Temp 727Q7 General – 14 205,5 – 4,53212 0 0 0 16 602,8 – 1 403,02 727Q7 MaxClimb 12 029,2 – 7,99864 – 0,05203 5,44617E-06 0 727Q7 MaxTakeoff 13 218,9 – 8,78972 – 0,05717 5,9848E-06 0 727Q9 General – 14 095,4 – 4,77532 0 0 0 16 666,2 – 1 490,42 727Q9 MaxClimb 12 746,2 – 8,11613 – 0,00049 – 4,53384E-06 0 727Q9 MaxTakeoff 13 705,6 – 8,72702 – 0,00053 – 4,8751E-06 0 727QF General – 10 908 – 23,3571 – 0,0723 – 0,00000138 0 10 929,8 2 380,86 727QF MaxClimb 11 266 – 9,335 0,169297 – 4,70391E-06 0 727QF MaxClimbHi­ 13 966 – 9,335 0 0 – 90 Temp 727QF MaxContHi­ 14 687 – 9,335 0 0 – 90 Temp 727QF MaxContinuous 11 987 – 9,335 0,158001 – 4,70391E-06 0 727QF MaxTakeoff 14 100 – 12,25 0,1495 – 0,00001175 0L 168/710 EN Official Journal of the European Union 1.7.2015 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) 727QF MaxTkoffHi­ 16 800 – 12,25 0 0 – 90 Temp 737 General – 14 095,4 – 4,77532 0 0 0 16 666,2 – 1 490,42 737 MaxClimb 12 740,1 – 7,93589 – 0,02662 – 4,2762E-07 0 737 MaxTakeoff 13 847,9 – 8,62596 – 0,02894 – 4,648E-07 0 737300 General 11 106 – 10,09 – 0,0409 0 0 – 369,8 4,835 737300 MaxClimb 17 383,1 – 15,6072 0,148043 – 0,000001 – 24,2 737300 MaxClimbHi­ 20 363,9 – 17,0452 – 0,06578 – 0,000001 – 119 Temp 737300 MaxTakeoff 19 347 – 25,8689 0,456499 – 0,0000112 – 14,78 737300 MaxTkoffHi­ 21 143,7 – 26,2402 0,398451 – 0,000014 – 79,95 Temp 7373B2 General 11 106 – 10,09 – 0,0409 0 0 – 369,8 4,835 7373B2 MaxClimb 18 623,5 – 16,4797 0,169674 0 – 9,126 7373B2 MaxClimbHi­ 21 906,6 – 17,4327 – 0,07536 0 – 132,5 Temp 7373B2 MaxTakeoff 21 480,7 – 25,888 0,225791 0 – 8,441 7373B2 MaxTkoffHi­ 25 393,2 – 25,7175 – 0,0246 0 – 141,3 Temp 737400 General 21 384 – 13,79 – 0,0435 0 0 – 615,8 6,409 737400 MaxClimb 19 662,2 – 18,221 0,207237 0 0 737400 MaxClimbHi­ 22 875,1 – 18,001 – 0,07615 0 – 124,7 Temp 737400 MaxTakeoff 22 116,3 – 26,0175 0,259442 0 0 737400 MaxTkoffHi­ 26 883,2 – 26,1707 – 0,04324 0 – 159,7 Temp 737500 General 11 106 – 10,09 0,0409 0 0 – 369,8 4,835 737500 MaxClimb 17 530,9 – 16,3556 0,153997 – 0,0000013 – 23,39 737500 MaxClimbHi­ 20 510,5 – 17,1336 – 0,07687 – 0,0000004 – 122,3 Temp1.7.2015 EN Official Journal of the European Union L 168/711 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) 737500 MaxTakeoff 19 629,4 – 26,7504 0,550433 – 0,0000217 – 7,999 737500 MaxTkoffHi­ 22 636,2 – 28,0937 0,225263 0,0000409 – 105,6 Temp 737700 MaxClimb 22 106,7 – 23,7147 0,165546 0,0000065 0 737700 MaxClimbHi­ 29 618,1 – 24,596 – 0,273 0 – 249,1 Temp 737700 MaxTakeoff 23 534,8 – 29,3547 0,308407 0 0 737700 MaxTkoffHi­ 29 335,5 – 28,632 – 0,105 0 – 195,6 Temp 737800 MaxClimb 22 403,5 – 27,2645 0,305603 0 0 737800 MaxClimbHi­ 26 593,3 – 26,293 – 0,078 0 – 174,4 Temp 737800 MaxTakeoff 26 089,1 – 29,1098 0,143559 0 0 737800 MaxTkoffHi­ 30 143,2 – 29,773 – 0,029 0 – 145,2 Temp 737D17 General – 14 773,7 – 5,09534 0 0 0 17 717,3 – 1 845,07 737D17 MaxClimb 13 083,2 – 7,13185 0,196733 – 0,000024569 0 737D17 MaxTakeoff 15 519,8 – 8,46009 0,233373 – 0,000029145 0 737N17 General – 14 773,7 – 5,09534 0 0 0 17 717,3 – 1 845,07 737N17 MaxClimb 13 083,2 – 7,13185 0,196733 – 0,000024569 0 737N17 MaxTakeoff 15 519,8 – 8,46009 0,233373 – 0,000029145 0 737N9 General – 14 095,4 – 4,77532 0 0 0 16 666,2 – 1 490,42 737N9 MaxClimb 12 740,1 – 7,93589 – 0,02662 – 4,2762E-07 0 737N9 MaxTakeoff 13 847,9 – 8,62596 – 0,02894 – 4,648E-07 0 737QN General – 14 095,4 – 4,77532 0 0 0 16 666,2 – 1 490,42 737QN MaxClimb 12 740,1 – 7,93589 – 0,02662 – 4,2762E-07 0 737QN MaxTakeoff 13 847,9 – 8,62596 – 0,02894 – 4,648E-07 0 74710Q General – 141 079 – 11,7298 – 0,02833 0 0 201 105 – 53 843 74710Q MaxClimb 36 791,4 – 43,5074 0,3004 – 0,0000092 0L 168/712 EN Official Journal of the European Union 1.7.2015 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) 74710Q MaxTakeoff 42 780,7 – 50,59 0,349279 – 0,000010697 0 747200 General – 141 079 – 11,7298 – 0,02833 0 0 201 105 – 53 843 747200 MaxClimb 36 791,4 – 43,5074 0,3004 – 0,0000092 0 747200 MaxTakeoff 42 780,7 – 50,59 0,349279 – 0,000010697 0 74720A General – 32 370 – 7,83 – 0,02105 0 0 47 590 0 74720A MaxClimb 34 860 – 35 0,4962 0 0 74720A MaxTakeoff 40 870 – 40,11 0,4435 0 0 74720B General – 28 110 – 10,05 – 0,03543 0 0 46 375 0 74720B MaxClimb 39 594 – 38,08 0,5262 0 0 74720B MaxTakeoff 48 866 – 43,68 0,6641 0 0 747400 General – 49 250 0 0 0 0 62 210 0 747400 MaxClimb 44 157,4 – 42,6142 0,635772 0 0 747400 MaxClimbHi­ 56 826,2 – 45,4912 – 0,20856 0 – 392,3 Temp 747400 MaxTakeoff 53 290,5 – 53,434 0,606283 0 0 747400 MaxTkoffHi­ 66 921,4 – 54,5627 – 0,1278 0 – 410,2 Temp 7478 IdleApproach 5 920 – 19,02 0,225 0 0 7478 MaxClimb 50 523 – 39,8663 0,842437 – 0,000015 0 7478 MaxClimbHi­ 56 739,2 – 27,469 – 0,1411 – 0,000015 – 343,137 Temp 7478 MaxTakeoff 64 247,2 – 66,0662 0,481932 0,000004 0 7478 MaxTkoffHi­ 80 923,7 – 71,3162 – 0,30655 – 0,00001 – 520,464 Temp 747SP General – 141 079 – 11,7298 – 0,02833 0 0 201 105 – 53 843 747SP MaxClimb 36 791,4 – 43,5074 0,3004 – 0,0000092 0 747SP MaxTakeoff 42 780,7 – 50,59 0,349279 – 0,000010697 0 757300 MaxClimb 29 549,2 – 30,6086 0,398179 0 01.7.2015 EN Official Journal of the European Union L 168/713 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) 757300 MaxClimbHi­ 36 157 – 30,9643 – 0,16465 0 – 250,7 Temp 757300 MaxTakeoff 40 175,5 – 35,323 – 0,11328 0 0 757300 MaxTkoffHi­ 46 892,4 – 35,6127 – 0,53031 0 – 241,7 Temp 757PW General – 44 951 – 0,83 0,0198 0 0 52 972 0 757PW MaxClimb 27 775,1 – 27,6876 0,381725 0 0 757PW MaxClimbHi­ 34 748,3 – 29,9467 – 0,16641 0 – 250,7 Temp 757PW MaxTakeoff 36 214,8 – 48,2704 0,908044 0 0 757PW MaxTkoffHi­ 45 592,5 – 49,7383 0,213208 0 – 290,6 Temp 757RR General – 44 907 – 21,97 – 0,0589 0 0 46 999 0 757RR MaxClimb 30 065,2 – 32,4779 0,397321 0 0 757RR MaxClimbHi­ 36 735,1 – 32,445 – 0,16871 0 – 258,4 Temp 757RR MaxTakeoff 37 802,1 – 38,2839 0,527181 0 0 757RR MaxTkoffHi­ 45 336,5 – 39,1302 – 0,00514 0 – 257,4 Temp 767300 General – 49 250 0 0 0 0 62 210 0 767300 MaxClimb 45 480 – 41,9 0,559 0 0 767300 MaxTakeoff 56 370 – 53 0,251 0 0 767400 MaxClimb 45 902,7 – 39,5895 0,633446 0 0 767400 MaxClimbHi­ 63 647,5 – 41,082 – 0,55 0 – 562,3 Temp 767400 MaxTakeoff 60 475,4 – 56,8041 0,478788 0 0 767400 MaxTkoffHi­ 72 425,5 – 55,569 – 0,236 0 – 416,2 Temp 767CF6 General 62 790 – 35,03 – 0,1177 0 0 – 1 610,37 14 767CF6 MaxClimb 38 057 – 43,24 0,705 0 0 767CF6 MaxTakeoff 44 769 – 48,34 0,5 0 0L 168/714 EN Official Journal of the European Union 1.7.2015 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) 767JT9 General – 39 777 – 17,367 – 0,0467 0 0 56 550 0 767JT9 MaxClimb 38 700 – 34,5 0,49 0 0 767JT9 MaxTakeoff 43 190 – 38,3 0,876 0 0 777200 General 32 710 0 0 0 0 – 1 258 16,16 777200 MaxClimb 67 093,7 – 85,7553 1,8498 – 0,000076 0 777200 MaxClimbHi­ 82 096,7 – 72,2859 – 0,32818 – 0,0000179 – 637 Temp 777200 MaxTakeoff 93 672,6 – 122,251 1,1818 – 0,0000806 0 777200 MaxTkoffHi­ 114 758,6 – 125,38 – 0,159 – 0,0000261 – 702,4 Temp 777300 MaxClimb 64 636,2 – 70,833 0,880073 0 0 777300 MaxClimbHi­ 90 015,1 – 70,745 – 0,852 0 – 823 Temp 777300 MaxTakeoff 87 833,8 – 97,7894 0,27543 0 0 777300 MaxTkoffHi­ 103 835,2 – 97,831 – 0,632 0 – 549,1 Temp 7773ER IdleApproach 8 950 – 27,25 0,131 0 0 7773ER MaxClimb 92 110 – 119 1,14 – 0,000007 0 7773ER MaxClimbHi­ 96 550 – 69,4 – 0,542 – 0,00005 – 533 Temp 7773ER MaxTakeoff 112 250 – 120 0,713 – 0,00011 0 7878R IdleApproach 3 425 – 12,03 0,0955 0 0 7878R MaxClimb 61 142,6 – 78,8116 1,219801 – 0,000039 0 7878R MaxClimbHi­ 65 000 – 55 0,1 – 0,00002 – 404,274 Temp 7878R MaxTakeoff 71 214,6 – 93,4796 0,652462 0,000002 0 7878R MaxTkoffHi­ 86 784,2 – 92 – 0,27021 – 0,00001 – 520,488 Temp A300-622R General – 148 952 – 6,71 – 0,03 0 0 203 740 – 50 104,71.7.2015 EN Official Journal of the European Union L 168/715 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) A300-622R IdleApproach 8 432,8 – 47,7662 0,750523 – 0,000059071 0 A300-622R IdleApproachHi­ 8 432,8 – 47,7662 0,750523 – 0,000059071 0 Temp A300-622R MaxClimb 44 457,2 – 45,778 0,735506 – 0,000015775 0 A300-622R MaxClimbHi­ 52 183,7 – 44,1929 0 0 – 271 Temp A300-622R MaxTakeoff 56 307,1 – 50,9157 0,405632 – 2,0986E-06 0 A300-622R MaxTkoffHi­ 61 250,3 – 51,5373 0 0 – 192 Temp A300B4-203 General – 132 687 – 30,4092 – 0,10796 4,02686E-07 0 2 535,75 – 8,23842 A300B4-203 MaxClimb 43 416,5 – 35 – 0,12523 6,27209E-07 0 A300B4-203 MaxTakeoff 49 336,9 – 39,8243 – 0,14231 7,12738E-07 0 A310-304 General 41 317 – 32,9 – 0,0857 – 0,0000016 0 – 1 131,6 11,8 A310-304 IdleApproach 4 613,2 – 22,0136 0,082133 – 2,7376E-06 0 A310-304 IdleApproachHi­ 4 613,2 – 22,0136 0,082133 – 2,7376E-06 0 Temp A310-304 MaxClimb 42 008 – 49,5706 1,64076 – 0,000043059 0 A310-304 MaxClimbHi­ 55 143,3 – 37,4839 0 0 – 505 Temp A310-304 MaxTakeoff 50 530,5 – 51,1538 1,26398 – 0,000012839 0 A310-304 MaxTkoffHi­ 71 457,7 – 50,7768 0 0 – 608 Temp A319-131 General – 105 513 – 6,58 0,006828 – 8,055E-07 0 149 900 – 42 300 A319-131 IdleApproach 1 219,5 – 7,22737 0,154266 – 0,000007955 0 A319-131 IdleApproachHi­ 1 219,5 – 7,22737 0,154266 – 0,000007955 0 Temp A319-131 MaxClimb 14 957,2 1,71654 0,442593 – 0,000013824 0 A319-131 MaxClimbHi­ 12 977,6 18,59062 0 0 – 78,7 Temp A319-131 MaxTakeoff 21 435,4 – 21,3236 0,309465 1,26125E-05 0L 168/716 EN Official Journal of the European Union 1.7.2015 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) A319-131 MaxTkoffHi­ 23 853,8 – 18,7311 0 0 – 76,8 Temp A320-211 General 24 380 – 18,534 – 0,07842 – 2,509E-07 0 – 669,457 6,9451 A320-211 IdleApproach 2 858,8 – 14,7325 0,096537 – 6,7861E-06 0 A320-211 IdleApproachHi­ 2 858,8 – 14,7325 0,096537 – 6,7861E-06 0 Temp A320-211 MaxClimb 16 859,1 – 4,3786 0,183576 2,9851E-06 0 A320-211 MaxClimbHi­ 19 148,5 – 6,50173 0 0 – 95 Temp A320-211 MaxTakeoff 23 652,9 – 22,9338 0,295879 – 5,4631E-06 0 A320-211 MaxTkoffHi­ 27 385 – 23,3 0 0 – 132 Temp A320-232 General – 65 083,3 – 7,25 – 0,01918 2,575E-08 0 87 817,6 – 18 693,1 A320-232 IdleApproach 1 138,9 – 6,52566 0,1667 – 9,2579E-06 0 A320-232 IdleApproachHi­ 1 138,9 – 6,52566 0,1667 – 9,2579E-06 0 Temp A320-232 MaxClimb 15 539,2 – 4,08932 0,438331 – 0,00001439 0 A320-232 MaxClimbHi­ 14 111,4 10,67953 0 0 – 82,2 Temp A320-232 MaxTakeoff 24 746,2 – 25,2473 0,304165 9,2451E-06 0 A320-232 MaxTkoffHi­ 29 506,5 – 24,4165 0 0 – 139 Temp A321-232 General – 26 190,2 – 6,6 – 0,0197 – 3,408E-07 0 33 032,2 0 A321-232 IdleApproach 1 274,1 – 7,34054 0,175187 – 0,000011478 0 A321-232 IdleApproachHi­ 1 274,1 – 7,34054 0,175187 – 0,000011478 0 Temp A321-232 MaxClimb 21 870,8 – 21,4867 0,380647 – 5,5566E-06 0 A321-232 MaxClimbHi­ 24 158,5 – 16,8504 0 0 – 147 Temp A321-232 MaxTakeoff 28 636,4 – 26,7318 0,249782 – 3,9163E-06 01.7.2015 EN Official Journal of the European Union L 168/717 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) A321-232 MaxTkoffHi­ 31 608,2 – 25,9736 0 0 – 114 Temp A330-301 General – 36 339,3 – 31,32 – 0,1297 0 0 484,645 4,0056 A330-301 IdleApproach 4 572,4 – 26,0005 0,013461 2,8669E-06 0 A330-301 IdleApproachHi­ 4 572,4 – 26,0005 0,013461 2,8669E-06 0 Temp A330-301 MaxClimb 34 249,9 25,9859 0,764157 – 8,1437E-07 0 A330-301 MaxClimbHi­ 46 667,8 10,51272 0 0 – 346 Temp A330-301 MaxTakeoff 61 384,5 – 48,4678 0,582821 – 6,2628E-06 0 A330-301 MaxTkoffHi­ 69 058 – 46,465 0 0 – 288 Temp A330-343 General – 127 410 – 9,31 – 0,0386 0,000000569 0 162 922 – 29 498,6 A330-343 IdleApproach 3 134,3 – 13,0338 0,085938 1,7155E-06 0 A330-343 IdleApproachHi­ 3 134,3 – 13,0338 0,085938 1,7155E-06 0 Temp A330-343 MaxClimb 44 462 – 12,031 0,711026 5,12762E-06 0 A330-343 MaxClimbHi­ 63 522,4 – 50,7504 0 0 – 411 Temp A330-343 MaxTakeoff 69 831 – 77,9676 0,882955 – 0,000026894 0 A330-343 MaxTkoffHi­ 85 732,2 – 78,8957 0 0 – 451 Temp A340-211 General 19 716 – 17,65 – 0,0878 0 0 – 590,77 7,341 A340-211 IdleApproach 4 019,5 – 20,508 – 0,02271 1,16972E-05 0 A340-211 IdleApproachHi­ 4 019,5 – 20,508 – 0,02271 1,16972E-05 0 Temp A340-211 MaxClimb 26 802,9 – 28,8264 0,31673 3,50144E-06 0 A340-211 MaxClimbHi­ 31 091,8 – 31,4492 0 0 – 160 Temp A340-211 MaxTakeoff 29 929,8 – 30,7732 0,29922 – 4,1757E-06 0L 168/718 EN Official Journal of the European Union 1.7.2015 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) A340-211 MaxTkoffHi­ 34 594,4 – 30,094 0 0 – 175 Temp A340-642 IdleApproach 6 529,4 – 29,9521 0,272155 – 0,000020281 0 A340-642 IdleApproachHi­ 6 529,4 – 29,9521 0,272155 – 0,000020281 0 Temp A340-642 MaxClimb 42 621,6 – 44,2784 0,484124 2,668E-07 0 A340-642 MaxClimbHi­ 50 112 – 60,5262 0 0 – 212 Temp A340-642 MaxTakeoff 55 248,1 – 61,4744 0,506968 – 9,6324E-06 0 A340-642 MaxTkoffHi­ 63 276,8 – 59,6458 0 0 – 300 Temp A380-841 IdleApproach 10 914,8 – 31,2899 – 2,1424 0,000260636 0 A380-841 IdleApproachHi­ 10 914,8 – 31,2899 – 2,1424 0,000260636 0 Temp A380-841 MaxClimb 63 586,2 – 53,9292 1,23082 – 0,00003343 0 A380-841 MaxClimbHi­ 72 974,3 – 52,6993 0 0 – 420 Temp A380-841 MaxTakeoff 71 176,1 – 84,4052 0,220679 0,000428339 0 A380-841 MaxTkoffHi­ 90 820,8 – 94,5354 0 0 – 610 Temp A380-861 IdleApproach 8 921,7 – 30,2153 – 0,87777 0,000104691 0 A380-861 IdleApproachHi­ 8 921,7 – 30,2153 – 0,87777 0,000104691 0 Temp A380-861 MaxClimb 66 053,2 – 61,754 0,977183 – 0,000025178 0 A380-861 MaxClimbHi­ 73 729,7 – 65,1895 0 0 – 324 Temp A380-861 MaxTakeoff 70 053,6 – 76,0931 0,838794 – 0,000010766 0 A380-861 MaxTkoffHi­ 83 320,5 – 82,3362 0 0 – 432 Temp BAC111 MaxClimb 9 827,9 – 5,89674 – 0,01966 0 01.7.2015 EN Official Journal of the European Union L 168/719 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) BAC111 MaxTakeoff 11 168,1 – 6,70084 – 0,02234 0 0 BAE146 General – 13 783 – 9,9585 0,056057 – 1,23124E-05 0 304,295 – 0,84327 BAE146 MaxClimb 6 339,4 – 9,9585 0,056057 – 0,0000035 0 BAE146 MaxTakeoff 6 542,4 – 9,9585 0,056057 – 0,0000035 0 BAE300 General – 13 783 – 9,9585 0,056057 – 1,23124E-05 0 304,295 – 0,84327 BAE300 MaxClimb 6 339,4 – 9,9585 0,056057 – 0,0000035 0 BAE300 MaxTakeoff 6 542,4 – 9,9585 0,056057 – 0,0000035 0 CIT3 MaxClimb 2 987,4 – 3,4992 0,06123 – 1,1664E-06 0 CIT3 MaxTakeoff 3 319,3 – 3,888 0,068032 – 0,000001296 0 CL600 MaxClimb 5 543,3 – 5,6542 0,08442 0 0 CL600 MaxTakeoff 6 159,2 – 6,2824 0,0938 0 0 CL601 MaxClimb 6 517,3 – 6,6476 0,09776 0 0 CL601 MaxTakeoff 7 241,4 – 7,3862 0,10862 0 0 CNA208 MaxClimb 2 953,9 – 8,581 – 0,00453 – 7,2035E-07 – 1,44 CNA208 MaxTakeoff 3 245,2 – 11,69 – 0,01053 – 6,777E-07 – 1,62 CNA500 General 1 743,1 – 1,64678 – 0,00201 – 1,5642E-07 0 – 49,6794 0,545 CNA500 MaxClimb 1 919,5 – 1,99614 0,0615 – 2,40502E-06 0 CNA500 MaxTakeoff 2 132,8 – 2,21793 0,068333 – 2,67224E-06 0 CNA510 General 4 234,6 – 1,68388 0,001047 – 5,78019E-08 0 – 103,817 0,811333 CNA510 MaxClimb 1 486 – 1,60533 0 – 1,04748E-07 0 CNA510 MaxTakeoff 1 492,8 – 1,87734 0 – 2,55208E-06 0 CNA525C General 1 528,4 – 2,83667 – 0,00013 2,55648E-07 0 – 51,50512788 0,724013467L 168/720 EN Official Journal of the European Union 1.7.2015 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) CNA525C MaxClimb 3 001,7 – 2,38854 0,004585 – 1,4045E-07 0 CNA525C MaxTakeoff 3 464,1 – 2,5254 0,001981 – 1,46353E-06 0 CNA55B General 1 373,8 – 2,2903 – 8,9E-05 3,2273E-08 0 – 44,861 0,66327 CNA55B MaxClimb 2 323,1 – 2,4386 0,002159 – 2,1456E-07 0 CNA55B MaxTakeoff 2 658,7 – 2,6269 – 0,00359 1,7262E-07 0 CNA560E General 1 533,4 – 2,49247 0,011973 – 6,90894E-07 0 – 53,9835 0,839574 CNA560E MaxClimb 3 194,3 – 2,53358 0,028038 2,70832E-07 0 CNA560E MaxTakeoff 3 316,5 – 2,7005 0,04349 – 6,52616E-07 0 CNA560U MaxClimb 2 597,5 – 2,22178 0,023781 6,12239E-08 0 CNA560U MaxTakeoff 2 920 – 2,0264 0,025133 2,95314E-07 0 CNA560XL MaxClimb 3 454,5 – 3,98132 – 0,0704 0 0 CNA560XL MaxTakeoff 3 838,3 – 4,42368 – 0,07823 0 0 CNA680 General 2 904,8 – 4,80092 – 0,00174 5,62892E-07 0 – 101,327 1,3401 CNA680 MaxClimb 5 520,2 – 5,32711 – 0,02377 1,89918E-06 0 CNA680 MaxTakeoff 5 683 – 6,55907 – 0,00159 8,72971E-07 0 CNA750 General 4 778,6 – 6,56521 0,000671 – 4,11321E-07 0 – 146,712 1,9748 CNA750 MaxClimb 6 097,8 – 7,0102 – 0,00528 3,74689E-08 0 CNA750 MaxTakeoff 6 127,8 – 7,07624 – 0,00394 3,95764E-08 0 CONCRD MaxClimb 33 252,1 – 26,6 0,2328 0 0 CONCRD MaxTakeoff 39 653 – 31,722 0,2776 0 0 CRJ9-ER General 6 087,3 – 9,35507 – 0,04736 1,55476E-07 – 1,4767 – 183,9266 2,785981 CRJ9-ER IdleApproach 1 163,1 – 4,5855 – 0,0238 1,63611E-06 – 0,0249 CRJ9-ER MaxClimb 10 438,3 – 9,64192 0,15855 – 3,00077E-07 – 1,3095 CRJ9-ER MaxClimbHi­ 12 973,4 – 9,57675 – 0,05589 3,05523E-07 – 100,415 Temp CRJ9-ER MaxTakeoff 13 260,6 – 16,6244 0,19849 – 7,00045E-06 – 1,62241.7.2015 EN Official Journal of the European Union L 168/721 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) CRJ9-ER MaxTkoffHi­ 16 247,3 – 17,4575 0,077341 – 1,06353E-05 – 109,219 Temp CRJ9-LR General 6 087,3 – 9,35507 – 0,04736 1,55476E-07 – 1,4767 – 183,9266 2,785981 CRJ9-LR IdleApproach 1 163,1 – 4,5855 – 0,0238 1,63611E-06 – 0,0249 CRJ9-LR MaxClimb 10 438,3 – 9,64192 0,15855 – 3,00077E-07 – 1,3095 CRJ9-LR MaxClimbHi­ 12 973,4 – 9,57675 – 0,05589 3,05523E-07 – 100,415 Temp CRJ9-LR MaxTakeoff 13 260,6 – 16,6244 0,19849 – 7,00045E-06 – 1,6224 CRJ9-LR MaxTkoffHi­ 16 247,3 – 17,4575 0,077341 – 1,06353E-05 – 109,219 Temp DC1010 General 25 027,6 – 27,4313 – 0,07828 0 0 – 694,556 8,02362 DC1010 MaxClimb 30 596 – 28,4416 – 0,10164 5,0902E-07 0 DC1010 MaxTakeoff 35 985,4 – 30,9909 – 0,11075 5,5465E-07 0 DC1030 MaxClimb 38 520 – 29,38 0,49 0 0 DC1030 MaxTakeoff 49 310 – 42,42 0,61 0 0 DC1040 General – 143 602 – 14,4996 – 0,05026 0 0 204 567 – 54 761,9 DC1040 MaxClimb 34 087,9 – 12,9859 – 0,04641 2,3241E-07 0 DC1040 MaxTakeoff 41 594,9 – 22,3071 – 0,07971 3,9923E-07 0 DC850 General – 22 582,8 – 6,58409 – 0,02081 0 0 29 070,9 – 4 341,84 DC850 MaxClimb 14 243,5 – 5,6565 – 0,02021 1,0123E-07 0 DC850 MaxTakeoff 15 670,3 – 5,8955 – 0,02107 1,0551E-07 0 DC860 General – 27 959,5 – 6,35297 – 0,01835 0 0 35 850,3 – 6 157,74 DC860 MaxClimb 15 558,7 – 7,2339 – 0,02585 1,2947E-07 0 DC860 MaxTakeoff 16 740,5 – 4,9394 – 0,01765 8,8401E-08 0 DC870 General 11 106 – 10,09 – 0,0409 0 0 – 369,8 4,835 DC870 MaxClimb 18 859 – 17,91 0,1953 0 – 2,034 DC870 MaxTakeoff 20 758 – 20,65 0,2173 0 0L 168/722 EN Official Journal of the European Union 1.7.2015 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) DC8QN General – 27 959,5 – 6,35297 – 0,01835 0 0 35 850,3 – 6 157,74 DC8QN MaxClimb 15 558,7 – 7,2339 – 0,02585 1,2947E-07 0 DC8QN MaxTakeoff 16 740,5 – 4,9394 – 0,01765 8,8401E-08 0 DC910 General – 10 596,5 – 1,51369 – 0,00525 0 0 11 541,7 162,698 DC910 MaxClimb 11 194,3 – 3,0274 – 0,01082 5,4181E-08 0 DC910 MaxTakeoff 12 308,2 – 0,478 0,001708 8,55E-09 0 DC930 General – 13 523,2 – 2,66888 – 0,00925 0 0 15 803,6 – 1 257,94 DC930 MaxClimb 11 561,8 – 2,94773 – 0,01053 5,2756E-08 0 DC930 MaxTakeoff 12 972 – 2,31038 – 0,00826 4,1349E-08 0 DC93LW General – 13 523,2 – 2,66888 – 0,00925 0 0 15 803,6 – 1 257,94 DC93LW MaxClimb 11 561,8 – 2,94773 – 0,01053 5,2756E-08 0 DC93LW MaxTakeoff 12 972 – 2,31038 – 0,00826 4,1349E-08 0 DC950 General – 13 523,2 – 2,66888 – 0,00925 0 0 15 803,6 – 1 257,94 DC950 MaxClimb 12 365,4 – 2,54939 – 0,00911 4,5627E-08 0 DC950 MaxTakeoff 14 698,5 – 2,13511 – 0,00763 3,8212E-08 0 DC95HW General – 13 523,2 – 2,66888 – 0,00925 0 0 15 803,6 – 1 257,94 DC95HW MaxClimb 12 365,4 – 2,54939 – 0,00911 4,5627E-08 0 DC95HW MaxTakeoff 14 698,5 – 2,13511 – 0,00763 3,8212E-08 0 DC9Q7 General – 10 596,5 – 1,51369 – 0,00525 0 0 11 541,7 162,698 DC9Q7 MaxClimb 11 194,3 – 3,0274 – 0,01082 5,4181E-08 0 DC9Q7 MaxTakeoff 12 308,2 – 0,478 0,001708 8,55E-09 0 DC9Q9 General – 13 523,2 – 2,66888 – 0,00925 0 0 15 803,6 – 1 257,94 DC9Q9 MaxClimb 11 561,8 – 2,94773 – 0,01053 5,2756E-08 0 DC9Q9 MaxTakeoff 12 972 – 2,31038 – 0,00826 4,1349E-08 0 DHC8 General 2 010,7 – 19,409 0,07743 0 0 54,6666 – 0,0828 DHC8 MaxClimb 6 323,6 – 21,4445 0,088232 0 01.7.2015 EN Official Journal of the European Union L 168/723 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) DHC8 MaxTakeoff 7 026,2 – 23,8272 0,098036 0 0 DHC830 General 1 623,1 – 18,411 0,075104 0 0 72,6356 – 0,17951 DHC830 MaxClimb 6 679 – 21,9919 0,090305 0 0 DHC830 MaxTakeoff 7 421,1 – 24,4354 0,100339 0 0 DO228 MaxClimb 2 571 – 7,9721 0,07004 – 4,9292E-06 0 DO228 MaxTakeoff 2 524,3 – 8,067 0,06042 – 6,8678E-06 0 DO328 MaxClimb 7 752,5 – 23,2 0,225 – 0,0000158 0 DO328 MaxTakeoff 8 138,2 – 28,1 0,199 – 0,000021 0 ECLIPSE500 MaxClimb 947,7 – 0,73662 0,018307 2,63346E-07 – 0,0571 ECLIPSE500 MaxClimbHi­ 1 077,4 – 1,20966 – 0,00912 1,28125E-07 – 9,84248 Temp ECLIPSE500 MaxTakeoff 1 039,2 – 1,57439 0,034769 – 0,000002274 – 0,0323 ECLIPSE500 MaxTkoffHi­ 1 258,9 – 1,6144 – 0,00748 3,13285E-08 – 10,7499 Temp ECLIPSE500 ReduceClimb 1 084,2 – 1,38862 0,009974 7,08687E-08 0,048579 ECLIPSE500 ReduceClimbHi­ 1 168,6 – 1,50732 – 0,01586 3,07776E-07 – 11,2558 Temp EMB120 MaxClimb 4 668 – 11,932 0,0664 0 – 5,663 EMB120 MaxTakeoff 5 212 – 12,45 0,0728 0 – 6,87 EMB145 MaxClimb 5 554,3 – 6,86092 0,065416 0 – 4,036 EMB145 MaxTakeoff 7 499,5 – 9,12812 0,045563 0 – 22,89 EMB14L MaxClimb 6 432,5 – 7,56929 0,069004 0 – 5,419 EMB14L MaxTakeoff 7 246,1 – 8,61031 0,232825 0 – 0,9689 EMB170 IdleApproach 945 – 3,5 – 0,01 0 0 EMB170 MaxClimb 11 716 – 13,423 0,25 – 0,000019 0L 168/724 EN Official Journal of the European Union 1.7.2015 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) EMB170 MaxTakeoff 13 350 – 17,43 0,1875 – 0,000013 – 4,47 EMB175 IdleApproach 945 – 3,5 – 0,01 0 0 EMB175 MaxClimb 11 716 – 13,423 0,25 – 0,000019 0 EMB175 MaxTakeoff 13 350 – 17,43 0,1875 – 0,000013 – 4,47 EMB190 IdleApproach 1 080 – 3,65 0,011 0 0 EMB190 MaxClimb 15 137 – 14,3 0,239 – 0,0000187 0 EMB190 MaxTakeoff 17 499 – 18,99 0,3207 – 0,000021 – 4,29 EMB195 IdleApproach 1 080 – 3,65 0,011 0 0 EMB195 MaxClimb 15 137 – 14,3 0,239 – 0,0000187 0 EMB195 MaxTakeoff 17 499 – 18,99 0,3207 – 0,000021 – 4,29 F10062 MaxClimb 10 472 – 9,57 0,137 0 0 F10062 MaxTakeoff 13 551 – 16,56 0,2804 0 0 F10065 MaxClimb 10 970 – 10,52 0,1238 0 0 F10065 MaxTakeoff 14 814 – 16,72 0,065 0 0 F28MK2 MaxClimb 8 408 – 4,72 0,1048 0 0 F28MK2 MaxTakeoff 9 851 – 7,68 0,0889 0 0 F28MK4 MaxClimb 8 459 – 4,874 0,0997 0 0 F28MK4 MaxTakeoff 9 905 – 7,445 0,0765 0 0 FAL20 MaxClimb 4 102 – 2,3831 – 0,11465 1,02126E-05 0 FAL20 MaxTakeoff 4 017,4 – 3,4567 0,058024 – 2,49247E-06 0 GII MaxClimb 9 827,9 – 5,89674 – 0,01966 0 0 GII MaxTakeoff 11 324 – 9,697 0,1539 – 0,000004 01.7.2015 EN Official Journal of the European Union L 168/725 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) GII MaxTkoffHi­ 12 833 – 8,35 0,0346 – 0,000004 – 74,58 Temp GII ReduceClimb 6 030 0 – 0,0081 0,0000002 0 GII ReduceTakeoff 9 060 – 7,27 0,121 – 0,000003 0 GII ReduTkoffHi­ 10 266 – 6,25 0,0277 – 0,0000003 – 59,7 Temp GIIB MaxClimb 9 827,9 – 5,89674 – 0,01966 0 0 GIIB MaxTakeoff 11 324 – 9,697 0,1539 – 0,000004 0 GIIB MaxTkoffHi­ 12 833 – 8,35 0,0346 – 0,000004 – 74,58 Temp GIIB ReduceClimb 5 369 0 – 0,0081 0 0 GIIB ReduceTakeoff 9 060 – 7,27 0,121 – 0,000003 0 GIIB ReduTkoffHi­ 10 266 – 6,25 0,0277 – 0,0000003 – 59,7 Temp GIV MaxClimb 10 770 – 10,96 0,1784 – 0,000001 0 GIV MaxClimbHi­ 11 805 – 9,4 – 0,0624 0 – 89 Temp GIV MaxTakeoff 13 725 – 18,2 0,3189 – 0,00002 0 GIV MaxTkoffHi­ 17 129 – 17,6 – 0,0472 0,0000003 – 114 Temp GV MaxClimb 12 400 – 11,6 0,12 0 0 GV MaxClimbHi­ 14 900 – 11,2 – 0,11 0 – 107 Temp GV MaxTakeoff 14 600 – 18,86 0,1649 0 0 GV MaxTkoffHi­ 18 970 – 18,4 – 0,115 0 – 126,5 Temp IA1125 MaxClimb 3 114,4 – 3,4992 0,04125 – 2,81988E-06 0 IA1125 MaxTakeoff 3 460,5 – 3,888 0,045834 – 3,1332E-06 0 L1011 General – 80 222,2 – 25,0263 0 0 0 92 893,5 – 10 186,1L 168/726 EN Official Journal of the European Union 1.7.2015 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) L1011 MaxClimb 34 204,8 – 43,8172 0,270193 2,0153E-06 0 L1011 MaxTakeoff 40 720 – 52,1633 0,321659 2,3992E-06 0 L10115 MaxClimb 39 532,9 – 44,0258 0,27148 2,02494E-06 0 L10115 MaxTakeoff 46 840 – 52,1633 0,321659 2,3992E-06 0 LEAR25 MaxClimb 2 560,9 – 1,8352 – 0,01509 1,95912E-06 0 LEAR25 MaxTakeoff 2 845,4 – 2,03911 – 0,01677 2,1768E-06 0 LEAR35 MaxClimb 3 071 – 3,4992 – 0,00397 1,38915E-06 0 LEAR35 MaxTakeoff 3 412,2 – 3,888 – 0,00441 1,5435E-06 0 MD11GE MaxClimb 47 037 – 45,71 0,854 0 – 368,1 MD11GE MaxTakeoff 57 156 – 42,73 0,303 0 – 357,5 MD11PW MaxClimb 51 197 – 59,27 0,416 0 – 357 MD11PW MaxTakeoff 57 661 – 51,3 0,513 0 – 426,6 MD81 General – 15 384 – 10 0,019 0 0 17 917 0 MD81 MaxClimb 18 040,9 – 8,83022 – 0,02993 0 – 114,3 MD81 MaxClimbHi­ 21 047,1 – 12,8373 – 0,07163 0 – 151,8 Temp MD81 MaxTakeoff 18 810,5 – 11,1271 0,092622 0 – 2,101 MD81 MaxTkoffHi­ 22 678,5 – 14,546 – 0,05823 0 – 138,4 Temp MD82 General – 13 488 – 10 0,025 0 0 16 750 0 MD82 MaxClimb 16 810,1 – 5,36467 0,048334 0 – 60,8 MD82 MaxClimbHi­ 22 606,4 – 13,9975 – 0,09177 0 – 168,1 Temp MD82 MaxTakeoff 19 344,5 – 15,5531 0,333164 0 – 1,031 MD82 MaxTkoffHi­ 24 452 – 16,6869 0,005711 0 – 162,5 Temp1.7.2015 EN Official Journal of the European Union L 168/727 K1 K4 ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/ft) Gb (lb/ft2) H (lb/ °C) K2 (lb/EPR2) K3 (lb/(N1/√θ)) (lb/EPR) (lb/(N1/√θ)2) MD83 General – 13 845 – 13,33 0,019 0 0 17 500 0 MD83 MaxClimb 18 075,2 – 7,63873 0,058915 0 – 64,7 MD83 MaxClimbHi­ 23 181,6 – 13,4908 – 0,09344 0 – 164 Temp MD83 MaxTakeoff 20 080,8 – 11,9047 0,191099 0 – 4,078 MD83 MaxTkoffHi­ 25 460,4 – 15,5681 – 0,05468 0 – 176,1 Temp MD9025 General – 31 899 – 8,5718 – 0,0276 0 0 37 206 0 MD9025 MaxClimb 23 881 – 30,625 0,2551 0 0 MD9025 MaxClimbHi­ 27 078,4 – 30,625 0 0 – 213,2 Temp MD9025 MaxTakeoff 23 066 – 23,5769 0,3147 0 0 MD9025 MaxTkoffHi­ 28 697,1 – 23,5769 0 0 – 225,2 Temp MD9028 General – 31 899 – 8,5718 – 0,0276 0 0 37 206 0 MD9028 MaxClimb 23 421 – 26,5453 0,2599 0 0 MD9028 MaxClimbHi­ 26 678,6 – 26,5453 0 0 – 217,2 Temp MD9028 MaxTakeoff 25 656 – 25,3418 0,2419 0 0 MD9028 MaxTkoffHi­ 30 520 – 25,3418 0 0 – 194,6 Temp MU3001 General 1 743,1 – 1,64678 – 0,00201 – 1,5642E-07 0 – 49,6794 0,545 MU3001 MaxClimb 1 919,5 – 1,99614 0,0615 – 2,40502E-06 0 MU3001 MaxTakeoff 2 132,8 – 2,21793 0,068333 – 2,67224E-06 0 PA42 MaxClimb 2 295,2 – 6,6307 0,041917 5,8567E-07 0 PA42 MaxTakeoff 2 219,6 – 5,9898 0,044468 2,8008E-07 0L 168/728 EN Official Journal of the European Union 1.7.2015 Table I-8 Propeller engine coefficients Installed Net Propulsive Power ACFT_ID Thrust rating Propeller Efficiency (hp) BEC58P MaxClimb 0,90 261,3 BEC58P MaxTakeoff 0,90 310,0 CNA172 MaxClimb 0,69 140,0 CNA172 MaxTakeoff 0,67 155,0 CNA182 MaxClimb 0,78 189,8 CNA182 MaxTakeoff 0,75 222,4 CNA206 MaxClimb 0,77 234,0 CNA206 MaxTakeoff 0,70 300,0 CNA20T MaxClimb 0,77 238,0 CNA20T MaxTakeoff 0,69 310,0 CNA441 MaxClimb 0,90 620,0 CNA441 MaxTakeoff 0,90 635,5 CVR580 MaxClimb 0,85 3 344,0 CVR580 MaxTakeoff 0,85 3 800,0 DC3 MaxClimb 0,85 1 130,0 DC3 MaxTakeoff 0,85 1 302,0 DC6 MaxClimb 0,90 1 750,0 DC6 MaxTakeoff 0,90 1 900,0 DHC6 MaxClimb 0,90 557,5 DHC6 MaxTakeoff 0,90 587,0 DHC6QP MaxClimb 0,90 557,5 DHC6QP MaxTakeoff 0,90 587,0 DHC7 MaxClimb 0,90 846,0 DHC7 MaxTakeoff 0,90 940,0 HS748A MaxClimb 0,90 1 805,0 HS748A MaxTakeoff 0,90 2 006,0 L188 MaxClimb 0,90 3 180,0 L188 MaxTakeoff 0,90 3 460,0 PA30 MaxClimb 0,80 130,5 PA30 MaxTakeoff 0,80 139,5 SD330 MaxClimb 0,90 972,0 SD330 MaxTakeoff 0,90 1 080,0 SF340 MaxClimb 0,90 1 587,0 SF340 MaxTakeoff 0,90 1 763,0Table I-9 Noise power distance data (NPD data) Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) 2CF650 LAmax A 10 000,0 99,2 91,9 86,7 81,0 72,1 63,0 56,7 49,6 41,6 33,1 2CF650 LAmax A 25 000,0 105,3 98,3 93,4 88,0 79,5 70,5 64,3 57,4 49,7 41,5 2CF650 LAmax D 25 000,0 105,3 98,3 93,4 88,0 79,5 70,5 64,3 57,4 49,7 41,5 2CF650 LAmax D 40 000,0 109,1 102,3 97,6 92,5 84,3 75,4 69,3 62,6 55,1 47,2 2CF650 SEL A 10 000,0 99,9 95,0 91,4 87,5 81,3 74,6 69,7 64,2 57,7 50,7 2CF650 SEL A 25 000,0 103,7 99,3 96,1 92,7 87,1 80,6 75,8 70,5 64,3 57,5 2CF650 SEL D 25 000,0 103,7 99,3 96,1 92,7 87,1 80,6 75,8 70,5 64,3 57,5 2CF650 SEL D 40 000,0 106,8 102,9 100,1 97,1 92,0 85,8 81,0 75,9 69,9 63,4 2CF680 LAmax A 7 000,0 96,3 89,8 85,2 80,2 71,9 63,2 56,9 50,8 44,1 37,7 2CF680 LAmax A 12 000,0 97,5 90,9 86,3 81,3 73,0 64,4 58,3 52,3 45,8 39,6 2CF680 LAmax D 17 000,0 98,2 91,5 87,0 82,1 74,2 65,8 59,7 53,6 46,9 40,4 2CF680 LAmax D 25 000,0 98,5 92,6 88,3 83,7 76,4 68,0 62,0 55,6 48,7 41,8 2CF680 LAmax D 33 000,0 101,5 95,8 91,7 87,3 80,2 71,8 65,8 59,4 52,5 45,5 2CF680 LAmax D 41 000,0 104,4 99,0 95,2 91,0 84,1 75,8 69,7 63,2 56,0 48,8 2CF680 SEL A 7 000,0 98,1 93,9 90,8 87,4 81,4 75,0 70,3 65,7 60,6 55,7 2CF680 SEL A 12 000,0 99,3 95,0 91,9 88,5 82,5 76,2 71,7 67,2 62,3 57,6 2CF680 SEL D 17 000,0 100,0 95,6 92,6 89,3 83,7 77,6 73,1 68,5 63,4 58,4 2CF680 SEL D 25 000,0 100,3 96,7 93,9 90,9 85,9 79,8 75,4 70,5 65,2 59,8 2CF680 SEL D 33 000,0 103,3 99,9 97,3 94,5 89,7 83,6 79,2 74,3 69,0 63,5 1.7.2015 EN Official Journal of the European Union L 168/729Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) 2CF680 SEL D 41 000,0 106,2 103,1 100,8 98,2 93,6 87,6 83,1 78,1 72,5 66,8 2CF68D LAmax A 10 020,0 97,7 91,0 85,8 81,1 73,0 64,5 58,5 51,7 44,8 38,3 2CF68D LAmax A 23 190,0 103,3 96,5 91,5 86,5 77,5 68,3 61,7 54,6 47,5 40,4 2CF68D LAmax D 25 940,0 101,9 94,6 89,8 85,0 77,5 68,9 62,6 55,3 47,5 37,2 2CF68D LAmax D 39 180,0 104,2 97,6 93,1 89,0 81,7 73,4 66,8 60,1 52,2 42,2 2CF68D LAmax D 51 530,0 108,4 102,1 97,8 93,5 86,7 78,9 72,8 66,3 58,7 49,2 2CF68D LAmax D 55 500,0 111,4 105,1 100,8 96,5 88,7 82,4 76,3 70,3 62,7 54,0 2CF68D SEL A 10 020,0 99,5 95,1 91,4 88,3 82,5 76,3 71,9 66,6 61,3 56,3 2CF68D SEL A 23 190,0 105,1 100,6 97,1 93,7 87,0 80,1 75,1 69,5 64,0 58,4 2CF68D SEL D 25 940,0 103,7 98,7 95,4 92,2 87,0 80,7 76,0 70,2 64,0 55,2 2CF68D SEL D 39 180,0 106,0 101,7 98,7 96,2 91,2 85,2 80,2 75,0 68,7 60,2 2CF68D SEL D 51 530,0 110,2 106,2 103,4 100,7 96,2 90,7 86,2 81,2 75,2 67,2 2CF68D SEL D 55 500,0 113,2 109,2 106,4 103,7 98,2 94,2 89,7 85,2 79,2 72,0 2J155D LAmax A 500,0 87,0 79,3 74,0 68,2 59,0 49,2 42,4 35,2 27,6 20,0 2J155D LAmax A 1 000,0 92,9 85,4 80,2 74,6 65,6 56,0 49,4 42,4 35,0 27,6 2J155D LAmax D 1 500,0 98,3 90,9 85,7 80,1 71,2 61,7 55,1 48,1 40,7 33,4 2J155D LAmax D 2 400,0 103,2 97,1 92,5 87,5 79,2 70,0 63,4 56,3 48,7 41,1 2J155D LAmax D 2 800,0 107,7 101,4 96,9 91,8 83,5 74,2 67,7 60,6 53,0 45,4 2J155D SEL A 500,0 87,3 81,9 78,1 73,8 66,9 59,3 54,0 48,3 42,3 36,2 2J155D SEL A 1 000,0 93,3 88,1 84,4 80,3 73,6 66,3 61,1 55,6 49,7 43,8 L 168/730 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) 2J155D SEL D 1 500,0 99,5 94,3 90,6 86,5 79,9 72,6 67,5 62,0 56,1 50,3 2J155D SEL D 2 400,0 106,2 102,4 99,3 95,8 89,8 82,8 77,8 72,2 66,1 59,9 2J155D SEL D 2 800,0 109,9 106,0 102,9 99,4 93,3 86,4 81,3 75,7 69,6 63,4 2JT8D LAmax A 3 000,0 102,6 94,6 88,6 82,3 73,8 64,5 58,0 51,0 42,8 34,4 2JT8D LAmax A 6 000,0 105,4 97,9 91,5 85,8 77,2 68,5 61,9 55,1 47,1 38,5 2JT8D LAmax D 8 000,0 108,6 100,7 95,6 89,9 81,8 73,2 66,5 59,9 52,0 43,8 2JT8D LAmax D 10 000,0 111,6 104,3 99,5 94,6 86,3 77,7 71,8 64,9 57,2 48,9 2JT8D LAmax D 12 000,0 115,9 108,9 104,3 99,4 91,1 82,8 76,8 70,1 62,8 54,6 2JT8D LAmax D 14 000,0 120,8 113,4 109,4 104,5 96,4 88,2 82,3 75,8 68,6 60,9 2JT8D SEL A 3 000,0 102,3 97,2 92,9 88,5 82,8 75,6 70,9 65,4 58,8 51,8 2JT8D SEL A 6 000,0 106,1 100,5 96,7 93,0 87,2 80,9 76,1 70,7 64,1 56,9 2JT8D SEL D 8 000,0 108,8 103,9 100,5 96,8 91,5 85,7 80,5 75,1 68,9 62,0 2JT8D SEL D 10 000,0 111,4 107,2 104,3 101,1 95,7 89,5 85,0 79,8 73,5 66,7 2JT8D SEL D 12 000,0 115,1 111,1 108,4 105,5 100,2 94,3 89,9 85,0 78,8 72,1 2JT8D SEL D 14 000,0 119,8 115,9 113,3 110,5 105,4 99,7 95,3 90,3 84,5 78,4 2JT8D2 LAmax A 4 000,0 89,8 82,7 78,0 73,2 65,6 57,3 51,1 44,5 37,7 31,3 2JT8D2 LAmax A 4 667,0 90,8 83,6 79,0 74,2 66,6 58,2 52,0 45,4 38,6 32,2 2JT8D2 LAmax A 5 333,0 91,8 84,6 79,9 75,1 67,5 59,1 52,9 46,3 39,4 33,0 2JT8D2 LAmax A 6 000,0 92,9 85,6 80,9 76,1 68,4 60,0 53,8 47,1 40,3 33,9 2JT8D2 LAmax D 9 000,0 100,6 93,9 89,5 84,8 77,3 69,0 62,9 56,1 49,2 42,5 1.7.2015 EN Official Journal of the European Union L 168/731Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) 2JT8D2 LAmax D 11 000,0 103,0 96,3 91,9 87,2 79,6 71,2 65,0 58,2 51,2 44,4 2JT8D2 LAmax D 13 000,0 105,4 98,7 94,2 89,5 81,8 73,3 67,1 60,2 53,1 46,3 2JT8D2 LAmax D 15 000,0 107,8 101,1 96,6 91,8 84,1 75,5 69,2 62,2 55,1 48,2 2JT8D2 LAmax D 17 000,0 110,2 103,5 99,0 94,2 86,4 77,6 71,3 64,2 57,0 50,1 2JT8D2 LAmax D 19 000,0 112,6 105,9 101,4 96,5 88,6 79,8 73,4 66,2 59,0 52,0 2JT8D2 SEL A 4 000,0 91,5 87,5 84,7 81,9 77,1 71,6 67,2 62,4 57,5 52,9 2JT8D2 SEL A 4 667,0 92,6 88,5 85,8 82,9 78,1 72,6 68,2 63,4 58,5 53,8 2JT8D2 SEL A 5 333,0 93,7 89,6 86,8 83,9 79,1 73,6 69,2 64,4 59,4 54,8 2JT8D2 SEL A 6 000,0 94,7 90,6 87,8 84,9 80,1 74,6 70,2 65,4 60,4 55,7 2JT8D2 SEL D 9 000,0 100,1 96,3 93,7 91,0 86,3 80,8 76,6 71,6 66,5 61,7 2JT8D2 SEL D 11 000,0 102,4 98,7 96,1 93,3 88,6 83,0 78,7 73,7 68,7 63,8 2JT8D2 SEL D 13 000,0 104,8 101,0 98,5 95,6 90,9 85,2 80,9 75,9 70,8 65,9 2JT8D2 SEL D 15 000,0 107,1 103,4 100,8 98,0 93,1 87,4 83,1 78,0 72,9 68,0 2JT8D2 SEL D 17 000,0 109,5 105,7 103,2 100,3 95,4 89,6 85,2 80,2 75,0 70,1 2JT8D2 SEL D 19 000,0 111,8 108,1 105,5 102,7 97,7 91,8 87,4 82,3 77,2 72,2 2JT8DH LAmax A 3 000,0 88,6 83,0 76,9 71,2 62,7 54,1 48,0 41,2 33,4 25,2 2JT8DH LAmax A 6 000,0 93,9 88,7 84,5 79,9 72,5 64,0 57,8 50,8 42,9 34,3 2JT8DH LAmax D 8 000,0 101,1 94,5 90,0 85,2 77,5 68,8 62,5 55,4 47,3 38,7 2JT8DH LAmax D 10 000,0 103,5 96,9 92,5 87,7 79,9 71,2 64,8 57,6 49,6 41,2 2JT8DH LAmax D 12 000,0 108,0 101,4 97,0 92,2 84,5 75,8 69,4 62,4 54,4 45,9 L 168/732 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) 2JT8DH LAmax D 14 000,0 110,7 104,2 99,8 95,1 87,5 79,0 72,8 65,9 58,2 50,0 2JT8DH SEL A 3 000,0 92,6 88,5 85,0 81,2 75,5 69,0 64,1 58,5 51,9 44,9 2JT8DH SEL A 6 000,0 97,9 93,6 90,8 87,9 83,0 76,7 71,7 65,9 59,2 51,8 2JT8DH SEL D 8 000,0 99,5 95,8 93,2 90,3 85,4 79,0 73,8 67,9 61,1 53,6 2JT8DH SEL D 10 000,0 103,6 99,9 97,3 94,4 89,5 83,0 77,8 71,8 65,0 57,7 2JT8DH SEL D 12 000,0 107,2 103,5 100,9 98,0 93,1 86,7 81,5 75,6 68,9 61,5 2JT8DH SEL D 14 000,0 110,8 107,2 104,6 101,8 97,0 90,6 85,6 79,9 73,4 66,4 2JT8DL LAmax A 3 000,0 92,7 85,7 80,8 75,8 67,8 59,0 52,6 45,4 37,2 28,7 2JT8DL LAmax A 6 000,0 96,7 89,9 85,3 80,4 72,4 63,6 57,2 50,0 41,8 33,2 2JT8DL LAmax D 8 000,0 102,0 95,2 90,7 85,8 77,8 69,0 62,6 55,5 47,3 38,7 2JT8DL LAmax D 10 000,0 105,7 98,5 93,9 89,0 81,0 72,2 65,8 58,6 50,6 42,0 2JT8DL LAmax D 12 000,0 109,3 102,5 98,0 93,2 85,3 76,5 70,0 62,9 54,9 46,4 2JT8DL LAmax D 14 000,0 112,5 105,8 101,3 96,4 88,5 79,5 72,9 65,7 57,6 49,1 2JT8DL SEL A 3 000,0 94,7 90,2 87,0 83,7 78,4 71,7 66,5 60,4 53,5 46,1 2JT8DL SEL A 6 000,0 97,9 94,0 91,2 88,2 83,0 76,5 71,2 65,2 58,3 50,8 2JT8DL SEL D 8 000,0 101,2 97,3 94,5 91,5 86,3 79,7 74,5 68,5 61,6 54,1 2JT8DL SEL D 10 000,0 104,6 101,3 98,4 95,3 90,1 83,6 78,3 72,4 65,5 58,1 2JT8DL SEL D 12 000,0 108,1 104,7 101,9 99,0 94,0 87,4 82,1 76,2 69,4 62,1 2JT8DL SEL D 14 000,0 111,7 108,0 105,3 102,4 97,3 90,6 85,3 79,2 72,3 65,0 2JT8DN LAmax A 3 000,0 90,6 84,2 79,7 74,9 67,3 59,2 53,6 47,7 41,5 35,4 1.7.2015 EN Official Journal of the European Union L 168/733Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) 2JT8DN LAmax A 5 000,0 95,8 89,3 84,8 80,0 72,4 64,3 58,8 52,9 46,6 40,5 2JT8DN LAmax D 6 000,0 96,8 90,8 86,5 81,8 74,1 65,8 59,9 53,7 47,0 40,4 2JT8DN LAmax D 8 000,0 101,2 95,2 90,9 86,1 78,5 70,2 64,4 58,2 51,6 45,0 2JT8DN LAmax D 10 000,0 105,1 99,1 94,7 90,0 82,3 73,8 67,9 61,6 54,8 48,0 2JT8DN LAmax D 12 000,0 108,5 102,5 98,1 93,3 85,5 77,0 71,0 64,6 57,8 51,0 2JT8DN LAmax D 14 000,0 111,4 105,4 101,0 96,3 88,5 80,1 74,1 67,8 60,9 54,2 2JT8DN LAmax D 16 000,0 113,8 107,8 103,4 98,7 90,9 82,5 76,5 70,1 63,3 56,6 2JT8DN SEL A 3 000,0 94,0 90,4 87,5 84,2 78,4 71,7 66,7 61,3 55,3 49,3 2JT8DN SEL A 5 000,0 98,5 94,9 92,1 88,8 83,0 76,3 71,4 66,0 60,0 53,9 2JT8DN SEL D 6 000,0 98,6 94,8 92,0 88,8 83,4 77,4 73,0 68,3 63,1 57,9 2JT8DN SEL D 8 000,0 102,7 99,0 96,1 92,9 87,6 81,5 77,2 72,5 67,4 62,3 2JT8DN SEL D 10 000,0 106,6 102,9 100,0 96,8 91,3 85,1 80,7 75,9 70,6 65,3 2JT8DN SEL D 12 000,0 110,2 106,4 103,5 100,2 94,7 88,4 83,9 79,0 73,7 68,3 2JT8DN SEL D 14 000,0 113,1 109,5 106,7 103,5 98,0 91,8 87,3 82,4 77,0 71,6 2JT8DN SEL D 16 000,0 115,9 112,3 109,5 106,3 100,8 94,6 90,1 85,2 79,8 74,4 2JT8DQ LAmax A 3 000,0 94,9 88,2 83,6 78,6 70,8 62,3 56,1 49,2 41,3 32,8 2JT8DQ LAmax A 6 000,0 99,1 92,4 87,8 82,8 75,0 66,5 60,3 53,4 45,5 37,0 2JT8DQ LAmax D 8 000,0 104,1 97,4 92,7 87,8 80,0 71,6 65,5 58,6 50,9 42,6 2JT8DQ LAmax D 10 000,0 109,2 102,5 98,4 92,8 85,2 76,8 70,8 64,1 56,5 48,5 2JT8DQ LAmax D 12 000,0 114,6 107,9 103,3 98,2 90,5 82,3 76,4 69,7 62,4 54,6 L 168/734 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) 2JT8DQ LAmax D 14 000,0 120,1 113,4 108,8 104,0 96,1 87,9 82,1 75,6 68,4 60,9 2JT8DQ SEL A 3 000,0 94,6 90,8 87,9 84,8 79,8 73,4 69,0 63,6 57,2 50,2 2JT8DQ SEL A 6 000,0 99,8 96,0 93,1 90,0 85,0 78,9 74,2 68,8 62,4 55,4 2JT8DQ SEL D 8 000,0 104,3 100,6 97,7 94,7 89,7 83,7 79,1 73,8 67,6 60,8 2JT8DQ SEL D 10 000,0 109,0 105,2 102,5 99,5 94,6 88,6 84,1 79,0 72,9 66,3 2JT8DQ SEL D 12 000,0 113,8 110,1 107,4 104,5 99,6 93,8 89,3 84,2 78,4 72,1 2JT8DQ SEL D 14 000,0 119,1 115,4 112,8 110,0 105,1 99,4 95,0 90,1 84,4 78,4 2JT8DW LAmax A 3 000,0 102,6 94,6 88,6 82,3 73,8 64,5 58,0 51,0 42,8 34,4 2JT8DW LAmax A 6 000,0 105,4 97,9 91,5 85,8 77,2 68,5 61,9 55,1 47,1 38,5 2JT8DW LAmax D 8 000,0 108,6 100,7 95,6 89,9 81,8 73,2 66,5 59,9 52,0 43,8 2JT8DW LAmax D 10 000,0 111,6 104,3 99,5 94,6 86,3 77,7 71,8 64,9 57,2 48,9 2JT8DW LAmax D 12 000,0 115,9 108,9 104,3 99,4 91,1 82,8 76,8 70,1 62,8 54,6 2JT8DW LAmax D 14 000,0 120,8 113,4 109,4 104,5 96,4 88,2 82,3 75,8 68,6 60,9 2JT8DW SEL A 3 000,0 102,3 97,2 92,9 88,5 82,8 75,6 70,9 65,4 58,8 51,8 2JT8DW SEL A 6 000,0 106,1 100,5 96,7 93,0 87,2 80,9 76,1 70,7 64,1 56,9 2JT8DW SEL D 8 000,0 108,8 103,9 100,5 96,8 91,5 85,7 80,5 75,1 68,9 62,0 2JT8DW SEL D 10 000,0 111,4 107,2 104,3 101,1 95,7 89,5 85,0 79,8 73,5 66,7 2JT8DW SEL D 12 000,0 115,1 111,1 108,4 105,5 100,2 94,3 89,9 85,0 78,8 72,1 2JT8DW SEL D 14 000,0 119,8 115,9 113,3 110,5 105,4 99,7 95,3 90,3 84,5 78,4 2JT8QW LAmax A 3 000,0 94,9 88,2 83,6 78,6 70,8 62,3 56,1 49,2 41,3 32,8 1.7.2015 EN Official Journal of the European Union L 168/735Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) 2JT8QW LAmax A 6 000,0 99,1 92,4 87,8 82,8 75,0 66,5 60,3 53,4 45,5 37,0 2JT8QW LAmax D 8 000,0 104,1 97,4 92,7 87,8 80,0 71,6 65,5 58,6 50,9 42,6 2JT8QW LAmax D 10 000,0 109,2 102,5 98,4 92,8 85,2 76,8 70,8 64,1 56,5 48,5 2JT8QW LAmax D 12 000,0 114,6 107,9 103,3 98,2 90,5 82,3 76,4 69,7 62,4 54,6 2JT8QW LAmax D 14 000,0 120,1 113,4 108,8 104,0 96,1 87,9 82,1 75,6 68,4 60,9 2JT8QW SEL A 3 000,0 94,6 90,8 87,9 84,8 79,8 73,4 69,0 63,6 57,2 50,2 2JT8QW SEL A 6 000,0 99,8 96,0 93,1 90,0 85,0 78,9 74,2 68,8 62,4 55,4 2JT8QW SEL D 8 000,0 104,3 100,6 97,7 94,7 89,7 83,7 79,1 73,8 67,6 60,8 2JT8QW SEL D 10 000,0 109,0 105,2 102,5 99,5 94,6 88,6 84,1 79,0 72,9 66,3 2JT8QW SEL D 12 000,0 113,8 110,1 107,4 104,5 99,6 93,8 89,3 84,2 78,4 72,1 2JT8QW SEL D 14 000,0 119,1 115,4 112,8 110,0 105,1 99,4 95,0 90,1 84,4 78,4 2PW535 LAmax A 500,0 89,5 81,8 76,3 70,3 60,6 50,0 42,6 34,6 26,2 17,7 2PW535 LAmax A 700,0 89,6 82,2 76,9 71,1 61,6 51,2 43,9 36,1 28,7 19,5 2PW535 LAmax D 1 200,0 96,1 87,5 81,6 75,4 65,6 55,3 48,3 40,9 33,2 25,6 2PW535 LAmax D 1 600,0 99,2 89,9 83,7 77,2 67,2 57,0 50,2 43,1 35,8 28,8 2PW535 LAmax D 2 000,0 100,7 92,2 86,4 80,3 70,9 61,1 54,4 47,4 40,2 33,1 2PW535 LAmax D 3 000,0 103,5 96,4 91,5 86,1 77,3 67,9 61,3 54,3 46,8 39,4 2PW535 SEL A 500,0 89,4 84,8 81,3 77,4 70,8 63,2 57,8 51,9 45,6 39,1 2PW535 SEL A 700,0 89,3 85,1 81,8 78,1 71,7 64,5 59,3 53,5 47,3 41,0 2PW535 SEL D 1 200,0 90,8 87,1 84,1 80,7 74,7 67,8 62,8 57,2 51,1 44,9 L 168/736 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) 2PW535 SEL D 1 600,0 92,6 89,0 86,2 82,9 77,2 70,6 65,8 60,5 54,7 48,8 2PW535 SEL D 2 000,0 96,0 92,3 89,4 86,1 80,4 73,9 69,2 64,0 58,3 52,6 2PW535 SEL D 3 000,0 102,3 98,9 96,2 93,1 87,7 81,5 77,0 72,0 66,6 61,1 2R2800 LAmax A 30,0 92,6 86,1 81,7 77,0 69,5 61,3 55,5 49,6 43,4 36,6 2R2800 LAmax A 100,0 103,5 97,2 92,9 88,4 81,3 73,6 68,0 61,9 55,3 47,9 2R2800 LAmax D 30,0 92,6 86,1 81,7 77,0 69,5 61,3 55,5 49,6 43,4 36,6 2R2800 LAmax D 100,0 103,5 97,2 92,9 88,4 81,3 73,6 68,0 61,9 55,3 47,9 2R2800 SEL A 30,0 96,9 92,7 89,7 86,5 81,3 75,3 71,0 66,6 61,9 56,6 2R2800 SEL A 100,0 107,5 103,0 99,9 96,6 91,3 85,4 81,0 76,2 70,7 64,5 2R2800 SEL D 30,0 96,9 92,7 89,7 86,5 81,3 75,3 71,0 66,6 61,9 56,6 2R2800 SEL D 100,0 107,5 103,0 99,9 96,6 91,3 85,4 81,0 76,2 70,7 64,5 3JT8D LAmax A 3 000,0 104,6 96,6 90,6 84,3 75,8 66,5 60,0 53,0 44,8 36,4 3JT8D LAmax A 6 000,0 107,4 98,9 93,5 87,8 79,2 70,5 63,9 57,1 49,1 40,5 3JT8D LAmax D 8 000,0 110,6 102,7 97,6 91,9 83,8 75,2 68,5 61,9 54,0 45,8 3JT8D LAmax D 10 000,0 113,6 106,3 101,5 96,6 88,3 79,7 73,8 66,9 59,2 50,9 3JT8D LAmax D 12 000,0 117,9 110,9 106,3 101,4 93,1 84,8 78,8 72,1 64,8 56,6 3JT8D LAmax D 14 000,0 122,8 115,4 111,4 106,5 98,4 90,2 84,3 77,8 70,6 62,8 3JT8D SEL A 3 000,0 104,3 99,2 94,9 90,5 84,8 77,6 72,9 67,4 60,8 53,8 3JT8D SEL A 6 000,0 108,1 102,5 98,7 95,0 89,2 82,9 78,1 72,7 66,1 58,9 3JT8D SEL D 8 000,0 110,8 105,9 102,5 98,8 93,5 87,7 82,5 77,1 70,9 64,0 1.7.2015 EN Official Journal of the European Union L 168/737Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) 3JT8D SEL D 10 000,0 113,4 109,2 106,3 103,1 97,7 91,5 87,0 81,8 75,5 68,7 3JT8D SEL D 12 000,0 117,1 113,1 110,4 107,5 102,2 96,3 91,9 87,0 80,8 74,1 3JT8D SEL D 14 000,0 121,8 117,9 115,3 112,5 107,4 101,7 97,3 92,3 86,5 80,4 3JT8DQ LAmax A 3 000,0 96,9 90,2 85,6 80,6 72,8 64,3 58,1 51,2 43,3 34,8 3JT8DQ LAmax A 6 000,0 101,1 94,4 89,8 84,8 77,0 68,5 62,3 55,4 47,5 39,0 3JT8DQ LAmax D 8 000,0 106,1 99,4 94,8 89,8 82,0 73,6 67,5 60,6 52,9 44,6 3JT8DQ LAmax D 10 000,0 111,2 104,5 99,9 95,0 87,2 78,8 72,8 66,1 58,5 50,5 3JT8DQ LAmax D 12 000,0 116,6 109,9 105,3 100,4 92,5 84,3 78,4 71,7 64,4 56,6 3JT8DQ LAmax D 14 000,0 122,1 115,4 110,8 106,0 98,1 89,9 84,1 77,6 70,4 62,9 3JT8DQ SEL A 3 000,0 96,6 92,8 89,8 86,8 81,8 75,4 71,0 65,6 59,2 52,2 3JT8DQ SEL A 6 000,0 101,8 98,0 95,1 92,0 87,0 80,9 76,2 70,8 64,4 57,4 3JT8DQ SEL D 8 000,0 106,3 102,6 99,7 96,7 91,7 85,7 81,1 75,8 69,6 62,8 3JT8DQ SEL D 10 000,0 111,0 107,2 104,5 101,5 96,6 90,6 86,1 81,0 74,9 68,3 3JT8DQ SEL D 12 000,0 115,8 112,1 109,4 106,5 101,6 95,8 91,3 86,2 80,4 74,1 3JT8DQ SEL D 14 000,0 121,1 117,4 114,8 112,0 107,1 101,4 97,0 92,1 86,4 80,4 3JT8E5 LAmax A 3 000,0 96,4 89,3 84,5 79,3 71,3 62,6 56,1 49,0 41,0 32,0 3JT8E5 LAmax A 5 000,0 98,0 91,3 86,7 81,8 74,0 65,4 59,1 52,2 44,3 35,6 3JT8E5 LAmax D 7 000,0 104,7 97,8 93,0 87,8 79,5 70,3 63,4 55,8 47,3 38,0 3JT8E5 LAmax D 10 000,0 109,2 102,3 97,5 92,4 84,2 75,1 68,4 61,3 53,3 44,7 3JT8E5 LAmax D 12 000,0 112,1 105,3 100,6 95,6 87,7 79,3 73,2 66,7 59,5 51,5 L 168/738 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) 3JT8E5 LAmax D 14 000,0 115,5 108,7 104,1 99,1 91,4 83,1 77,1 70,9 63,9 56,2 3JT8E5 SEL A 3 000,0 98,2 93,4 90,1 86,5 80,8 74,4 69,5 63,9 57,5 50,0 3JT8E5 SEL A 5 000,0 99,8 95,4 92,3 89,0 83,5 77,2 72,5 67,1 60,8 53,6 3JT8E5 SEL D 7 000,0 106,5 101,9 98,6 95,0 89,0 82,1 76,8 70,7 63,8 56,0 3JT8E5 SEL D 10 000,0 111,0 106,4 103,1 99,6 93,7 86,9 81,8 76,2 69,8 62,7 3JT8E5 SEL D 12 000,0 113,9 109,4 106,2 102,8 97,2 91,1 86,6 81,6 76,0 69,5 3JT8E5 SEL D 14 000,0 117,3 112,8 109,7 106,3 100,9 94,9 90,5 85,8 80,4 74,2 3JT8E7 LAmax A 3 000,0 95,1 88,3 84,0 78,3 70,1 61,1 54,4 47,2 39,2 30,4 3JT8E7 LAmax A 5 000,0 98,1 91,3 86,5 81,3 73,1 64,1 57,4 50,2 42,2 33,4 3JT8E7 LAmax D 7 000,0 103,9 97,0 92,2 87,0 78,7 69,5 62,6 55,0 46,5 37,2 3JT8E7 LAmax D 10 000,0 109,1 102,2 97,4 92,2 83,9 74,7 68,0 60,8 52,9 44,0 3JT8E7 LAmax D 12 000,0 111,9 105,2 100,4 95,4 87,4 78,6 72,1 65,1 57,0 47,9 3JT8E7 LAmax D 14 000,0 114,6 107,9 103,2 98,2 90,3 81,7 75,2 68,3 60,5 51,7 3JT8E7 SEL A 3 000,0 96,9 92,4 89,6 85,5 79,6 72,9 67,8 62,1 55,7 48,4 3JT8E7 SEL A 5 000,0 99,9 95,4 92,1 88,5 82,6 75,9 70,8 65,1 58,7 51,4 3JT8E7 SEL D 7 000,0 105,7 101,1 97,8 94,2 88,2 81,3 76,0 69,9 63,0 55,2 3JT8E7 SEL D 10 000,0 110,9 106,3 103,0 99,4 93,4 86,5 81,4 75,7 69,4 62,0 3JT8E7 SEL D 12 000,0 113,7 109,3 106,0 102,6 96,9 90,4 85,5 80,0 73,5 65,9 3JT8E7 SEL D 14 000,0 116,4 112,0 108,8 105,4 99,8 93,5 88,6 83,2 77,0 69,7 4R2800 LAmax A 30,0 95,6 89,1 84,7 80,0 72,5 64,3 58,5 52,6 46,4 39,6 1.7.2015 EN Official Journal of the European Union L 168/739Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) 4R2800 LAmax A 100,0 106,5 100,2 95,9 91,4 84,3 76,6 71,0 64,9 58,3 50,9 4R2800 LAmax D 30,0 95,6 89,1 84,7 80,0 72,5 64,3 58,5 52,6 46,4 39,6 4R2800 LAmax D 100,0 106,5 100,2 95,9 91,4 84,3 76,6 71,0 64,9 58,3 50,9 4R2800 SEL A 30,0 99,9 95,7 92,7 89,5 84,3 78,3 74,0 69,6 64,9 59,6 4R2800 SEL A 100,0 110,5 106,0 102,9 99,6 94,3 88,4 84,0 79,2 73,7 67,5 4R2800 SEL D 30,0 99,9 95,7 92,7 89,5 84,3 78,3 74,0 69,6 64,9 59,6 4R2800 SEL D 100,0 110,5 106,0 102,9 99,6 94,3 88,4 84,0 79,2 73,7 67,5 501D13 LAmax A 30,0 93,0 86,4 81,8 76,9 68,9 59,4 52,0 44,0 36,2 28,6 501D13 LAmax A 100,0 96,8 90,3 85,9 81,3 74,3 67,0 62,1 57,0 51,5 45,4 501D13 LAmax D 30,0 93,0 86,4 81,8 76,9 68,9 59,4 52,0 44,0 36,2 28,6 501D13 LAmax D 100,0 96,8 90,3 85,9 81,3 74,3 67,0 62,1 57,0 51,5 45,4 501D13 SEL A 30,0 95,0 90,7 87,6 84,2 78,4 71,2 65,3 58,8 52,5 46,4 501D13 SEL A 100,0 97,1 92,8 89,9 86,8 82,0 77,0 73,6 69,9 66,0 61,4 501D13 SEL D 30,0 95,0 90,7 87,6 84,2 78,4 71,2 65,3 58,8 52,5 46,4 501D13 SEL D 100,0 97,1 92,8 89,9 86,8 82,0 77,0 73,6 69,9 66,0 61,4 A310 LAmax A 3 000,0 92,2 86,2 81,7 77,0 69,2 60,4 54,0 47,1 39,4 31,4 A310 LAmax A 12 000,0 95,5 89,4 84,4 79,2 70,8 61,9 55,6 48,6 40,8 32,6 A310 LAmax D 20 000,0 101,6 93,8 88,6 82,7 73,0 63,1 56,1 48,3 40,1 31,8 A310 LAmax D 30 000,0 103,4 95,3 89,9 84,2 75,4 66,1 59,6 52,5 44,5 36,1 A310 LAmax D 40 000,0 104,4 96,9 91,9 86,6 78,3 69,2 62,7 55,7 48,0 39,7 L 168/740 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) A310 LAmax D 50 000,0 108,8 101,6 96,7 91,5 83,0 73,7 67,7 61,0 53,3 44,8 A310 SEL A 3 000,0 97,5 93,3 90,1 87,0 81,6 75,7 71,2 66,4 60,0 51,9 A310 SEL A 12 000,0 98,9 94,5 91,3 88,0 82,6 76,4 71,8 66,4 60,5 52,3 A310 SEL D 20 000,0 102,7 98,3 94,5 90,5 83,8 76,5 71,6 66,1 59,5 52,7 A310 SEL D 30 000,0 103,7 99,2 95,8 92,3 86,7 80,4 75,8 70,4 64,3 57,6 A310 SEL D 40 000,0 104,5 100,4 97,6 94,4 89,2 83,4 79,0 73,9 68,0 61,4 A310 SEL D 50 000,0 108,0 103,9 101,2 98,2 93,3 87,8 83,6 78,6 72,9 66,4 AE3007 LAmax A 2 000,0 85,5 78,7 74,2 69,3 61,5 52,7 46,4 39,3 31,2 22,7 AE3007 LAmax A 3 000,0 90,4 83,5 78,7 73,5 65,5 56,8 50,6 43,6 35,4 26,9 AE3007 LAmax D 4 000,0 90,8 84,3 79,8 75,1 67,5 58,9 52,6 45,5 37,4 28,6 AE3007 LAmax D 5 000,0 93,0 86,6 82,1 77,4 69,8 61,2 54,9 47,8 39,8 31,3 AE3007 LAmax D 6 000,0 96,0 89,5 85,0 80,3 72,6 64,0 57,7 50,6 42,5 34,0 AE3007 SEL A 2 000,0 89,8 85,6 82,7 79,5 74,1 67,8 63,2 57,7 51,4 44,3 AE3007 SEL A 3 000,0 92,7 88,6 85,6 82,3 77,0 70,9 66,3 61,0 54,8 47,9 AE3007 SEL D 4 000,0 91,7 88,1 85,4 82,5 77,7 72,0 67,6 62,4 56,1 49,1 AE3007 SEL D 5 000,0 93,6 90,0 87,4 84,6 79,8 74,2 69,9 64,8 58,7 51,9 AE3007 SEL D 6 000,0 96,7 93,0 90,3 87,5 82,8 77,2 72,8 67,7 61,6 54,9 AE300C LAmax A 1 100,0 88,6 80,4 74,8 69,0 59,9 50,4 44,0 37,0 30,4 23,6 AE300C LAmax A 1 400,0 88,6 80,4 74,8 69,0 59,9 50,4 44,0 37,0 30,4 23,6 AE300C LAmax A 1 900,0 88,6 80,7 75,3 69,5 60,6 51,3 44,9 38,1 31,3 24,5 1.7.2015 EN Official Journal of the European Union L 168/741Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) AE300C LAmax D 3 500,0 90,6 83,5 78,4 73,1 64,4 55,2 48,7 42,0 34,7 27,5 AE300C LAmax D 4 500,0 92,7 85,7 80,7 75,5 67,1 58,1 51,9 45,2 38,3 31,4 AE300C LAmax D 5 500,0 94,7 88,0 83,3 78,2 69,9 60,9 54,7 47,9 40,9 33,9 AE300C SEL A 1 100,0 91,1 86,1 82,6 78,7 72,5 65,8 61,1 56,0 50,8 45,5 AE300C SEL A 1 400,0 91,1 86,1 82,6 78,7 72,5 65,8 61,1 56,0 50,8 45,5 AE300C SEL A 1 900,0 92,5 87,1 83,3 79,4 73,1 66,4 61,8 56,7 51,8 46,8 AE300C SEL D 3 500,0 92,9 88,2 84,7 80,8 74,4 67,2 62,1 56,7 50,6 44,6 AE300C SEL D 4 500,0 95,2 90,4 87,0 83,2 77,1 70,4 65,7 60,6 55,2 49,8 AE300C SEL D 5 500,0 96,6 92,4 89,3 85,7 79,7 72,9 68,0 62,7 57,0 51,2 AL502L LAmax A 1 900,0 88,4 81,5 76,6 71,3 62,7 53,2 46,4 39,1 31,4 23,2 AL502L LAmax A 5 000,0 98,0 91,5 86,9 82,2 74,4 65,8 59,4 52,6 45,1 36,8 AL502L LAmax D 1 900,0 88,4 81,5 76,6 71,3 62,7 53,2 46,4 39,1 31,4 23,2 AL502L LAmax D 5 000,0 98,0 91,5 86,9 82,2 74,4 65,8 59,4 52,6 45,1 36,8 AL502L SEL A 1 900,0 90,2 85,5 82,1 78,3 72,0 64,7 59,4 53,6 47,4 40,7 AL502L SEL A 5 000,0 101,1 96,8 93,8 90,5 85,0 78,6 73,8 68,4 62,5 55,6 AL502L SEL D 1 900,0 90,2 85,5 82,1 78,3 72,0 64,7 59,4 53,6 47,4 40,7 AL502L SEL D 5 000,0 101,1 96,8 93,8 90,5 85,0 78,6 73,8 68,4 62,5 55,6 AL502R LAmax A 1 600,0 91,2 84,5 79,7 74,5 66,3 57,0 50,1 42,3 33,7 25,0 AL502R LAmax A 5 200,0 101,6 94,8 89,8 84,6 76,3 67,5 61,2 54,3 47,0 39,7 AL502R LAmax D 1 600,0 91,2 84,5 79,7 74,5 66,3 57,0 50,1 42,3 33,7 25,0 L 168/742 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) AL502R LAmax D 5 200,0 101,6 94,8 89,8 84,6 76,3 67,5 61,2 54,3 47,0 39,7 AL502R SEL A 1 600,0 92,9 89,0 86,0 82,7 77,3 70,4 65,0 58,7 51,6 44,3 AL502R SEL A 5 200,0 102,3 98,4 95,4 92,1 86,8 80,4 75,6 70,3 64,4 58,7 AL502R SEL D 1 600,0 92,9 89,0 86,0 82,7 77,3 70,4 65,0 58,7 51,6 44,3 AL502R SEL D 5 200,0 102,3 98,4 95,4 92,1 86,8 80,4 75,6 70,3 64,4 58,7 BR710 LAmax A 1 830,0 87,7 80,6 75,8 70,7 62,6 54,0 47,8 41,1 33,7 26,0 BR710 LAmax A 2 000,0 87,9 80,7 75,9 70,7 62,7 54,0 47,9 41,2 33,7 25,9 BR710 LAmax A 3 000,0 88,9 81,7 76,7 71,5 63,4 54,8 48,6 41,7 34,1 26,1 BR710 LAmax A 4 000,0 90,1 82,9 77,9 72,7 64,6 55,9 49,7 42,8 35,1 27,1 BR710 LAmax A 5 000,0 92,5 85,3 80,4 75,0 66,6 57,6 51,1 44,0 35,9 27,5 BR710 LAmax A 6 000,0 94,7 87,7 82,7 77,3 68,8 59,8 53,3 46,0 37,9 29,3 BR710 LAmax A 7 000,0 96,7 89,7 84,7 79,3 70,9 61,8 55,2 47,9 39,7 31,1 BR710 LAmax A 8 000,0 98,4 91,5 86,5 81,1 72,7 63,6 57,1 49,8 41,6 32,9 BR710 LAmax A 9 000,0 99,9 93,0 88,0 82,7 74,4 65,3 58,8 51,5 43,3 34,7 BR710 LAmax A 10 000,0 101,0 94,1 89,3 84,0 75,8 66,8 60,4 53,2 45,0 36,5 BR710 LAmax A 11 000,0 101,6 95,0 90,2 85,1 77,0 68,2 61,8 54,7 46,7 38,3 BR710 LAmax A 12 000,0 102,6 95,6 90,9 85,9 78,0 69,3 63,1 56,1 48,3 40,1 BR710 LAmax A 12 900,0 102,9 95,9 91,3 86,4 78,7 70,3 64,1 57,3 49,7 41,7 BR710 LAmax D 4 000,0 90,0 82,7 77,7 72,5 64,1 55,2 48,9 41,8 33,9 25,7 BR710 LAmax D 5 000,0 92,5 85,3 80,4 75,0 66,6 57,6 51,1 44,0 35,9 27,5 1.7.2015 EN Official Journal of the European Union L 168/743Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) BR710 LAmax D 6 000,0 94,7 87,7 82,7 77,3 68,8 59,8 53,3 46,0 37,9 29,3 BR710 LAmax D 7 000,0 96,7 89,7 84,7 79,3 70,9 61,8 55,2 47,9 39,7 31,1 BR710 LAmax D 8 000,0 98,4 91,5 86,5 81,1 72,7 63,6 57,1 49,8 41,6 32,9 BR710 LAmax D 9 000,0 99,9 93,0 88,0 82,7 74,4 65,3 58,8 51,5 43,3 34,7 BR710 LAmax D 10 000,0 101,0 94,1 89,3 84,0 75,8 66,8 60,4 53,2 45,0 36,5 BR710 LAmax D 11 000,0 101,6 95,0 90,2 85,1 77,0 68,2 61,8 54,7 46,7 38,3 BR710 LAmax D 12 000,0 102,6 95,6 90,9 85,9 78,0 69,3 63,1 56,1 48,3 40,1 BR710 LAmax D 12 900,0 102,9 95,9 91,3 86,4 78,7 70,3 64,1 57,3 49,7 41,7 BR710 SEL A 1 830,0 90,3 85,8 82,8 79,6 74,3 68,3 63,8 58,7 53,0 46,8 BR710 SEL A 2 000,0 90,3 85,9 82,9 79,7 74,4 68,4 63,9 58,8 53,0 46,8 BR710 SEL A 3 000,0 91,0 86,6 83,6 80,3 75,0 69,1 64,6 59,5 53,6 47,2 BR710 SEL A 4 000,0 92,2 87,6 84,5 81,2 76,0 70,1 65,7 60,6 54,7 48,2 BR710 SEL A 5 000,0 92,7 88,5 85,6 82,3 76,9 70,8 66,3 61,1 54,9 48,1 BR710 SEL A 6 000,0 94,7 90,5 87,6 84,2 78,8 72,7 68,1 62,9 56,7 49,9 BR710 SEL A 7 000,0 96,5 92,4 89,4 86,1 80,6 74,5 69,9 64,7 58,5 51,7 BR710 SEL A 8 000,0 98,1 94,1 91,1 87,8 82,3 76,2 71,7 66,4 60,3 53,5 BR710 SEL A 9 000,0 99,6 95,6 92,6 89,4 83,9 77,9 73,4 68,1 62,0 55,3 BR710 SEL A 10 000,0 100,9 96,9 94,0 90,8 85,5 79,5 75,0 69,8 63,8 57,1 BR710 SEL A 11 000,0 102,1 98,1 95,3 92,2 86,9 81,0 76,6 71,5 65,5 58,9 BR710 SEL A 12 000,0 103,1 99,1 96,4 93,4 88,3 82,5 78,1 73,1 67,2 60,7 L 168/744 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) BR710 SEL A 12 900,0 103,8 99,9 97,3 94,4 89,5 83,8 79,5 74,5 68,7 62,3 BR710 SEL D 4 000,0 90,5 86,4 83,5 80,2 74,9 68,9 64,4 59,2 53,0 46,2 BR710 SEL D 5 000,0 92,7 88,5 85,6 82,3 76,9 70,8 66,3 61,1 54,9 48,1 BR710 SEL D 6 000,0 94,7 90,5 87,6 84,2 78,8 72,7 68,1 62,9 56,7 49,9 BR710 SEL D 7 000,0 96,5 92,4 89,4 86,1 80,6 74,5 69,9 64,7 58,5 51,7 BR710 SEL D 8 000,0 98,1 94,1 91,1 87,8 82,3 76,2 71,7 66,4 60,3 53,5 BR710 SEL D 9 000,0 99,6 95,6 92,6 89,4 83,9 77,9 73,4 68,1 62,0 55,3 BR710 SEL D 10 000,0 100,9 96,9 94,0 90,8 85,5 79,5 75,0 69,8 63,8 57,1 BR710 SEL D 11 000,0 102,1 98,1 95,3 92,2 86,9 81,0 76,6 71,5 65,5 58,9 BR710 SEL D 12 000,0 103,1 99,1 96,4 93,4 88,3 82,5 78,1 73,1 67,2 60,7 BR710 SEL D 12 900,0 103,8 99,9 97,3 94,4 89,5 83,8 79,5 74,5 68,7 62,3 BR715 LAmax A 4 250,0 89,2 81,6 76,8 71,6 63,4 54,6 48,3 41,6 34,7 28,2 BR715 LAmax A 5 000,0 89,6 82,4 77,5 72,4 64,2 55,4 49,1 42,3 35,5 28,9 BR715 LAmax A 5 750,0 89,9 83,0 78,2 73,0 64,9 56,1 49,7 43,0 36,1 29,6 BR715 LAmax A 9 875,0 93,8 87,0 82,4 77,6 69,8 61,4 55,3 48,6 41,8 35,3 BR715 LAmax D 11 000,0 95,7 88,9 84,3 79,5 71,7 63,1 57,0 50,2 43,4 36,9 BR715 LAmax D 13 000,0 98,6 91,9 87,3 82,5 74,6 66,0 59,8 52,9 46,0 39,4 BR715 LAmax D 15 000,0 101,2 94,5 90,0 85,1 77,2 68,5 62,2 55,3 48,3 41,6 BR715 LAmax D 17 000,0 103,5 97,0 92,4 87,5 79,6 70,7 64,4 57,4 50,4 43,7 BR715 LAmax D 19 000,0 106,4 99,9 95,3 90,4 82,4 73,4 67,0 60,0 52,9 46,2 1.7.2015 EN Official Journal of the European Union L 168/745Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) BR715 LAmax D 19 750,0 107,5 101,0 96,5 91,6 83,5 74,5 68,1 61,1 53,9 47,2 BR715 SEL A 4 250,0 91,9 87,1 84,1 80,7 75,2 69,0 64,4 59,4 54,2 49,4 BR715 SEL A 5 000,0 92,2 88,0 84,9 81,5 76,1 69,9 65,3 60,3 55,2 50,3 BR715 SEL A 5 750,0 92,5 88,6 85,6 82,2 76,8 70,6 66,0 61,0 55,9 51,1 BR715 SEL A 9 875,0 95,7 91,5 88,7 85,6 80,5 74,8 70,5 65,6 60,7 56,0 BR715 SEL D 11 000,0 97,3 93,1 90,3 87,2 82,1 76,4 72,1 67,2 62,3 57,6 BR715 SEL D 13 000,0 99,8 95,7 92,9 89,8 84,7 78,9 74,7 69,8 64,9 60,2 BR715 SEL D 15 000,0 102,1 98,0 95,2 92,1 87,0 81,2 77,0 72,1 67,2 62,5 BR715 SEL D 17 000,0 104,1 100,1 97,3 94,2 89,1 83,3 79,0 74,2 69,2 64,6 BR715 SEL D 19 000,0 106,6 102,7 99,8 96,7 91,6 85,8 81,5 76,7 71,8 67,2 BR715 SEL D 19 750,0 107,6 103,7 100,8 97,7 92,6 86,8 82,5 77,7 72,8 68,2 CF34 LAmax A 2 000,0 87,3 80,7 76,0 71,1 63,0 54,1 47,6 40,6 33,0 24,6 CF34 LAmax A 3 000,0 90,6 83,8 79,0 73,9 65,6 56,5 49,8 42,7 34,9 26,5 CF34 LAmax D 4 000,0 93,1 86,3 81,5 76,5 68,4 59,6 53,1 46,0 38,2 29,6 CF34 LAmax D 5 000,0 95,0 88,2 83,5 78,6 70,6 61,9 55,6 48,7 40,9 32,3 CF34 LAmax D 6 000,0 97,2 90,9 86,1 81,2 73,2 64,5 58,2 51,5 43,5 34,9 CF34 SEL A 2 000,0 90,9 86,7 83,3 79,9 74,1 67,4 62,4 56,9 50,7 43,9 CF34 SEL A 3 000,0 94,3 89,8 86,5 82,9 76,9 70,0 64,8 59,2 52,9 46,0 CF34 SEL D 4 000,0 96,3 91,8 88,5 85,0 79,1 72,5 67,5 61,9 55,6 48,6 CF34 SEL D 5 000,0 97,7 93,2 90,0 86,5 80,8 74,3 69,5 64,1 57,9 50,7 L 168/746 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) CF34 SEL D 6 000,0 99,7 95,2 92,0 88,5 82,8 76,3 71,5 66,1 59,9 52,7 CF3410E LAmax A 3 000,0 90,1 83,6 79,1 74,4 66,9 58,6 52,6 45,7 37,9 29,5 CF3410E LAmax A 5 000,0 91,9 85,3 80,7 75,9 68,3 59,9 53,9 47,2 39,6 31,4 CF3410E LAmax D 8 000,0 94,9 88,5 84,0 79,3 71,9 63,7 57,7 51,0 43,3 34,8 CF3410E LAmax D 10 000,0 97,6 91,1 86,6 81,9 74,3 66,0 60,2 53,4 45,6 37,1 CF3410E LAmax D 15 000,0 103,3 96,8 92,3 87,5 79,8 71,3 65,1 58,3 50,4 42,0 CF3410E SEL A 3 000,0 92,5 88,8 86,1 83,2 78,4 72,7 68,3 63,3 57,2 50,5 CF3410E SEL A 5 000,0 93,9 90,1 87,4 84,4 79,5 73,9 69,6 64,7 58,9 52,4 CF3410E SEL D 8 000,0 95,9 92,2 89,6 86,7 81,8 76,3 72,1 67,1 61,2 54,5 CF3410E SEL D 10 000,0 98,6 94,9 92,1 89,2 84,4 78,8 74,6 69,9 63,9 57,2 CF3410E SEL D 15 000,0 103,8 100,2 97,5 94,6 89,8 84,1 79,9 74,9 69,1 62,6 CF348C5 LAmax A 2 500,0 89,7 83,1 78,6 73,8 66,2 57,6 51,3 44,1 36,0 27,3 CF348C5 LAmax A 7 250,0 91,3 84,7 80,2 75,4 67,6 58,9 52,6 45,5 37,6 29,2 CF348C5 LAmax D 7 250,0 94,5 87,9 83,5 78,7 71,0 62,3 56,0 48,8 40,5 31,7 CF348C5 LAmax D 16 250,0 103,6 97,1 92,6 87,9 80,2 71,6 65,3 58,3 50,3 42,0 CF348C5 SEL A 2 500,0 93,1 89,2 86,4 83,3 78,2 72,0 67,1 61,5 54,9 47,7 CF348C5 SEL A 7 250,0 95,2 91,0 88,1 85,0 79,8 73,6 68,8 63,2 56,8 49,9 CF348C5 SEL D 7 250,0 96,4 92,3 89,5 86,5 81,5 75,3 70,4 64,7 58,0 50,6 CF348C5 SEL D 16 250,0 104,7 100,9 98,2 95,3 90,4 84,4 79,6 74,0 67,6 60,7 CF348E LAmax A 3 000,0 91,1 84,4 79,8 74,8 66,8 57,8 51,3 44,0 35,9 27,5 1.7.2015 EN Official Journal of the European Union L 168/747Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) CF348E LAmax A 4 000,0 92,0 85,3 80,7 75,8 67,8 59,0 52,5 45,5 37,6 29,6 CF348E LAmax D 7 000,0 95,5 88,9 84,3 79,4 71,5 62,8 56,5 49,5 41,6 33,5 CF348E LAmax D 9 000,0 99,3 92,7 88,2 83,4 75,5 66,8 60,6 53,7 46,0 38,0 CF348E LAmax D 11 000,0 103,3 96,6 92,0 87,1 79,2 70,3 64,0 57,2 49,6 41,8 CF348E SEL A 3 000,0 93,5 89,6 86,7 83,5 78,2 72,0 67,2 61,6 55,3 48,6 CF348E SEL A 4 000,0 94,7 90,7 87,9 84,7 79,4 73,3 68,7 63,3 57,2 50,7 CF348E SEL D 7 000,0 97,3 93,2 90,5 87,4 82,3 76,2 71,7 66,4 60,4 54,0 CF348E SEL D 9 000,0 100,3 96,5 93,9 91,0 86,0 80,3 75,9 70,9 65,0 58,6 CF348E SEL D 11 000,0 103,4 99,7 97,1 94,2 89,4 83,8 79,5 74,6 68,9 62,5 CF565C LAmax A 3 000,0 93,3 86,6 82,1 77,3 69,7 61,5 55,6 48,9 41,5 33,6 CF565C LAmax A 5 000,0 94,2 87,3 82,5 77,6 69,9 61,6 55,6 49,0 41,5 33,6 CF565C LAmax D 12 500,0 98,9 89,4 82,8 76,4 67,3 57,8 51,3 44,2 36,3 27,7 CF565C LAmax D 20 000,0 103,4 95,3 89,8 83,9 75,3 66,2 59,9 53,0 45,0 36,3 CF565C LAmax D 27 500,0 106,9 99,4 94,4 89,3 81,0 71,9 65,4 58,3 50,2 41,5 CF565C SEL A 3 000,0 98,7 92,8 89,9 86,8 81,7 76,0 71,7 66,6 60,8 54,3 CF565C SEL A 5 000,0 99,0 93,3 90,1 86,9 81,9 76,1 71,8 66,7 60,9 54,3 CF565C SEL D 12 500,0 98,8 92,6 88,7 84,8 78,6 71,9 67,1 61,6 55,4 48,5 CF565C SEL D 20 000,0 105,3 99,9 96,4 92,9 87,3 81,0 76,4 70,9 64,7 57,8 CF565C SEL D 27 500,0 108,0 103,5 100,5 97,4 92,1 86,2 81,7 76,2 70,7 64,6 CF567B LAmax A 3 000,0 93,0 85,9 81,1 76,1 68,0 59,2 52,5 45,6 37,5 29,3 L 168/748 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) CF567B LAmax A 4 000,0 93,6 86,5 81,7 76,6 68,7 59,9 53,4 46,6 37,8 29,7 CF567B LAmax A 5 000,0 94,1 87,0 82,2 77,2 69,2 60,5 54,1 47,4 39,0 31,1 CF567B LAmax A 6 000,0 94,6 87,5 82,7 77,6 69,7 61,1 54,7 48,1 40,4 32,9 CF567B LAmax A 7 000,0 95,0 87,9 83,0 78,0 70,1 61,5 55,2 48,7 41,8 34,5 CF567B LAmax D 10 000,0 95,2 87,9 83,6 78,8 71,3 63,0 57,3 50,4 44,2 36,9 CF567B LAmax D 13 000,0 98,1 91,0 86,7 82,0 74,5 66,3 60,7 53,9 46,9 39,6 CF567B LAmax D 16 000,0 100,5 93,7 89,3 84,6 77,3 69,2 63,5 56,8 49,4 42,1 CF567B LAmax D 19 000,0 102,7 96,0 91,7 87,1 79,7 71,7 66,1 59,5 52,2 44,9 CF567B LAmax D 23 500,0 107,2 100,9 96,5 91,9 84,7 76,8 71,4 64,6 57,7 50,4 CF567B SEL A 3 000,0 95,5 91,3 88,2 84,9 79,5 73,3 68,3 63,2 55,9 49,6 CF567B SEL A 4 000,0 96,2 91,9 88,8 85,6 80,2 74,1 69,4 64,3 56,8 50,7 CF567B SEL A 5 000,0 96,7 92,5 89,4 86,1 80,8 74,8 70,1 65,2 58,0 52,4 CF567B SEL A 6 000,0 97,2 93,0 89,9 86,7 81,4 75,5 70,9 66,0 59,4 54,3 CF567B SEL A 7 000,0 97,7 93,4 90,4 87,1 81,9 76,0 71,5 66,7 60,8 55,6 CF567B SEL D 10 000,0 96,3 92,1 89,4 86,3 81,4 75,9 72,0 67,0 61,3 51,9 CF567B SEL D 13 000,0 99,2 95,2 92,4 89,4 84,7 79,3 75,4 70,5 64,5 56,1 CF567B SEL D 16 000,0 101,7 97,6 95,0 92,1 87,4 82,1 78,3 73,5 67,3 60,0 CF567B SEL D 19 000,0 103,9 99,9 97,3 94,5 89,9 84,7 81,0 76,2 70,3 63,7 CF567B SEL D 23 500,0 108,4 104,5 102,0 99,3 95,0 89,9 86,4 81,5 75,5 69,5 CF66D LAmax A 8 000,0 99,2 92,0 86,6 81,0 72,1 63,0 56,5 49,1 40,8 32,5 1.7.2015 EN Official Journal of the European Union L 168/749Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) CF66D LAmax A 14 000,0 102,1 95,0 89,9 84,5 76,0 67,0 60,6 53,3 45,1 37,1 CF66D LAmax D 20 000,0 104,5 97,6 92,7 87,5 79,3 70,4 64,1 56,9 48,9 41,0 CF66D LAmax D 28 000,0 106,2 99,4 94,6 89,5 81,5 72,6 66,4 59,3 51,3 43,6 CF66D LAmax D 36 000,0 107,8 101,1 96,5 91,5 83,7 74,9 68,7 61,7 53,8 46,2 CF66D SEL A 8 000,0 100,7 95,5 91,7 87,5 81,1 74,0 68,8 63,0 56,3 49,7 CF66D SEL A 14 000,0 104,4 99,5 95,9 92,0 85,9 79,0 73,9 68,3 61,7 55,2 CF66D SEL D 20 000,0 106,8 102,2 98,7 95,0 89,0 82,3 77,3 71,8 65,4 58,9 CF66D SEL D 28 000,0 109,3 104,8 101,4 98,0 92,2 85,6 80,7 75,3 69,0 62,6 CF66D SEL D 36 000,0 110,9 106,6 103,3 100,0 94,3 87,8 83,0 77,6 71,4 65,1 CF680C LAmax A 5 500,0 94,4 87,4 82,8 78,0 70,4 61,9 55,7 48,8 40,9 31,7 CF680C LAmax A 7 000,0 95,3 88,1 83,5 78,5 70,7 62,1 55,8 49,0 40,9 31,4 CF680C LAmax A 12 000,0 95,9 88,8 84,1 79,1 71,3 62,7 56,4 49,6 41,7 32,5 CF680C LAmax A 15 000,0 98,9 91,2 86,2 80,7 72,3 63,4 57,0 50,1 42,0 32,1 CF680C LAmax D 17 000,0 101,6 93,6 87,8 81,4 71,6 62,2 55,8 48,8 40,6 30,5 CF680C LAmax D 21 000,0 100,8 93,1 87,6 81,7 72,6 63,6 57,4 50,7 42,7 33,0 CF680C LAmax D 25 000,0 100,6 93,1 87,8 82,3 73,8 65,0 59,0 52,4 44,7 35,2 CF680C LAmax D 33 000,0 101,3 94,2 89,3 84,2 76,3 67,9 62,1 55,7 48,2 39,2 CF680C LAmax D 41 000,0 103,1 96,3 91,5 86,7 79,1 70,9 65,1 58,9 51,5 42,6 CF680C LAmax D 54 000,0 109,7 103,2 98,8 94,0 86,4 78,2 72,5 66,2 59,0 50,4 CF680C SEL A 5 500,0 95,9 93,2 90,4 87,2 82,1 76,2 71,6 66,4 60,4 53,5 L 168/750 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) CF680C SEL A 7 000,0 96,6 93,7 90,7 87,5 82,2 76,2 71,5 66,4 60,4 53,4 CF680C SEL A 12 000,0 98,0 94,9 91,8 88,5 83,0 76,9 72,2 67,1 61,0 53,9 CF680C SEL A 15 000,0 99,2 97,1 93,8 90,1 84,2 77,6 72,9 67,7 61,6 54,5 CF680C SEL D 17 000,0 104,5 99,3 95,3 90,7 83,1 75,4 70,6 65,4 59,2 51,4 CF680C SEL D 21 000,0 103,1 98,4 94,7 90,5 83,7 76,8 72,3 67,3 61,4 53,9 CF680C SEL D 25 000,0 102,5 98,0 94,6 90,8 84,6 78,2 73,8 69,1 63,4 56,2 CF680C SEL D 33 000,0 102,6 98,5 95,5 92,1 86,7 80,9 76,9 72,3 66,9 60,1 CF680C SEL D 41 000,0 104,0 100,1 97,3 94,2 89,2 83,8 79,9 75,4 70,1 63,5 CF680C SEL D 54 000,0 109,8 106,1 103,6 100,8 96,1 90,8 86,9 82,6 77,5 71,2 CF680E LAmax A 6 000,0 93,8 86,6 82,0 77,2 69,6 61,4 55,4 48,7 41,1 33,0 CF680E LAmax A 12 000,0 96,7 89,2 84,3 79,1 71,0 62,4 56,2 49,2 41,6 33,5 CF680E LAmax D 34 000,0 105,5 97,4 92,0 86,3 77,7 68,4 61,8 54,3 46,2 37,4 CF680E LAmax D 42 000,0 106,0 98,2 93,2 88,0 79,8 70,7 64,2 56,9 48,8 40,1 CF680E LAmax D 52 000,0 107,5 100,1 95,2 90,2 82,3 73,8 67,6 60,6 52,7 44,0 CF680E LAmax D 62 000,0 111,7 104,4 99,6 94,5 86,6 78,4 72,4 65,6 57,6 48,8 CF680E SEL A 6 000,0 99,1 93,5 90,3 87,1 81,9 76,1 71,7 66,6 60,3 53,7 CF680E SEL A 12 000,0 100,0 94,8 91,5 88,2 82,8 76,9 72,3 67,1 60,8 54,2 CF680E SEL D 34 000,0 106,7 101,4 98,1 94,5 88,6 82,2 77,6 72,2 65,9 58,9 CF680E SEL D 42 000,0 107,2 102,4 99,4 96,0 90,6 84,4 79,9 74,6 68,4 61,5 CF680E SEL D 52 000,0 108,4 104,1 101,2 98,2 93,2 87,4 83,0 77,6 71,6 64,8 1.7.2015 EN Official Journal of the European Union L 168/751Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) CF680E SEL D 62 000,0 112,7 108,3 105,4 102,5 97,6 91,9 87,7 82,5 76,5 70,4 CF700 LAmax A 850,0 98,2 90,6 84,9 78,7 68,7 59,1 52,4 45,3 37,6 29,2 CF700 LAmax A 1 500,0 100,5 93,5 88,6 83,5 74,6 64,9 57,6 49,7 41,7 33,0 CF700 LAmax D 2 500,0 101,0 94,0 89,1 84,0 75,9 66,9 60,2 52,8 44,8 36,1 CF700 LAmax D 3 750,0 108,6 101,4 96,3 91,0 82,4 72,6 65,3 57,2 48,4 38,9 CF700 SEL A 850,0 100,7 95,3 91,2 86,4 78,7 71,4 66,2 60,5 54,4 47,4 CF700 SEL A 1 500,0 102,8 97,8 94,1 90,0 83,4 75,9 70,1 63,7 57,2 50,0 CF700 SEL D 2 500,0 104,2 99,5 96,1 92,5 86,7 79,9 74,7 68,9 62,3 55,1 CF700 SEL D 3 750,0 111,3 106,4 102,8 99,0 92,6 85,1 79,2 72,7 65,4 57,4 CFM562 LAmax A 5 000,0 96,4 89,8 85,2 80,4 72,6 64,0 57,5 50,3 42,1 33,4 CFM562 LAmax A 10 000,0 100,5 94,0 89,2 84,4 76,7 68,7 61,8 54,7 46,5 37,8 CFM562 LAmax D 10 000,0 100,5 94,0 89,2 84,4 76,7 68,7 61,8 54,7 46,5 37,8 CFM562 LAmax D 15 500,0 106,1 99,5 94,8 89,9 82,3 73,9 67,8 60,8 52,6 43,9 CFM562 SEL A 5 000,0 97,9 93,5 90,4 87,1 81,9 75,6 70,7 64,9 58,2 51,0 CFM562 SEL A 10 000,0 101,5 97,2 94,2 91,0 85,9 79,8 75,0 69,3 62,6 55,4 CFM562 SEL D 10 000,0 101,5 97,2 94,2 91,0 85,9 79,8 75,0 69,3 62,6 55,4 CFM562 SEL D 15 500,0 106,5 102,5 99,6 96,5 91,6 85,7 81,0 75,5 68,9 61,6 CFM563 LAmax A 2 500,0 93,4 85,7 80,8 75,6 67,4 58,2 51,5 44,0 36,5 29,1 CFM563 LAmax A 3 500,0 94,5 86,7 81,8 76,5 68,2 59,1 52,5 45,1 37,6 30,4 CFM563 LAmax A 4 500,0 95,8 88,0 83,0 77,7 69,5 60,4 53,9 46,6 39,2 32,1 L 168/752 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) CFM563 LAmax A 5 500,0 97,2 89,3 84,4 79,1 71,0 62,0 55,6 48,3 41,0 33,9 CFM563 LAmax D 6 500,0 95,8 89,1 84,5 79,6 71,7 63,2 56,9 49,8 42,5 35,7 CFM563 LAmax D 9 000,0 97,0 90,3 85,8 80,9 73,2 64,8 58,6 51,6 44,5 37,8 CFM563 LAmax D 11 500,0 98,6 92,0 87,4 82,7 75,0 66,7 60,6 53,8 46,8 40,2 CFM563 LAmax D 14 000,0 100,4 93,8 89,3 84,5 77,0 68,8 62,8 56,0 49,2 42,7 CFM563 LAmax D 16 500,0 102,2 95,7 91,2 86,5 79,0 70,9 65,0 58,4 51,6 45,3 CFM563 LAmax D 19 000,0 104,4 97,9 93,5 88,9 81,5 73,5 67,6 61,1 54,5 48,3 CFM563 SEL A 2 500,0 94,7 90,2 87,1 83,7 78,1 71,5 66,7 61,1 55,4 49,8 CFM563 SEL A 3 500,0 96,3 91,5 88,3 84,7 79,0 72,5 67,7 62,2 56,6 51,2 CFM563 SEL A 4 500,0 97,6 92,8 89,5 85,8 80,1 73,7 69,0 63,6 58,1 52,8 CFM563 SEL A 5 500,0 98,8 93,9 90,6 86,9 81,4 75,0 70,4 65,1 59,7 54,4 CFM563 SEL D 6 500,0 96,4 92,3 89,3 86,1 80,9 75,2 70,8 65,6 60,3 55,4 CFM563 SEL D 9 000,0 97,9 93,7 90,7 87,5 82,4 76,8 72,5 67,5 62,5 57,7 CFM563 SEL D 11 500,0 99,5 95,4 92,5 89,3 84,3 78,9 74,7 69,9 64,9 60,3 CFM563 SEL D 14 000,0 101,1 97,2 94,4 91,3 86,5 81,2 77,1 72,3 67,5 63,0 CFM563 SEL D 16 500,0 102,8 99,0 96,3 93,5 88,8 83,6 79,6 74,9 70,2 65,8 CFM563 SEL D 19 000,0 104,7 101,2 98,7 96,0 91,5 86,4 82,5 78,0 73,4 69,1 CFM565 LAmax A 2 700,0 91,7 84,4 79,7 74,8 67,0 58,5 52,2 45,3 37,5 29,5 CFM565 LAmax A 6 000,0 93,8 86,1 80,9 75,6 67,4 58,7 52,4 45,5 37,7 29,7 CFM565 LAmax D 12 000,0 100,3 92,0 86,2 80,3 71,1 61,7 55,4 48,6 40,9 33,1 1.7.2015 EN Official Journal of the European Union L 168/753Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) CFM565 LAmax D 15 500,0 102,5 94,9 89,5 83,6 74,0 65,0 58,8 52,1 44,7 36,8 CFM565 LAmax D 19 000,0 104,3 96,6 91,1 85,7 77,2 68,2 62,2 55,5 47,9 40,0 CFM565 LAmax D 22 500,0 105,9 98,9 94,1 88,9 80,9 72,5 66,1 59,4 51,7 43,3 CFM565 SEL A 2 700,0 96,6 90,5 87,5 84,2 78,9 72,8 68,2 62,9 56,8 50,3 CFM565 SEL A 6 000,0 97,4 91,6 88,2 84,8 79,3 73,1 68,5 63,3 57,1 50,6 CFM565 SEL D 12 000,0 100,9 96,2 92,4 88,3 81,9 75,5 71,1 66,0 60,0 53,8 CFM565 SEL D 15 500,0 103,6 99,0 95,3 91,5 85,6 79,3 74,9 69,9 64,2 57,9 CFM565 SEL D 19 000,0 104,7 100,5 97,3 93,9 88,3 82,4 78,1 73,2 67,3 61,0 CFM565 SEL D 22 500,0 106,5 102,4 99,6 96,4 91,4 85,7 81,5 76,5 70,8 64,3 CJ610 LAmax A 700,0 98,5 91,9 87,3 82,4 74,3 65,0 58,0 50,1 41,3 31,6 CJ610 LAmax A 1 800,0 117,1 110,3 105,6 100,5 92,2 82,5 75,1 66,7 57,0 46,0 CJ610 LAmax D 1 800,0 117,1 110,3 105,6 100,5 92,2 82,5 75,1 66,7 57,0 46,0 CJ610 LAmax D 2 600,0 122,2 115,0 109,8 104,3 95,3 85,3 77,6 68,9 59,0 47,9 CJ610 SEL A 700,0 100,8 96,4 93,3 89,9 84,0 77,0 71,5 65,1 57,8 49,6 CJ610 SEL A 1 800,0 119,3 114,8 111,6 108,0 101,9 94,5 88,6 81,6 73,4 63,9 CJ610 SEL D 1 800,0 119,3 114,8 111,6 108,0 101,9 94,5 88,6 81,6 73,4 63,9 CJ610 SEL D 2 600,0 124,7 119,7 116,0 112,0 105,3 97,5 91,3 84,1 75,7 66,1 CT75 LAmax A 30,0 86,9 80,5 76,1 71,6 64,5 57,0 51,6 45,6 38,6 30,9 CT75 LAmax A 75,0 88,1 81,7 77,4 73,0 66,0 58,5 53,3 47,6 41,3 34,5 CT75 LAmax D 75,0 88,1 81,7 77,4 73,0 66,0 58,5 53,3 47,6 41,3 34,5 L 168/754 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) CT75 LAmax D 100,0 95,2 88,9 84,7 80,3 73,4 66,1 60,8 54,8 47,9 40,1 CT75 SEL A 30,0 87,5 83,4 80,5 77,5 72,7 67,4 63,6 59,1 53,6 47,3 CT75 SEL A 75,0 89,0 85,1 82,5 79,5 75,1 69,9 66,2 62,0 57,2 51,8 CT75 SEL D 75,0 89,0 85,1 82,5 79,5 75,1 69,9 66,2 62,0 57,2 51,8 CT75 SEL D 100,0 97,0 92,8 90,1 87,3 82,9 77,8 74,0 69,5 64,1 57,8 EPW118 LAmax A 700,0 88,9 82,0 77,1 71,9 63,6 55,2 49,3 42,9 34,7 27,0 EPW118 LAmax A 1 000,0 88,3 81,5 76,8 71,8 64,0 55,5 49,4 42,4 33,5 25,1 EPW118 LAmax D 2 000,0 85,8 79,2 74,8 70,2 63,0 55,2 49,6 43,2 35,4 28,1 EPW118 LAmax D 3 000,0 86,4 79,9 75,6 71,1 64,0 56,6 51,3 45,6 38,7 32,1 EPW118 LAmax D 3 800,0 92,0 85,7 81,5 77,1 70,4 63,3 58,4 53,0 46,2 39,7 EPW118 SEL A 700,0 94,5 87,5 82,7 77,5 69,2 60,7 54,9 48,4 40,3 32,6 EPW118 SEL A 1 000,0 94,9 88,1 83,4 78,4 70,6 62,1 56,0 49,0 40,2 31,7 EPW118 SEL D 2 000,0 98,4 91,9 87,4 82,8 75,6 67,8 62,2 55,9 48,1 40,7 EPW118 SEL D 3 000,0 98,7 92,3 87,9 83,4 76,4 68,9 63,7 58,0 51,0 44,5 EPW118 SEL D 3 800,0 100,9 94,6 90,4 86,0 79,3 72,2 67,3 61,9 55,0 48,6 FJ44-4 LAmax A 600,0 86,7 79,1 73,8 68,1 59,1 49,4 42,7 35,7 28,2 20,8 FJ44-4 LAmax A 900,0 89,1 81,8 76,6 70,9 61,7 51,7 44,6 37,1 29,1 21,1 FJ44-4 LAmax D 1 700,0 96,4 88,4 82,8 76,9 67,6 57,7 50,9 43,7 36,2 28,8 FJ44-4 LAmax D 2 400,0 98,2 91,8 87,1 81,8 73,2 63,5 56,7 49,3 41,3 33,4 FJ44-4 LAmax D 3 000,0 101,5 95,2 90,6 85,4 76,8 67,3 60,5 53,1 45,2 37,3 1.7.2015 EN Official Journal of the European Union L 168/755Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) FJ44-4 LAmax D 3 300,0 103,8 97,4 92,7 87,5 78,9 69,4 62,7 55,4 47,6 39,8 FJ44-4 SEL A 600,0 87,3 82,8 79,5 75,9 70,0 63,4 58,8 53,9 48,6 43,3 FJ44-4 SEL A 900,0 90,4 85,5 82,0 78,1 71,8 64,9 60,0 54,8 49,2 43,6 FJ44-4 SEL D 1 700,0 94,2 90,0 86,8 83,2 77,2 70,5 65,7 60,6 55,0 49,3 FJ44-4 SEL D 2 400,0 98,2 94,4 91,5 88,2 82,5 76,0 71,3 66,1 60,5 54,8 FJ44-4 SEL D 3 000,0 102,0 98,5 95,7 92,5 86,9 80,4 75,7 70,5 64,9 59,1 FJ44-4 SEL D 3 300,0 104,5 101,0 98,2 95,0 89,5 83,2 78,6 73,5 68,0 62,4 GE90 LAmax A 12 000,0 94,2 86,8 81,8 76,8 68,9 60,3 54,1 47,5 40,8 34,5 GE90 LAmax A 17 000,0 95,3 87,9 82,9 77,9 69,9 61,2 55,0 48,3 41,5 35,1 GE90 LAmax A 22 000,0 96,6 89,0 84,0 78,9 70,7 62,0 55,6 48,9 42,0 35,6 GE90 LAmax A 27 000,0 97,9 90,0 84,9 79,7 71,4 62,5 56,2 49,4 42,5 36,0 GE90 LAmax D 31 000,0 97,5 90,7 86,0 80,8 72,8 63,8 57,5 50,4 43,3 36,4 GE90 LAmax D 41 000,0 98,8 92,0 87,3 82,2 74,2 65,3 59,0 52,1 45,1 38,4 GE90 LAmax D 51 000,0 100,6 93,8 89,2 84,1 76,2 67,3 61,1 54,3 47,5 40,9 GE90 LAmax D 61 000,0 102,8 96,0 91,4 86,4 78,5 69,7 63,6 56,9 50,1 43,5 GE90 LAmax D 71 000,0 105,0 98,3 93,7 88,7 80,8 72,1 66,1 59,4 52,7 46,3 GE90 LAmax D 81 000,0 109,0 102,4 97,8 92,9 85,2 76,7 70,8 64,4 58,0 52,0 GE90 SEL A 12 000,0 97,7 92,8 89,5 86,3 80,9 74,9 70,4 65,5 60,5 55,8 GE90 SEL A 17 000,0 98,6 93,9 90,6 87,2 81,7 75,7 71,1 66,1 61,1 56,4 GE90 SEL A 22 000,0 99,8 94,9 91,5 88,1 82,5 76,3 71,7 66,7 61,6 56,9 L 168/756 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) GE90 SEL A 27 000,0 101,0 95,9 92,4 88,8 83,2 76,9 72,3 67,2 62,1 57,3 GE90 SEL D 31 000,0 100,0 95,8 92,7 89,2 83,5 76,9 72,2 66,9 61,4 56,2 GE90 SEL D 41 000,0 101,2 97,1 94,2 90,7 85,1 78,5 73,9 68,7 63,4 58,4 GE90 SEL D 51 000,0 102,7 98,8 95,9 92,5 87,0 80,6 76,1 71,1 66,0 61,1 GE90 SEL D 61 000,0 104,4 100,6 97,7 94,5 89,2 82,9 78,6 73,7 68,7 64,0 GE90 SEL D 71 000,0 106,1 102,3 99,5 96,4 91,3 85,3 81,1 76,3 71,5 66,9 GE90 SEL D 81 000,0 109,1 105,4 102,7 99,7 95,0 89,6 85,7 81,3 77,0 73,0 GE9015 LAmax A 12 000,0 96,1 88,9 84,3 79,4 71,6 63,2 57,1 50,5 43,8 37,5 GE9015 LAmax A 17 333,0 96,5 89,3 84,6 79,7 71,9 63,4 57,3 50,7 43,9 37,6 GE9015 LAmax A 22 667,0 97,2 90,0 85,3 80,3 72,5 63,9 57,6 51,0 44,1 37,7 GE9015 LAmax A 28 000,0 98,2 90,9 86,1 81,1 73,2 64,5 58,1 51,4 44,4 37,9 GE9015 LAmax D 39 000,0 100,4 93,2 88,4 83,4 75,3 66,5 60,1 52,9 45,6 38,6 GE9015 LAmax D 50 600,0 101,8 94,7 89,9 84,8 76,6 67,7 61,5 54,5 47,4 40,6 GE9015 LAmax D 62 200,0 103,5 96,6 91,8 86,7 78,5 69,6 63,3 56,4 49,4 42,7 GE9015 LAmax D 73 800,0 105,5 98,6 93,8 88,7 80,5 71,7 65,4 58,6 51,7 45,0 GE9015 LAmax D 85 400,0 108,5 101,7 96,9 91,9 83,8 75,1 68,9 62,1 55,3 48,8 GE9015 LAmax D 97 000,0 114,5 107,6 103,0 98,1 90,4 81,8 75,7 68,9 61,9 55,4 GE9015 SEL A 12 000,0 99,5 94,9 91,8 88,7 83,5 77,6 73,1 68,3 63,3 58,6 GE9015 SEL A 17 333,0 99,9 95,2 92,1 88,9 83,6 77,7 73,2 68,3 63,2 58,5 GE9015 SEL A 22 667,0 100,5 95,9 92,8 89,5 84,1 78,1 73,5 68,5 63,4 58,6 1.7.2015 EN Official Journal of the European Union L 168/757Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) GE9015 SEL A 28 000,0 101,3 96,7 93,5 90,2 84,8 78,7 74,0 68,9 63,7 58,9 GE9015 SEL D 39 000,0 102,7 97,8 94,4 90,9 85,3 78,9 74,3 68,9 63,5 58,3 GE9015 SEL D 50 600,0 103,6 98,9 95,7 92,3 86,7 80,4 75,9 70,7 65,5 60,6 GE9015 SEL D 62 200,0 105,0 100,5 97,4 94,1 88,5 82,3 77,9 72,9 67,8 63,0 GE9015 SEL D 73 800,0 106,6 102,3 99,2 96,0 90,5 84,4 80,0 75,1 70,1 65,4 GE9015 SEL D 85 400,0 109,3 105,0 102,1 98,9 93,6 87,7 83,4 78,6 73,7 69,1 GE9015 SEL D 97 000,0 114,7 110,6 107,7 104,7 99,7 94,1 89,9 85,1 80,2 75,6 GENX67 LAmax A 7 000,0 99,0 91,8 87,0 82,2 74,4 65,9 59,6 52,8 45,9 39,4 GENX67 LAmax A 12 000,0 99,6 92,4 87,6 82,8 75,0 66,5 60,2 53,3 46,4 39,9 GENX67 LAmax A 17 000,0 100,0 92,8 88,0 83,2 75,3 66,7 60,4 53,5 46,5 40,0 GENX67 LAmax A 22 000,0 100,4 93,2 88,3 83,4 75,4 66,8 60,4 53,5 46,5 39,9 GENX67 LAmax D 17 000,0 101,0 94,3 89,7 84,9 77,2 68,7 62,5 55,5 48,4 41,5 GENX67 LAmax D 25 000,0 101,5 94,8 90,2 85,3 77,5 68,8 62,6 55,6 48,4 41,6 GENX67 LAmax D 33 000,0 102,9 96,2 91,5 86,6 78,7 70,0 63,7 56,6 49,5 42,6 GENX67 LAmax D 41 000,0 104,8 98,0 93,4 88,5 80,5 71,7 65,4 58,3 51,0 44,1 GENX67 LAmax D 49 000,0 107,0 100,2 95,5 90,6 82,6 73,8 67,4 60,2 53,0 46,0 GENX67 LAmax D 57 000,0 110,1 103,4 98,7 93,8 85,8 76,9 70,5 63,2 55,9 49,0 GENX67 SEL A 7 000,0 101,0 96,8 93,9 90,9 85,7 79,7 75,1 70,0 64,9 60,1 GENX67 SEL A 12 000,0 101,6 97,4 94,5 91,4 86,2 80,2 75,6 70,5 65,3 60,4 GENX67 SEL A 17 000,0 102,3 98,0 95,0 91,9 86,6 80,6 75,9 70,7 65,4 60,5 L 168/758 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) GENX67 SEL A 22 000,0 102,8 98,5 95,5 92,3 86,9 80,8 76,1 70,8 65,4 60,4 GENX67 SEL D 17 000,0 102,0 98,1 95,3 92,4 87,4 81,7 77,3 72,1 66,9 61,8 GENX67 SEL D 25 000,0 102,6 98,6 95,8 92,8 87,6 81,7 77,3 72,1 66,9 61,8 GENX67 SEL D 33 000,0 103,9 99,9 97,1 94,0 88,8 82,8 78,4 73,2 68,0 62,9 GENX67 SEL D 41 000,0 105,5 101,6 98,8 95,7 90,5 84,5 80,1 74,9 69,7 64,7 GENX67 SEL D 49 000,0 107,4 103,5 100,7 97,7 92,5 86,6 82,2 77,0 71,8 66,8 GENX67 SEL D 57 000,0 110,1 106,3 103,5 100,6 95,5 89,7 85,3 80,2 75,1 70,2 GP7270 LAmax A 5 500,0 92,0 86,2 81,9 77,4 69,8 61,4 55,3 48,6 41,2 33,5 GP7270 LAmax A 7 500,0 92,4 86,4 82,1 77,5 69,9 61,6 55,5 48,8 41,3 33,5 GP7270 LAmax A 12 000,0 93,4 87,0 82,5 77,9 70,3 61,9 55,8 49,1 41,6 33,7 GP7270 LAmax A 14 000,0 94,0 87,5 82,9 78,1 70,4 62,0 55,9 49,2 41,7 33,9 GP7270 LAmax D 40 000,0 99,3 92,8 88,5 83,7 75,9 67,2 60,9 53,9 45,9 37,3 GP7270 LAmax D 50 000,0 102,0 95,9 91,3 86,5 78,7 70,1 63,8 56,8 48,8 40,2 GP7270 LAmax D 60 000,0 104,1 98,2 93,8 89,1 81,6 73,0 66,8 59,7 51,7 43,1 GP7270 LAmax D 80 000,0 111,3 105,6 101,7 97,1 90,0 81,7 75,5 68,2 61,1 52,5 GP7270 SEL A 5 500,0 96,8 92,6 89,8 86,7 81,6 75,7 71,2 66,2 60,4 54,2 GP7270 SEL A 7 500,0 97,3 93,0 90,0 86,9 81,8 75,9 71,5 66,4 60,6 54,3 GP7270 SEL A 12 000,0 98,4 93,9 90,8 87,6 82,4 76,4 72,0 66,9 61,0 54,6 GP7270 SEL A 14 000,0 99,0 94,3 91,2 88,0 82,7 76,8 72,3 67,2 61,3 54,8 GP7270 SEL D 40 000,0 102,6 98,2 95,0 91,8 86,5 80,6 76,1 71,0 64,9 58,2 1.7.2015 EN Official Journal of the European Union L 168/759Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) GP7270 SEL D 50 000,0 105,6 101,0 97,9 94,8 89,7 83,8 79,5 74,3 68,3 61,6 GP7270 SEL D 60 000,0 107,7 103,5 100,5 97,4 92,2 86,4 82,0 76,9 70,8 64,1 GP7270 SEL D 80 000,0 114,8 111,0 108,5 105,6 100,6 94,9 90,6 85,5 79,6 72,7 IO320B LAmax A 55,0 79,0 72,6 68,2 63,6 56,4 48,5 43,0 36,8 30,0 22,9 IO320B LAmax A 107,0 79,8 73,3 68,9 64,3 56,8 48,3 42,1 35,3 27,9 20,6 IO320B LAmax D 201,0 86,6 79,8 75,1 70,0 62,5 54,3 48,3 41,6 34,2 26,7 IO320B LAmax D 214,0 89,5 82,6 77,8 72,7 64,6 56,2 50,1 43,4 35,8 28,1 IO320B LAmax D 339,0 96,1 89,0 84,0 78,6 70,2 61,5 55,3 48,3 40,5 32,3 IO320B SEL A 55,0 82,3 78,4 75,7 72,9 68,2 62,8 58,8 54,3 49,2 44,1 IO320B SEL A 107,0 83,5 79,8 77,1 74,2 69,1 63,0 58,5 53,5 48,0 42,8 IO320B SEL D 201,0 90,2 85,8 82,8 79,6 74,3 68,3 63,9 58,8 53,0 47,2 IO320B SEL D 214,0 93,9 89,0 85,7 82,2 76,6 70,4 65,9 60,7 54,7 48,6 IO320B SEL D 339,0 98,8 94,5 91,4 88,1 82,5 76,1 71,4 66,1 60,0 53,5 IO360L LAmax A 26,6 71,6 64,2 59,7 55,0 47,7 39,8 34,4 28,5 22,4 16,9 IO360L LAmax A 58,2 78,8 72,2 67,7 62,9 55,2 46,7 40,7 34,1 27,0 20,3 IO360L LAmax D 59,6 82,7 75,6 71,1 66,4 58,9 50,8 45,0 38,6 31,7 24,5 IO360L LAmax D 100,0 84,6 77,8 73,2 68,2 60,4 52,0 46,2 39,9 33,5 25,6 IO360L SEL A 26,6 73,0 68,7 65,8 63,0 58,6 53,6 50,0 46,2 42,4 38,8 IO360L SEL A 58,2 79,3 75,3 72,7 69,9 65,1 59,6 55,5 51,1 46,3 43,0 IO360L SEL D 59,6 83,5 79,8 77,2 74,4 69,7 64,1 59,9 55,3 50,3 45,8 L 168/760 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) IO360L SEL D 100,0 84,9 81,4 78,9 76,0 71,2 65,5 61,3 56,5 51,8 46,3 IO540 LAmax A 2 400,0 82,2 75,8 71,7 67,3 60,6 53,5 48,7 43,4 37,7 31,6 IO540 LAmax A 2 500,0 86,4 80,1 75,9 71,5 64,7 57,6 52,7 47,4 41,7 35,6 IO540 LAmax A 2 700,0 94,6 88,2 83,8 79,3 72,0 63,9 58,2 52,2 45,6 38,8 IO540 LAmax D 2 500,0 92,0 85,6 81,2 76,7 69,5 62,0 56,8 51,3 45,2 38,8 IO540 LAmax D 2 700,0 99,0 92,6 88,3 83,8 76,6 68,7 63,1 56,9 50,0 42,7 IO540 SEL A 2 400,0 82,7 79,3 77,0 74,6 70,8 66,6 63,5 60,1 56,1 51,7 IO540 SEL A 2 500,0 86,6 83,2 80,8 78,4 74,4 70,2 67,1 63,7 59,8 55,4 IO540 SEL A 2 700,0 92,9 89,5 87,2 84,6 80,5 75,8 72,2 68,2 63,6 58,4 IO540 SEL D 2 500,0 91,8 88,3 85,8 83,2 78,9 74,1 70,8 67,1 63,0 58,3 IO540 SEL D 2 700,0 96,8 93,5 91,1 88,6 84,3 79,4 75,7 71,5 66,7 61,4 JT15D1 LAmax A 300,0 83,2 76,3 71,5 66,5 58,6 50,1 43,9 37,1 29,5 21,0 JT15D1 LAmax A 600,0 85,7 78,8 74,0 69,0 61,1 52,6 46,4 39,6 32,0 23,5 JT15D1 LAmax D 1 200,0 93,2 86,2 81,3 76,0 67,6 58,4 51,8 44,6 36,7 28,1 JT15D1 LAmax D 1 550,0 95,3 88,6 83,9 79,0 71,1 62,3 55,7 48,4 40,1 31,0 JT15D1 SEL A 300,0 85,6 81,0 77,7 74,2 68,5 62,3 57,6 52,3 46,2 39,2 JT15D1 SEL A 600,0 86,8 82,2 78,9 75,4 69,7 63,5 58,8 53,5 47,4 40,4 JT15D1 SEL D 1 200,0 96,4 91,7 88,2 84,5 78,3 71,4 66,3 60,6 54,2 47,1 JT15D1 SEL D 1 550,0 98,0 93,6 90,4 87,0 81,4 74,8 69,7 63,9 57,1 49,5 JT15D5 LAmax A 670,0 90,2 82,7 77,2 71,2 61,7 52,0 45,5 38,5 30,7 21,2 1.7.2015 EN Official Journal of the European Union L 168/761Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) JT15D5 LAmax A 1 500,0 101,3 94,4 89,6 84,4 75,8 67,2 61,3 54,4 46,4 37,5 JT15D5 LAmax D 1 500,0 101,3 94,4 89,6 84,4 75,8 67,2 61,3 54,4 46,4 37,5 JT15D5 LAmax D 2 100,0 103,7 97,2 92,6 87,8 80,1 72,0 66,0 59,2 51,1 42,2 JT15D5 SEL A 670,0 90,2 85,6 82,2 78,4 72,3 65,3 60,3 54,7 48,4 41,4 JT15D5 SEL A 1 500,0 104,1 99,8 96,8 93,4 87,3 81,1 76,6 71,3 64,8 57,4 JT15D5 SEL D 1 500,0 104,1 99,8 96,8 93,4 87,3 81,1 76,6 71,3 64,8 57,4 JT15D5 SEL D 2 100,0 106,0 102,4 99,7 96,8 91,6 85,7 81,2 75,9 69,3 61,8 JT3D LAmax A 4 000,0 111,8 104,5 98,9 93,0 81,8 67,8 59,2 50,9 41,8 32,9 JT3D LAmax A 6 000,0 114,0 106,8 101,5 95,5 84,6 71,3 63,3 55,3 46,4 37,2 JT3D LAmax D 8 000,0 115,9 109,0 103,7 98,0 87,6 75,4 67,7 59,8 51,1 42,1 JT3D LAmax D 10 000,0 117,5 110,8 105,6 100,0 90,4 79,5 71,8 63,8 55,2 46,5 JT3D LAmax D 12 000,0 118,2 111,5 106,4 101,0 92,1 82,0 74,5 66,8 58,6 49,7 JT3D LAmax D 15 000,0 119,7 113,0 107,9 102,5 94,0 85,0 78,1 70,3 62,0 53,5 JT3D SEL A 4 000,0 112,5 107,5 103,6 99,0 90,0 78,3 71,2 64,5 57,0 49,5 JT3D SEL A 6 000,0 114,8 109,8 105,9 101,5 92,8 81,8 75,2 68,9 61,7 54,1 JT3D SEL D 8 000,0 117,1 112,0 108,2 104,0 95,9 85,9 79,6 73,4 66,1 58,6 JT3D SEL D 10 000,0 119,0 113,9 110,1 106,0 98,5 90,0 83,7 77,5 70,1 62,8 JT3D SEL D 12 000,0 120,7 115,6 111,9 107,7 100,8 92,6 87,1 81,0 73,9 66,5 JT3D SEL D 15 000,0 122,5 117,4 113,6 109,5 103,1 96,4 90,8 85,1 77,9 70,4 JT3DQ LAmax A 3 000,0 102,8 95,2 89,6 83,1 74,3 65,0 58,4 51,0 42,6 34,0 L 168/762 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) JT3DQ LAmax A 5 000,0 105,2 96,2 89,9 84,4 75,7 66,2 59,5 52,1 43,9 35,5 JT3DQ LAmax D 11 000,0 107,5 100,8 96,3 91,4 83,5 75,0 68,7 61,7 53,6 45,3 JT3DQ LAmax D 15 500,0 114,2 107,7 103,2 98,7 91,4 83,7 78,2 72,0 64,9 57,3 JT3DQ SEL A 3 000,0 104,4 99,4 95,6 91,4 84,8 77,8 72,6 66,7 59,9 52,7 JT3DQ SEL A 5 000,0 105,1 100,0 96,2 91,9 85,4 78,4 73,2 67,3 60,6 53,7 JT3DQ SEL D 11 000,0 109,1 105,4 102,7 99,8 95,0 88,9 84,2 78,6 72,1 65,2 JT3DQ SEL D 15 500,0 116,9 113,3 110,8 108,1 103,5 98,1 94,1 89,4 83,9 77,7 JT4A LAmax A 4 000,0 109,2 101,7 96,3 90,5 80,6 69,0 61,7 54,5 45,7 36,9 JT4A LAmax A 6 000,0 111,1 103,6 98,2 92,5 82,7 71,2 63,7 56,3 48,1 39,5 JT4A LAmax D 10 000,0 116,5 109,3 104,1 98,5 89,3 79,0 71,6 63,7 54,5 45,4 JT4A LAmax D 12 000,0 119,6 112,4 107,4 102,0 93,1 82,9 75,3 67,4 58,4 48,8 JT4A LAmax D 15 000,0 125,3 118,3 113,2 108,0 99,1 89,2 81,5 73,5 64,3 54,6 JT4A SEL A 4 000,0 110,8 105,4 101,2 97,0 89,6 80,6 74,3 68,6 60,9 52,7 JT4A SEL A 6 000,0 112,7 107,3 103,3 99,0 91,8 82,9 76,8 71,1 63,6 55,7 JT4A SEL D 10 000,0 117,4 112,4 108,7 104,5 97,4 89,2 83,3 76,9 69,4 61,5 JT4A SEL D 12 000,0 120,0 115,2 111,6 107,5 100,6 92,6 86,6 80,3 72,6 64,7 JT4A SEL D 15 000,0 125,5 120,8 117,6 113,5 106,9 99,3 93,3 86,6 78,7 70,6 JT9D7Q LAmax A 8 560,0 101,8 95,4 91,0 86,3 78,6 69,9 63,6 56,7 49,0 40,9 JT9D7Q LAmax A 14 000,0 103,3 96,8 92,2 87,1 79,2 70,5 64,2 57,5 49,9 41,9 JT9D7Q LAmax D 24 370,0 106,3 99,8 95,3 90,3 82,6 74,2 68,1 61,6 54,2 46,4 1.7.2015 EN Official Journal of the European Union L 168/763Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) JT9D7Q LAmax D 34 850,0 110,0 103,8 99,4 94,7 87,2 78,7 72,7 66,0 58,6 50,8 JT9D7Q LAmax D 40 240,0 112,5 106,3 102,0 97,3 89,9 81,4 75,3 68,6 61,2 53,4 JT9D7Q LAmax D 44 940,0 115,3 109,1 104,8 100,0 92,6 84,2 78,0 71,4 63,9 56,1 JT9D7Q SEL A 8 560,0 103,6 99,5 96,6 93,5 88,1 81,7 77,0 71,6 65,5 58,9 JT9D7Q SEL A 14 000,0 105,1 100,9 97,8 94,3 88,7 82,3 77,6 72,4 66,4 59,9 JT9D7Q SEL D 24 370,0 108,1 103,9 100,9 97,5 92,1 86,0 81,5 76,5 70,7 64,4 JT9D7Q SEL D 34 850,0 111,8 107,9 105,0 101,9 96,7 90,5 86,1 80,9 75,1 68,8 JT9D7Q SEL D 40 240,0 114,3 110,4 107,6 104,5 99,4 93,2 88,7 83,5 77,7 71,4 JT9D7Q SEL D 44 940,0 117,1 113,2 110,4 107,2 102,1 96,0 91,4 86,3 80,4 74,1 JT9DBD LAmax A 8 000,0 106,5 99,5 94,5 89,0 79,8 69,1 61,2 53,2 44,9 36,3 JT9DBD LAmax A 14 000,0 111,0 104,0 99,0 93,5 84,3 73,6 65,7 57,7 49,4 40,8 JT9DBD LAmax D 20 000,0 114,3 107,2 102,1 96,5 87,1 76,9 69,8 62,3 54,2 45,4 JT9DBD LAmax D 28 000,0 116,4 109,3 104,2 98,5 89,0 79,1 72,3 65,0 57,0 48,0 JT9DBD LAmax D 36 000,0 117,9 110,8 105,7 100,0 90,5 80,6 73,8 66,5 58,5 49,7 JT9DBD SEL A 8 000,0 108,2 103,5 99,9 96,0 89,1 80,6 74,2 67,6 60,9 53,7 JT9DBD SEL A 14 000,0 113,2 108,5 104,9 101,0 94,1 85,6 79,2 72,6 65,9 58,7 JT9DBD SEL D 20 000,0 116,6 111,8 108,1 104,0 96,9 89,0 83,4 77,3 70,7 63,4 JT9DBD SEL D 28 000,0 118,7 113,9 110,2 106,0 98,8 91,2 85,9 80,0 73,5 66,2 JT9DBD SEL D 36 000,0 120,2 115,4 111,7 107,5 100,3 92,7 87,4 81,5 75,0 67,7 JT9DFL LAmax A 8 000,0 103,0 95,5 90,2 84,3 75,1 66,0 59,7 52,6 44,5 35,6 L 168/764 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) JT9DFL LAmax A 16 000,0 107,1 99,6 94,3 88,4 79,2 70,1 63,8 56,7 48,6 39,7 JT9DFL LAmax D 24 000,0 110,6 103,1 97,8 92,1 83,3 74,5 68,3 61,5 53,7 45,4 JT9DFL LAmax D 32 000,0 113,5 105,9 100,6 95,1 86,5 77,9 71,9 65,3 57,7 49,7 JT9DFL LAmax D 40 000,0 115,7 108,1 102,8 97,3 88,7 80,1 74,1 67,5 59,9 51,9 JT9DFL SEL A 8 000,0 102,3 97,8 94,3 90,5 84,4 77,7 72,9 67,3 60,7 53,3 JT9DFL SEL A 16 000,0 106,3 101,8 98,3 94,5 88,4 81,7 76,9 71,3 64,7 57,3 JT9DFL SEL D 24 000,0 109,4 105,1 101,7 98,0 92,2 85,8 81,2 75,9 69,7 62,8 JT9DFL SEL D 32 000,0 111,8 107,4 104,1 100,5 94,9 88,7 84,2 79,1 73,1 66,5 JT9DFL SEL D 40 000,0 113,8 109,4 106,1 102,5 96,9 90,7 86,2 81,1 75,1 68,5 O320D3 LAmax A 1 500,0 66,9 60,5 56,2 51,7 44,7 37,2 32,1 26,7 21,1 15,9 O320D3 LAmax A 1 600,0 68,1 61,7 57,4 52,9 45,9 38,4 33,2 27,7 21,9 16,6 O320D3 LAmax A 1 800,0 72,1 65,6 61,2 56,6 49,3 41,3 35,8 30,0 23,9 18,0 O320D3 LAmax D 2 150,0 79,8 73,1 68,6 63,9 56,2 47,9 42,2 36,1 29,7 23,1 O320D3 LAmax D 2 442,0 87,3 80,7 76,1 71,2 63,5 55,1 49,4 43,1 36,1 28,7 O320D3 LAmax D 2 600,0 88,8 82,1 77,5 72,6 64,7 56,2 50,2 43,8 36,7 29,3 O320D3 SEL A 1 500,0 69,0 65,6 62,8 60,2 56,0 51,3 48,0 44,5 41,3 38,2 O320D3 SEL A 1 600,0 70,4 67,1 64,6 62,0 57,7 53,0 49,6 45,9 42,3 38,9 O320D3 SEL A 1 800,0 74,1 70,5 68,0 65,3 60,7 55,5 51,8 47,8 43,8 39,9 O320D3 SEL D 2 150,0 80,4 76,9 74,3 71,4 66,5 60,9 57,0 52,7 48,1 43,7 O320D3 SEL D 2 442,0 87,9 84,2 81,5 78,5 73,4 67,9 63,9 59,5 54,4 48,9 1.7.2015 EN Official Journal of the European Union L 168/765Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) O320D3 SEL D 2 600,0 89,4 85,5 82,8 79,8 74,8 69,0 64,8 60,2 55,0 49,2 O470R LAmax A 169,0 73,3 67,1 62,9 58,6 51,8 44,6 39,6 34,1 28,1 21,8 O470R LAmax A 244,0 73,9 67,7 63,5 59,2 52,5 45,4 40,3 34,8 28,8 22,4 O470R LAmax D 533,0 87,5 81,2 77,0 72,7 65,7 58,2 52,7 46,6 39,7 32,3 O470R LAmax D 640,0 96,1 89,8 85,5 80,9 73,5 65,0 58,6 51,3 43,0 34,3 O470R SEL A 169,0 75,6 71,7 69,0 66,2 61,7 56,7 53,1 49,2 44,7 39,8 O470R SEL A 244,0 76,2 72,3 69,6 66,8 62,3 57,3 53,7 49,7 45,1 40,2 O470R SEL D 533,0 87,8 83,8 81,1 78,2 73,6 68,2 64,2 59,6 54,2 48,4 O470R SEL D 640,0 95,4 91,3 88,5 85,4 80,3 74,1 69,2 63,4 56,5 49,3 OLY593 LAmax A 10 000,0 115,8 109,2 104,6 99,8 92,0 83,2 76,5 68,8 60,3 50,7 OLY593 LAmax A 20 000,0 126,4 119,4 113,3 109,2 101,2 92,4 85,9 78,7 70,2 60,7 OLY593 LAmax D 20 000,0 126,4 119,4 113,3 109,2 101,2 92,4 85,9 78,7 70,2 60,7 OLY593 LAmax D 28 000,0 132,1 124,8 119,6 114,3 106,1 97,3 90,8 83,6 75,1 65,3 OLY593 LAmax D 32 000,0 134,0 126,7 121,4 116,0 107,8 98,9 92,4 85,2 76,7 67,3 OLY593 SEL A 10 000,0 117,7 113,4 110,3 107,0 101,5 94,8 89,6 83,5 76,5 68,3 OLY593 SEL A 20 000,0 130,3 125,5 122,0 118,3 112,6 106,1 101,1 95,3 88,3 80,3 OLY593 SEL D 20 000,0 130,3 125,5 122,0 118,3 112,6 106,1 101,1 95,3 88,3 80,3 OLY593 SEL D 28 000,0 136,4 131,3 127,6 123,8 118,0 111,4 106,4 100,6 93,7 85,7 OLY593 SEL D 32 000,0 138,4 133,2 129,4 125,5 119,6 113,0 108,0 102,2 95,3 87,4 PT6A114 LAmax A 400,0 90,0 83,6 79,4 75,0 68,0 60,4 54,8 48,3 40,5 31,7 L 168/766 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) PT6A114 LAmax A 427,0 90,0 83,6 79,4 75,0 68,0 60,4 54,8 48,3 40,5 31,7 PT6A114 LAmax A 463,0 90,3 84,0 79,7 75,2 68,2 60,6 55,1 48,7 41,1 32,6 PT6A114 LAmax D 1 009,0 88,2 82,0 77,8 73,5 66,7 59,1 53,5 47,1 39,4 30,8 PT6A114 LAmax D 1 899,0 90,0 83,8 79,7 75,4 68,7 61,4 56,1 50,1 43,1 35,4 PT6A114 SEL A 400,0 89,9 85,8 83,0 80,1 75,4 70,1 65,9 61,0 54,7 47,4 PT6A114 SEL A 427,0 89,9 85,8 83,0 80,1 75,4 70,1 65,9 61,0 54,7 47,4 PT6A114 SEL A 463,0 89,4 85,3 82,4 79,4 74,7 69,3 65,3 60,6 54,7 47,9 PT6A114 SEL D 1 009,0 87,7 83,8 81,1 78,3 73,7 68,4 64,3 59,4 53,2 46,1 PT6A114 SEL D 1 899,0 89,7 85,8 83,2 80,4 75,9 70,9 67,1 62,6 57,1 50,9 PT6A27 LAmax A 30,0 90,9 84,6 80,4 76,0 69,1 61,6 56,0 49,8 42,6 34,0 PT6A27 LAmax A 100,0 95,6 89,5 85,3 81,0 74,3 67,0 61,6 55,6 49,0 41,4 PT6A27 LAmax D 30,0 90,9 84,6 80,4 76,0 69,1 61,6 56,0 49,8 42,6 34,0 PT6A27 LAmax D 100,0 95,6 89,5 85,3 81,0 74,3 67,0 61,6 55,6 49,0 41,4 PT6A27 SEL A 30,0 91,3 87,2 84,4 81,6 76,9 71,7 67,6 62,9 57,2 50,0 PT6A27 SEL A 100,0 95,9 92,0 89,3 86,5 82,0 77,0 73,1 68,6 63,5 57,4 PT6A27 SEL D 30,0 91,3 87,2 84,4 81,6 76,9 71,7 67,6 62,9 57,2 50,0 PT6A27 SEL D 100,0 95,9 92,0 89,3 86,5 82,0 77,0 73,1 68,6 63,5 57,4 PT6A41 LAmax A 300,0 83,6 77,2 72,8 68,2 60,9 52,8 47,0 40,4 32,8 24,9 PT6A41 LAmax A 311,0 83,6 77,2 72,8 68,2 60,9 52,8 47,0 40,4 32,8 24,9 PT6A41 LAmax D 820,0 85,2 78,9 74,7 70,3 63,5 56,0 50,6 44,4 37,2 29,1 1.7.2015 EN Official Journal of the European Union L 168/767Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) PT6A41 LAmax D 1 153,0 87,2 81,0 76,9 72,6 65,9 58,6 53,4 47,5 40,6 32,9 PT6A41 SEL A 300,0 87,8 83,6 80,7 77,6 72,5 66,7 62,3 57,3 51,3 44,8 PT6A41 SEL A 311,0 87,8 83,6 80,7 77,6 72,5 66,7 62,3 57,3 51,3 44,8 PT6A41 SEL D 820,0 86,6 82,5 79,8 77,0 72,3 67,1 63,2 58,5 52,8 46,3 PT6A41 SEL D 1 153,0 88,6 84,7 82,0 79,2 74,8 69,8 66,0 61,6 56,2 50,0 PT6A45 LAmax A 35,0 87,2 81,0 76,7 72,4 65,1 57,7 52,9 48,0 41,9 35,1 PT6A45 LAmax A 65,0 87,8 81,4 77,0 72,5 64,9 57,4 52,4 47,4 41,7 35,5 PT6A45 LAmax D 65,0 87,8 81,4 77,0 72,5 64,9 57,4 52,4 47,4 41,7 35,5 PT6A45 LAmax D 100,0 94,9 88,6 84,4 80,0 72,6 65,2 60,3 55,4 49,4 42,4 PT6A45 SEL A 35,0 88,0 84,0 81,3 78,5 74,0 69,2 65,6 61,6 57,0 51,6 PT6A45 SEL A 65,0 88,5 84,4 81,5 78,5 73,7 68,5 64,8 60,9 56,8 52,0 PT6A45 SEL D 65,0 88,5 84,4 81,5 78,5 73,7 68,5 64,8 60,9 56,8 52,0 PT6A45 SEL D 100,0 95,1 91,1 88,4 85,5 81,0 76,1 72,4 68,4 63,8 58,4 PT6A50 LAmax A 35,0 83,9 78,2 74,0 68,8 60,7 51,8 45,5 38,6 31,4 24,2 PT6A50 LAmax A 40,0 87,4 81,7 77,5 72,4 64,2 55,5 49,0 42,1 34,4 26,7 PT6A50 LAmax D 80,0 84,7 78,5 74,4 69,8 62,5 54,0 48,1 41,3 34,0 26,4 PT6A50 LAmax D 100,0 86,9 80,7 76,6 72,0 64,7 56,2 50,2 43,5 36,4 29,3 PT6A50 SEL A 35,0 85,7 82,3 79,6 76,0 70,2 63,6 58,9 53,5 47,9 42,2 PT6A50 SEL A 40,0 89,2 85,8 83,1 79,6 73,7 67,3 62,4 57,0 50,9 44,7 PT6A50 SEL D 80,0 86,5 82,6 80,0 77,0 72,0 65,8 61,5 56,2 50,5 44,4 L 168/768 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) PT6A50 SEL D 100,0 88,7 84,8 82,2 79,2 74,2 68,0 63,6 58,4 52,9 47,3 PT6A67 LAmax A 400,0 87,8 81,2 76,8 72,2 64,9 56,7 50,6 43,5 35,4 27,1 PT6A67 LAmax A 600,0 89,1 82,4 77,9 73,3 66,1 58,1 52,3 45,7 37,8 29,2 PT6A67 LAmax D 1 000,0 90,2 83,7 79,2 74,5 67,0 58,8 52,9 46,7 39,9 33,2 PT6A67 LAmax D 1 100,0 90,2 83,7 79,2 74,5 67,0 58,8 52,9 46,7 39,9 33,2 PT6A67 LAmax D 1 600,0 87,9 81,5 77,2 72,7 65,7 58,1 52,7 46,9 40,5 34,0 PT6A67 LAmax D 1 700,0 87,9 81,5 77,2 72,7 65,7 58,1 52,7 46,9 40,5 34,0 PT6A67 SEL A 400,0 90,6 86,4 83,9 81,0 76,3 70,7 66,2 60,9 54,6 48,2 PT6A67 SEL A 600,0 90,8 86,6 83,9 80,9 76,3 71,0 66,8 61,8 55,7 48,8 PT6A67 SEL D 1 000,0 92,8 88,9 86,3 83,3 78,4 72,7 68,5 63,9 58,8 53,6 PT6A67 SEL D 1 100,0 92,8 88,9 86,3 83,3 78,4 72,7 68,5 63,9 58,8 53,6 PT6A67 SEL D 1 600,0 89,4 85,7 83,2 80,5 76,0 70,9 67,2 63,1 58,5 53,7 PT6A67 SEL D 1 700,0 89,4 85,7 83,2 80,5 76,0 70,9 67,2 63,1 58,5 53,7 PW119C LAmax A 108,0 91,0 84,0 79,0 73,6 64,7 55,1 48,4 41,1 33,2 25,4 PW119C LAmax A 465,0 91,8 84,6 79,4 73,7 64,1 53,6 46,5 39,0 31,1 22,9 PW119C LAmax D 3 412,0 87,2 80,6 76,2 71,5 64,3 56,5 51,0 44,9 38,3 31,6 PW119C LAmax D 4 300,0 88,8 82,4 78,2 73,8 67,0 59,9 55,0 49,7 43,9 37,8 PW119C LAmax D 4 301,0 88,8 82,4 78,2 73,8 67,0 59,9 55,0 49,7 43,9 37,8 PW119C SEL A 108,0 95,0 90,3 86,8 82,8 76,2 68,8 63,6 57,8 51,4 45,1 PW119C SEL A 465,0 95,3 90,4 86,7 82,5 75,1 66,9 61,3 55,3 48,8 42,2 1.7.2015 EN Official Journal of the European Union L 168/769Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) PW119C SEL D 3 412,0 90,0 85,7 82,7 79,6 74,6 69,1 65,0 60,5 55,4 50,1 PW119C SEL D 4 300,0 90,2 86,0 83,2 80,3 75,8 71,0 67,6 63,8 59,5 54,8 PW119C SEL D 4 301,0 90,2 86,0 83,2 80,3 75,8 71,0 67,6 63,8 59,5 54,8 PW120 LAmax A 35,0 87,1 80,3 75,5 70,5 62,4 54,0 48,9 43,8 39,1 34,8 PW120 LAmax A 40,0 90,0 83,7 79,2 74,3 66,7 59,0 54,0 48,8 43,4 38,1 PW120 LAmax D 90,0 82,8 76,9 72,9 68,7 62,8 56,3 51,8 47,3 42,3 37,6 PW120 LAmax D 100,0 85,2 79,4 75,8 71,9 65,9 59,7 55,3 51,0 46,2 41,6 PW120 LAmax D 150,0 90,2 84,4 80,8 76,9 70,9 64,7 60,3 56,0 51,2 46,6 PW120 SEL A 35,0 88,9 84,4 81,1 77,7 71,9 65,8 62,3 58,7 55,6 52,8 PW120 SEL A 40,0 91,8 87,8 84,8 81,5 76,2 70,8 67,4 63,7 59,9 56,1 PW120 SEL D 90,0 84,6 81,0 78,5 75,9 72,3 68,1 65,2 62,2 58,8 55,6 PW120 SEL D 100,0 87,0 83,5 81,4 79,1 75,4 71,5 68,7 65,9 62,7 59,6 PW120 SEL D 150,0 92,0 88,5 86,4 84,1 80,4 76,5 73,7 70,9 67,7 64,6 PW2037 LAmax A 5 000,0 93,3 86,7 82,1 77,1 69,2 60,2 53,4 46,2 38,2 30,2 PW2037 LAmax A 12 000,0 97,8 90,9 86,1 80,9 72,6 63,4 56,5 49,0 40,7 32,4 PW2037 LAmax D 13 000,0 95,6 89,2 84,6 79,6 71,4 62,1 55,2 47,6 39,3 30,8 PW2037 LAmax D 24 000,0 99,7 93,1 88,4 83,2 75,2 66,1 59,8 53,3 46,2 39,0 PW2037 LAmax D 30 000,0 101,5 95,5 91,1 86,4 78,8 70,1 63,7 57,0 49,5 41,9 PW2037 LAmax D 36 000,0 103,7 98,4 94,6 90,5 83,8 75,5 68,9 61,6 53,2 44,6 PW2037 SEL A 5 000,0 95,1 90,8 87,7 84,3 78,7 72,0 66,8 61,1 54,7 48,2 L 168/770 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) PW2037 SEL A 12 000,0 99,6 95,0 91,7 88,1 82,1 75,2 69,9 63,9 57,2 50,4 PW2037 SEL D 13 000,0 97,4 93,3 90,2 86,8 80,9 73,9 68,6 62,5 55,8 48,8 PW2037 SEL D 24 000,0 101,5 97,2 94,0 90,4 84,7 77,9 73,2 68,2 62,7 57,0 PW2037 SEL D 30 000,0 103,3 99,6 96,7 93,6 88,3 81,9 77,1 71,9 66,0 59,9 PW2037 SEL D 36 000,0 105,5 102,5 100,2 97,7 93,3 87,3 82,3 76,5 69,7 62,6 PW306C LAmax A 500,0 84,2 77,2 72,2 66,8 58,1 48,7 42,1 35,1 27,7 20,3 PW306C LAmax A 1 000,0 85,4 78,1 73,0 67,6 58,8 49,4 42,8 35,9 28,5 21,3 PW306C LAmax D 1 500,0 86,2 79,5 74,7 69,4 60,7 51,2 44,5 37,2 29,5 21,8 PW306C LAmax D 3 500,0 95,2 88,8 84,1 78,9 70,3 60,8 54,1 46,9 39,1 31,3 PW306C LAmax D 5 500,0 101,4 95,1 90,4 85,2 76,5 66,8 60,0 52,6 44,6 36,5 PW306C SEL A 500,0 85,4 81,5 78,6 75,2 69,3 62,7 57,8 52,6 46,8 41,0 PW306C SEL A 1 000,0 86,5 82,4 79,3 75,8 69,9 63,3 58,5 53,4 47,8 42,1 PW306C SEL D 1 500,0 85,8 82,3 79,5 76,2 70,6 64,0 59,1 53,8 47,9 41,9 PW306C SEL D 3 500,0 94,9 91,3 88,4 85,2 79,5 72,9 68,1 62,9 57,1 51,2 PW306C SEL D 5 500,0 101,3 97,9 95,1 91,9 86,3 79,8 75,0 69,7 64,0 58,1 PW4056 LAmax A 7 000,0 99,8 92,4 87,3 82,0 74,1 65,7 59,6 52,8 45,8 39,1 PW4056 LAmax A 10 000,0 99,9 92,4 87,3 82,0 74,2 65,8 59,7 52,8 45,8 39,0 PW4056 LAmax A 13 000,0 100,5 92,9 87,7 82,4 74,5 66,1 60,0 53,1 46,1 39,4 PW4056 LAmax A 16 000,0 101,4 93,6 88,2 82,9 74,9 66,5 60,4 53,6 46,6 40,0 PW4056 LAmax D 20 000,0 101,9 94,4 89,3 83,9 75,7 67,7 61,9 55,5 49,1 42,9 1.7.2015 EN Official Journal of the European Union L 168/771Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) PW4056 LAmax D 26 000,0 103,4 96,2 91,2 86,1 78,0 69,7 64,0 57,6 51,1 44,9 PW4056 LAmax D 32 000,0 105,1 98,0 93,2 88,1 80,2 71,8 66,0 59,7 53,2 47,0 PW4056 LAmax D 38 000,0 107,0 100,1 95,3 90,4 82,5 74,1 68,3 61,9 55,4 49,2 PW4056 LAmax D 44 000,0 109,5 102,7 98,0 93,1 85,3 76,9 71,2 64,8 58,3 52,2 PW4056 LAmax D 50 000,0 113,3 106,5 101,7 96,9 89,1 81,0 75,3 68,9 62,5 56,4 PW4056 SEL A 7 000,0 102,9 98,2 94,9 91,5 86,1 80,1 75,6 70,5 65,2 60,1 PW4056 SEL A 10 000,0 103,3 98,6 95,2 91,7 86,3 80,3 75,8 70,6 65,2 60,1 PW4056 SEL A 13 000,0 103,9 99,1 95,7 92,1 86,6 80,6 76,1 70,9 65,6 60,6 PW4056 SEL A 16 000,0 104,6 99,8 96,3 92,6 87,0 80,9 76,5 71,4 66,3 61,4 PW4056 SEL D 20 000,0 104,5 99,9 96,5 92,7 86,9 81,1 77,1 72,6 68,0 63,6 PW4056 SEL D 26 000,0 105,0 100,7 97,5 94,1 88,7 83,0 79,0 74,5 70,0 65,6 PW4056 SEL D 32 000,0 106,1 102,0 99,0 95,8 90,6 85,0 81,0 76,5 72,0 67,6 PW4056 SEL D 38 000,0 107,6 103,6 100,8 97,7 92,7 87,2 83,3 78,8 74,3 69,9 PW4056 SEL D 44 000,0 109,9 106,0 103,2 100,2 95,4 90,0 86,2 81,8 77,3 73,0 PW4056 SEL D 50 000,0 113,5 109,6 106,9 104,0 99,2 94,2 90,5 86,1 81,7 77,5 PW4158 LAmax A 4 000,0 97,0 90,1 84,8 78,9 70,6 62,1 56,0 49,2 41,5 33,6 PW4158 LAmax A 12 000,0 99,5 92,3 86,8 81,1 72,4 63,4 57,2 50,2 42,5 34,5 PW4158 LAmax D 23 000,0 104,9 95,7 89,4 83,0 73,2 62,8 56,1 49,2 41,7 34,0 PW4158 LAmax D 32 000,0 107,8 99,8 94,4 88,6 79,1 68,1 61,4 54,6 47,0 39,0 PW4158 LAmax D 41 000,0 108,7 101,0 95,9 90,3 81,0 71,5 65,1 58,2 50,5 42,4 L 168/772 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) PW4158 LAmax D 50 000,0 111,5 103,9 98,9 93,7 85,4 76,6 70,4 63,7 56,0 47,6 PW4158 SEL A 4 000,0 99,7 94,9 91,6 88,2 82,7 76,6 72,0 66,8 60,8 54,3 PW4158 SEL A 12 000,0 102,5 97,8 94,1 90,2 84,2 77,8 73,1 67,8 61,6 55,1 PW4158 SEL D 23 000,0 104,1 98,5 94,2 90,0 83,7 76,8 71,9 66,8 61,0 54,7 PW4158 SEL D 32 000,0 106,1 101,4 97,6 94,0 88,1 81,6 77,0 72,0 66,2 60,0 PW4158 SEL D 41 000,0 107,3 103,1 99,7 96,4 91,0 85,0 80,6 75,7 70,1 63,8 PW4158 SEL D 50 000,0 110,6 106,5 103,4 100,2 95,1 89,5 85,3 80,4 74,6 68,1 PW4460 LAmax A 9 300,0 99,2 92,8 87,4 82,4 74,1 65,9 59,6 53,2 46,6 40,4 PW4460 LAmax A 22 400,0 102,5 95,6 90,5 84,9 76,3 67,5 61,2 54,8 48,1 41,7 PW4460 LAmax D 24 960,0 101,9 94,1 89,1 84,0 76,2 67,6 61,3 54,8 47,2 40,0 PW4460 LAmax D 37 100,0 104,4 97,1 92,4 87,5 80,2 71,9 65,8 59,1 51,7 44,7 PW4460 LAmax D 49 010,0 107,4 100,9 96,4 91,9 84,7 76,9 70,8 64,4 56,7 50,2 PW4460 LAmax D 53 830,0 109,6 103,2 98,6 94,0 87,3 79,4 73,8 67,1 59,7 53,2 PW4460 SEL A 9 300,0 101,0 96,9 93,0 89,6 83,6 77,7 73,0 68,1 63,1 58,4 PW4460 SEL A 22 400,0 104,3 99,7 96,1 92,1 85,8 79,3 74,6 69,7 64,6 59,7 PW4460 SEL D 24 960,0 103,7 98,2 94,7 91,2 85,7 79,4 74,7 69,7 63,7 58,0 PW4460 SEL D 37 100,0 106,2 101,2 98,0 94,7 89,7 83,7 79,2 74,0 68,2 62,7 PW4460 SEL D 49 010,0 109,2 105,0 102,0 99,1 94,2 88,7 84,2 79,3 73,2 68,2 PW4460 SEL D 53 830,0 111,4 107,3 104,2 101,2 96,8 91,2 87,2 82,0 76,2 71,2 PW530A LAmax A 500,0 88,7 81,1 75,8 70,1 60,9 51,1 44,3 37,1 29,4 21,9 1.7.2015 EN Official Journal of the European Union L 168/773Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) PW530A LAmax A 800,0 90,3 82,7 77,5 71,8 62,9 53,3 46,7 39,7 32,3 25,0 PW530A LAmax D 1 200,0 94,0 87,0 81,9 76,3 67,2 57,2 50,1 42,6 34,5 26,4 PW530A LAmax D 1 600,0 95,8 89,1 84,2 78,9 70,0 60,3 53,4 45,9 38,0 30,0 PW530A LAmax D 2 000,0 98,5 91,8 86,8 81,4 72,4 62,5 55,5 47,9 39,8 31,7 PW530A LAmax D 2 400,0 100,2 93,6 88,8 83,5 74,7 65,0 58,1 50,7 42,8 34,8 PW530A SEL A 500,0 88,6 84,0 80,7 77,1 71,1 64,4 59,7 54,6 49,2 43,7 PW530A SEL A 800,0 90,4 85,8 82,5 78,9 73,0 66,6 62,0 57,1 51,8 46,6 PW530A SEL D 1 200,0 92,2 88,0 84,8 81,3 75,3 68,5 63,7 58,4 52,6 46,9 PW530A SEL D 1 600,0 95,5 91,5 88,4 84,8 78,8 71,9 66,9 61,4 55,5 49,5 PW530A SEL D 2 000,0 98,8 94,4 91,2 87,5 81,4 74,6 69,7 64,5 58,7 53,0 PW530A SEL D 2 400,0 100,2 96,4 93,5 90,1 84,2 77,4 72,5 67,0 61,1 55,0 PW545A LAmax A 550,0 91,5 84,2 78,9 73,1 63,6 53,3 46,0 38,2 29,9 21,6 PW545A LAmax A 750,0 93,0 85,6 80,3 74,5 65,1 54,7 47,4 39,6 31,3 23,0 PW545A LAmax D 1 750,0 94,4 87,6 82,7 77,3 68,3 58,5 51,5 44,0 35,9 27,8 PW545A LAmax D 2 000,0 94,6 87,6 82,5 77,1 68,3 58,7 52,1 45,0 37,5 30,0 PW545A LAmax D 2 500,0 96,4 89,3 84,3 78,9 70,1 60,6 53,9 46,8 39,3 31,8 PW545A LAmax D 3 000,0 97,4 90,8 86,1 81,0 72,6 63,5 57,1 50,2 42,8 35,5 PW545A LAmax D 3 500,0 99,7 93,2 88,5 83,4 75,1 66,0 59,6 52,8 45,6 38,3 PW545A SEL A 550,0 92,1 87,1 83,4 79,1 71,7 63,4 57,4 50,8 43,6 36,4 PW545A SEL A 750,0 93,6 88,6 84,8 80,5 73,2 64,9 58,9 52,4 45,3 38,1 PW545A SEL D 1 750,0 94,8 90,3 86,9 83,0 76,3 68,7 63,2 57,2 50,6 44,0 L 168/774 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) PW545A SEL D 2 000,0 95,9 91,1 87,5 83,6 77,1 69,8 64,7 59,1 53,1 47,1 PW545A SEL D 2 500,0 98,0 93,2 89,6 85,7 79,2 71,9 66,8 61,2 55,2 49,2 PW545A SEL D 3 000,0 98,7 94,4 91,2 87,6 81,5 74,6 69,7 64,3 58,5 52,6 PW545A SEL D 3 500,0 101,1 96,8 93,6 90,1 84,0 77,2 72,3 67,0 61,3 55,5 PW610F LAmax A 79,0 77,0 69,5 64,6 59,8 52,4 44,4 38,6 32,1 24,5 16,3 PW610F LAmax A 112,0 77,3 69,8 64,9 59,9 52,4 44,3 38,5 32,0 24,5 16,2 PW610F LAmax A 160,0 77,9 70,4 65,4 60,3 52,5 44,4 38,5 32,0 24,5 16,2 PW610F LAmax A 208,0 78,5 71,0 66,0 60,8 52,9 44,6 38,7 32,1 24,6 16,3 PW610F LAmax A 262,0 79,2 71,8 66,8 61,5 53,5 45,0 39,0 32,4 24,8 16,6 PW610F LAmax A 328,0 80,1 72,9 67,9 62,7 54,5 45,8 39,7 32,9 25,2 17,0 PW610F LAmax A 404,0 81,2 74,3 69,5 64,3 56,1 47,1 40,7 33,8 26,0 17,7 PW610F LAmax D 489,0 83,7 76,9 72,1 66,9 58,4 48,9 42,1 34,6 26,1 17,0 PW610F LAmax D 587,0 86,2 79,1 74,2 68,9 60,4 50,9 44,0 36,4 27,8 18,7 PW610F LAmax D 689,0 88,3 81,2 76,2 70,9 62,3 52,9 46,0 38,3 29,6 20,4 PW610F LAmax D 807,0 90,3 83,3 78,3 73,1 64,6 55,2 48,3 40,5 31,8 22,6 PW610F LAmax D 910,0 91,7 84,8 80,0 74,9 66,5 57,1 50,2 42,5 33,7 24,4 PW610F LAmax D 935,0 91,9 85,1 80,4 75,3 67,0 57,6 50,7 43,0 34,2 24,9 PW610F SEL A 79,0 78,5 74,3 71,3 68,3 63,5 58,1 54,0 49,2 43,4 36,9 PW610F SEL A 112,0 78,7 74,4 71,5 68,4 63,5 58,1 54,0 49,1 43,4 36,8 PW610F SEL A 160,0 79,0 74,7 71,8 68,7 63,7 58,2 54,0 49,2 43,4 36,8 PW610F SEL A 208,0 79,5 75,2 72,3 69,2 64,1 58,4 54,2 49,3 43,5 36,9 1.7.2015 EN Official Journal of the European Union L 168/775Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) PW610F SEL A 262,0 80,1 75,9 72,9 69,8 64,7 58,9 54,7 49,7 43,8 37,2 PW610F SEL A 328,0 81,0 76,9 74,0 70,8 65,7 59,8 55,5 50,4 44,4 37,7 PW610F SEL A 404,0 82,2 78,3 75,5 72,4 67,2 61,3 56,8 51,6 45,4 38,6 PW610F SEL D 489,0 83,4 79,6 76,8 73,6 68,4 62,1 57,3 51,7 44,9 37,5 PW610F SEL D 587,0 85,7 81,9 78,9 75,7 70,4 64,2 59,4 53,8 47,0 39,6 PW610F SEL D 689,0 87,9 84,1 81,0 77,7 72,4 66,3 61,5 55,9 49,2 41,7 PW610F SEL D 807,0 90,1 86,3 83,4 80,1 74,9 68,7 64,0 58,4 51,7 44,1 PW610F SEL D 910,0 91,8 88,1 85,3 82,2 77,0 70,8 66,1 60,5 53,7 46,1 PW610F SEL D 935,0 92,2 88,4 85,7 82,7 77,5 71,3 66,6 60,9 54,2 46,6 PW615F LAmax A 300,0 82,8 75,7 70,6 65,1 56,1 46,3 39,5 32,2 24,4 16,6 PW615F LAmax A 500,0 87,1 79,9 74,7 69,0 59,8 49,7 42,6 35,0 26,9 18,8 PW615F LAmax D 700,0 90,2 83,5 78,6 73,1 64,1 54,0 46,9 39,2 31,0 22,7 PW615F LAmax D 900,0 94,8 87,7 82,6 77,0 67,7 57,5 50,3 42,5 34,2 25,9 PW615F LAmax D 1 100,0 96,4 89,8 85,0 79,6 70,6 60,5 53,4 45,7 37,3 28,9 PW615F LAmax D 1 300,0 97,4 91,1 86,4 81,2 72,5 62,7 55,8 48,3 40,2 32,0 PW615F SEL A 300,0 85,5 81,7 78,7 75,3 69,5 62,8 58,0 52,7 46,9 41,1 PW615F SEL A 500,0 87,0 82,9 79,8 76,3 70,4 63,8 59,0 53,9 48,3 42,6 PW615F SEL D 700,0 89,6 85,7 82,6 79,0 73,0 65,9 60,8 55,2 49,1 42,8 PW615F SEL D 900,0 92,9 89,0 86,0 82,5 76,5 69,6 64,6 59,2 53,2 47,1 PW615F SEL D 1 100,0 95,6 92,0 89,1 85,7 79,8 73,0 68,0 62,5 56,5 50,4 L 168/776 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) PW615F SEL D 1 300,0 97,4 94,1 91,3 88,1 82,4 75,7 70,8 65,4 59,4 53,3 RAISQP LAmax A 23,0 77,2 70,0 65,1 59,9 51,5 42,3 36,2 30,0 23,6 17,9 RAISQP LAmax A 30,0 78,3 71,3 67,4 61,7 53,9 45,6 39,8 33,6 27,0 20,1 RAISQP LAmax D 60,0 84,7 78,1 73,6 68,9 61,5 53,8 48,4 42,6 36,3 29,8 RAISQP LAmax D 85,0 89,2 82,7 78,4 74,0 67,2 60,1 55,3 50,2 44,6 38,7 RAISQP LAmax D 100,0 96,8 90,5 86,3 82,1 75,4 68,3 63,3 57,7 51,3 44,6 RAISQP SEL A 23,0 82,3 77,9 74,7 71,4 65,5 59,2 54,8 50,1 45,6 41,3 RAISQP SEL A 30,0 82,6 78,6 76,3 72,7 67,6 61,8 57,6 52,9 48,2 43,9 RAISQP SEL D 60,0 87,6 84,1 81,6 78,8 74,1 68,8 65,0 60,8 56,1 51,4 RAISQP SEL D 85,0 92,3 88,6 86,1 83,4 79,2 74,7 71,3 68,0 63,9 60,1 RAISQP SEL D 100,0 97,8 94,5 92,3 90,0 86,3 82,0 78,9 75,2 70,9 66,0 RB183 LAmax A 1 798,0 94,7 87,6 82,6 77,6 69,3 60,8 54,7 47,4 38,9 29,9 RB183 LAmax A 2 698,0 95,6 89,1 84,5 79,8 72,3 64,0 57,9 50,6 42,0 32,9 RB183 LAmax A 3 147,0 98,1 91,3 86,4 81,6 74,2 65,6 59,5 52,2 43,7 34,8 RB183 LAmax A 3 597,0 98,7 92,2 87,3 82,6 75,6 67,2 61,1 53,8 45,3 36,3 RB183 LAmax A 4 496,0 100,4 94,3 90,1 85,4 78,8 70,4 64,3 57,0 48,5 39,5 RB183 LAmax D 4 496,0 101,6 95,0 90,6 85,8 78,6 70,9 65,2 58,5 50,0 39,6 RB183 LAmax D 10 116,0 119,8 113,4 108,9 104,2 96,9 89,3 83,5 76,9 68,4 58,0 RB183 SEL A 1 798,0 96,5 91,7 88,2 84,8 78,8 72,6 68,1 62,3 55,4 47,9 RB183 SEL A 2 698,0 97,4 93,2 90,1 87,0 81,8 75,8 71,3 65,5 58,5 50,9 RB183 SEL A 3 147,0 99,9 95,4 92,0 88,8 83,7 77,4 72,9 67,1 60,2 52,8 1.7.2015 EN Official Journal of the European Union L 168/777Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) RB183 SEL A 3 597,0 100,5 96,3 92,9 89,8 85,1 79,0 74,5 68,7 61,8 54,3 RB183 SEL A 4 496,0 102,2 98,4 95,7 92,6 88,3 82,2 77,7 71,9 65,0 57,5 RB183 SEL D 4 496,0 103,4 99,1 96,2 93,0 88,1 82,7 78,6 73,4 66,5 57,6 RB183 SEL D 10 116,0 121,6 117,5 114,5 111,4 106,4 101,1 96,9 91,8 84,9 76,0 RB183P LAmax A 1 798,0 93,7 86,9 82,3 77,3 69,1 60,6 54,2 46,5 37,4 27,6 RB183P LAmax A 2 698,0 94,0 87,9 83,8 79,5 72,0 63,5 57,0 49,3 40,2 30,5 RB183P LAmax A 3 147,0 97,0 90,5 85,9 81,3 73,7 64,9 58,5 50,8 41,9 32,4 RB183P LAmax A 3 597,0 97,8 91,5 87,2 82,5 74,9 66,4 59,9 52,2 43,3 33,7 RB183P LAmax A 4 496,0 99,9 93,8 89,6 85,3 77,8 69,3 62,8 55,1 46,1 36,4 RB183P LAmax D 4 496,0 101,5 94,6 89,9 84,9 77,4 69,3 63,3 56,3 47,5 36,5 RB183P LAmax D 10 116,0 116,3 109,6 104,9 100,1 92,5 84,4 78,4 71,4 62,5 51,5 RB183P SEL A 1 798,0 95,5 91,0 87,9 84,5 78,6 72,4 67,6 61,4 53,9 45,6 RB183P SEL A 2 698,0 95,8 92,0 89,4 86,7 81,5 75,3 70,4 64,2 56,7 48,5 RB183P SEL A 3 147,0 98,8 94,6 91,5 88,5 83,2 76,7 71,9 65,7 58,4 50,4 RB183P SEL A 3 597,0 99,6 95,6 92,8 89,7 84,4 78,2 73,3 67,1 59,8 51,7 RB183P SEL A 4 496,0 101,7 97,9 95,2 92,5 87,3 81,1 76,2 70,0 62,6 54,4 RB183P SEL D 4 496,0 103,3 98,7 95,5 92,1 86,9 81,1 76,7 71,2 64,0 54,5 RB183P SEL D 10 116,0 118,1 113,7 110,5 107,3 102,0 96,2 91,8 86,3 79,0 69,5 RB2112 LAmax A 8 000,0 99,2 92,0 86,6 81,0 72,1 63,0 56,5 49,1 40,8 32,5 RB2112 LAmax A 14 000,0 102,8 95,8 90,7 85,3 76,8 67,9 61,5 54,2 46,1 38,1 L 168/778 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) RB2112 LAmax D 20 000,0 104,8 97,4 93,0 87,8 79,6 70,7 64,4 57,2 49,2 41,4 RB2112 LAmax D 28 000,0 106,7 99,9 95,1 90,0 82,0 73,2 66,9 59,8 51,9 44,1 RB2112 LAmax D 36 000,0 108,3 101,6 97,0 92,0 84,2 75,4 69,2 62,2 54,3 46,7 RB2112 SEL A 8 000,0 100,7 95,5 91,7 87,5 81,1 74,0 68,8 63,0 56,3 49,7 RB2112 SEL A 14 000,0 104,8 100,0 96,4 92,5 86,4 79,5 74,5 68,8 62,3 55,8 RB2112 SEL D 20 000,0 107,3 102,6 99,1 95,5 89,5 82,8 77,8 72,3 65,8 59,5 RB2112 SEL D 28 000,0 109,8 105,3 101,9 98,5 92,7 86,1 81,2 75,8 69,5 63,2 RB2112 SEL D 36 000,0 111,4 107,1 103,8 100,5 94,8 88,3 83,5 78,1 71,9 65,6 RDA532 LAmax A 32,0 96,4 88,7 82,9 76,2 65,3 55,1 48,3 41,3 34,1 26,4 RDA532 LAmax A 73,0 98,2 91,1 86,2 81,2 73,6 65,9 60,5 54,7 48,2 40,7 RDA532 LAmax D 73,0 98,2 91,1 86,2 81,2 73,6 65,9 60,5 54,7 48,2 40,7 RDA532 LAmax D 100,0 98,6 92,2 87,8 83,4 76,4 68,9 63,4 57,3 50,3 42,0 RDA532 SEL A 32,0 98,9 93,5 89,1 84,0 75,3 67,3 62,0 56,5 50,8 44,6 RDA532 SEL A 73,0 100,2 95,4 92,0 88,4 83,1 77,7 73,8 69,5 64,5 58,5 RDA532 SEL D 73,0 100,2 95,4 92,0 88,4 83,1 77,7 73,8 69,5 64,5 58,5 RDA532 SEL D 100,0 101,3 97,2 94,3 91,4 86,7 81,4 77,5 72,8 67,3 60,6 RR535E LAmax A 6 000,0 91,9 84,7 80,1 75,2 67,4 58,6 52,1 45,1 38,1 31,4 RR535E LAmax A 7 000,0 92,0 84,9 80,3 75,4 67,6 58,8 52,4 45,4 38,4 31,8 RR535E LAmax A 8 000,0 92,2 85,2 80,6 75,6 67,8 59,0 52,7 45,8 38,8 32,2 RR535E LAmax A 9 000,0 92,5 85,5 80,8 75,9 68,0 59,3 53,0 46,2 39,2 32,7 1.7.2015 EN Official Journal of the European Union L 168/779Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) RR535E LAmax D 10 000,0 91,0 84,0 79,7 75,1 67,5 59,1 53,0 46,3 39,4 33,0 RR535E LAmax D 15 000,0 95,7 87,9 83,1 78,4 70,8 62,3 56,3 49,8 43,1 36,8 RR535E LAmax D 20 000,0 99,1 91,1 86,3 81,5 73,8 65,4 59,5 53,0 46,4 40,1 RR535E LAmax D 25 000,0 101,6 93,9 89,1 84,3 76,7 68,3 62,4 55,9 49,2 43,0 RR535E LAmax D 30 000,0 103,7 96,5 91,9 87,2 79,6 71,2 65,3 58,7 52,0 45,8 RR535E LAmax D 35 000,0 106,2 100,3 96,1 91,6 84,1 75,8 69,7 63,0 56,2 49,9 RR535E SEL A 6 000,0 95,9 90,9 87,8 84,6 79,2 72,9 68,1 62,9 57,6 52,5 RR535E SEL A 7 000,0 95,8 91,0 88,0 84,7 79,3 73,1 68,4 63,2 58,0 53,0 RR535E SEL A 8 000,0 95,9 91,2 88,2 84,9 79,6 73,4 68,7 63,6 58,4 53,5 RR535E SEL A 9 000,0 96,0 91,5 88,5 85,2 79,8 73,7 69,1 64,0 58,9 54,1 RR535E SEL D 10 000,0 93,9 89,5 86,4 83,5 78,3 72,4 68,0 63,0 57,9 53,2 RR535E SEL D 15 000,0 98,4 93,9 90,7 87,5 82,1 76,1 71,8 67,0 62,1 57,6 RR535E SEL D 20 000,0 101,6 97,1 94,0 90,8 85,4 79,4 75,1 70,4 65,7 61,2 RR535E SEL D 25 000,0 104,0 99,7 96,6 93,5 88,2 82,3 78,1 73,5 68,8 64,4 RR535E SEL D 30 000,0 106,0 101,8 98,8 95,9 90,8 85,1 81,0 76,5 71,8 67,5 RR535E SEL D 35 000,0 108,3 104,5 101,8 99,4 94,6 89,4 85,4 80,9 76,2 71,9 SPEYHK LAmax A 1 000,0 86,5 80,4 76,1 71,5 64,1 56,3 50,8 45,0 38,9 32,8 SPEYHK LAmax A 2 000,0 90,6 84,5 80,2 75,6 68,2 60,4 54,9 49,1 43,0 36,9 SPEYHK LAmax A 4 000,0 98,8 92,7 88,4 83,8 76,4 68,6 63,1 57,3 51,2 45,1 SPEYHK LAmax A 6 000,0 108,7 102,6 98,3 93,7 86,3 78,5 73,0 67,2 61,1 55,0 L 168/780 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) SPEYHK LAmax A 8 000,0 113,5 107,4 103,1 98,5 91,1 83,3 77,8 72,0 65,9 59,8 SPEYHK LAmax A 10 000,0 119,4 113,3 109,0 104,4 97,0 89,2 83,7 77,9 71,8 65,7 SPEYHK LAmax D 1 000,0 86,5 80,4 76,1 71,5 64,1 56,3 50,8 45,0 38,9 32,8 SPEYHK LAmax D 2 000,0 90,6 84,5 80,2 75,6 68,2 60,4 54,9 49,1 43,0 36,9 SPEYHK LAmax D 4 000,0 98,8 92,7 88,4 83,8 76,4 68,6 63,1 57,3 51,2 45,1 SPEYHK LAmax D 6 000,0 108,7 102,6 98,3 93,7 86,3 78,5 73,0 67,2 61,1 55,0 SPEYHK LAmax D 8 000,0 113,5 107,4 103,1 98,5 91,1 83,3 77,8 72,0 65,9 59,8 SPEYHK LAmax D 10 000,0 119,4 113,3 109,0 104,4 97,0 89,2 83,7 77,9 71,8 65,7 SPEYHK SEL A 1 000,0 89,4 85,5 82,5 79,1 73,3 66,8 62,1 56,9 51,3 45,6 SPEYHK SEL A 2 000,0 93,5 89,6 86,6 83,2 77,4 70,9 66,2 61,0 55,4 49,7 SPEYHK SEL A 4 000,0 101,7 97,8 94,8 91,4 85,6 79,1 74,4 69,2 63,6 57,9 SPEYHK SEL A 6 000,0 111,8 107,9 104,9 101,5 95,7 89,2 84,5 79,3 73,7 68,0 SPEYHK SEL A 8 000,0 117,3 113,4 110,4 107,0 101,2 94,7 90,0 84,8 79,2 73,5 SPEYHK SEL A 10 000,0 123,9 120,0 117,0 113,6 107,8 101,3 96,6 91,4 85,8 80,1 SPEYHK SEL D 1 000,0 89,4 85,5 82,5 79,1 73,3 66,8 62,1 56,9 51,3 45,6 SPEYHK SEL D 2 000,0 93,5 89,6 86,6 83,2 77,4 70,9 66,2 61,0 55,4 49,7 SPEYHK SEL D 4 000,0 101,7 97,8 94,8 91,4 85,6 79,1 74,4 69,2 63,6 57,9 SPEYHK SEL D 6 000,0 111,8 107,9 104,9 101,5 95,7 89,2 84,5 79,3 73,7 68,0 SPEYHK SEL D 8 000,0 117,3 113,4 110,4 107,0 101,2 94,7 90,0 84,8 79,2 73,5 SPEYHK SEL D 10 000,0 123,9 120,0 117,0 113,6 107,8 101,3 96,6 91,4 85,8 80,1 1.7.2015 EN Official Journal of the European Union L 168/781Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) T1KBFP LAmax A 5 250,0 92,3 85,1 80,3 75,4 67,4 58,8 52,6 45,9 39,1 32,7 T1KBFP LAmax A 10 500,0 92,7 85,5 80,7 75,7 67,8 59,2 53,0 46,3 39,6 33,3 T1KBFP LAmax A 15 750,0 93,6 86,4 81,5 76,5 68,6 60,0 53,9 47,2 40,5 34,3 T1KBFP LAmax A 21 000,0 94,6 87,4 82,5 77,5 69,5 61,0 54,9 48,3 41,7 35,5 T1KBFP LAmax D 20 000,0 92,9 85,9 81,3 76,4 68,5 60,0 53,9 47,0 40,1 33,6 T1KBFP LAmax D 29 000,0 94,8 88,0 83,3 78,2 70,1 61,4 55,2 48,5 41,7 35,4 T1KBFP LAmax D 38 000,0 97,1 90,2 85,7 80,4 72,3 63,5 57,3 50,7 44,0 37,8 T1KBFP LAmax D 47 000,0 99,5 92,5 88,2 82,8 74,6 65,9 59,8 53,2 46,6 40,4 T1KBFP LAmax D 56 000,0 101,9 94,8 90,8 85,1 77,0 68,4 62,4 55,9 49,3 43,2 T1KBFP LAmax D 65 000,0 105,2 97,8 94,2 88,3 80,3 71,9 66,0 59,6 53,2 47,2 T1KBFP SEL A 5 250,0 94,9 90,5 87,4 84,3 79,1 73,1 68,5 63,4 58,3 53,5 T1KBFP SEL A 10 500,0 95,9 91,3 88,2 84,9 79,4 73,3 68,7 63,7 58,6 53,9 T1KBFP SEL A 15 750,0 97,1 92,5 89,2 85,8 80,2 74,1 69,6 64,7 59,6 55,0 T1KBFP SEL A 21 000,0 98,4 93,7 90,2 86,8 81,2 75,2 70,8 65,9 61,0 56,4 T1KBFP SEL D 20 000,0 96,4 91,8 88,6 84,8 79,1 73,0 68,5 63,5 58,4 53,6 T1KBFP SEL D 29 000,0 97,1 92,7 90,0 86,1 80,5 74,5 70,1 65,2 60,3 55,8 T1KBFP SEL D 38 000,0 98,6 94,3 91,8 87,9 82,4 76,6 72,3 67,5 62,8 58,4 T1KBFP SEL D 47 000,0 100,5 96,2 94,0 89,9 84,7 78,9 74,8 70,1 65,5 61,2 T1KBFP SEL D 56 000,0 102,5 98,3 96,2 92,1 87,0 81,5 77,4 72,9 68,3 64,1 T1KBFP SEL D 65 000,0 105,4 101,2 99,3 95,1 90,2 84,9 81,0 76,6 72,2 68,2 L 168/782 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) T56A7 LAmax A 30,0 96,0 89,4 84,8 79,9 71,9 62,4 55,0 47,0 39,2 31,6 T56A7 LAmax A 100,0 99,8 93,3 88,9 84,3 77,3 70,0 65,1 60,0 54,5 48,4 T56A7 LAmax D 30,0 96,0 89,4 84,8 79,9 71,9 62,4 55,0 47,0 39,2 31,6 T56A7 LAmax D 100,0 99,8 93,3 88,9 84,3 77,3 70,0 65,1 60,0 54,5 48,4 T56A7 SEL A 30,0 98,0 93,7 90,6 87,2 81,4 74,2 68,3 61,8 55,5 49,4 T56A7 SEL A 100,0 100,1 95,8 92,9 89,8 85,0 80,0 76,6 72,9 69,0 64,4 T56A7 SEL D 30,0 98,0 93,7 90,6 87,2 81,4 74,2 68,3 61,8 55,5 49,4 T56A7 SEL D 100,0 100,1 95,8 92,9 89,8 85,0 80,0 76,6 72,9 69,0 64,4 TAY620 LAmax A 3 372,0 89,1 82,7 78,4 73,9 66,8 58,9 53,1 46,9 40,4 34,3 TAY620 LAmax A 5 620,0 93,0 86,8 82,6 78,0 70,7 62,6 56,8 50,3 43,6 37,2 TAY620 LAmax D 4 496,0 91,5 85,3 81,0 76,1 68,7 60,2 54,3 48,0 41,4 35,7 TAY620 LAmax D 13 489,0 106,2 100,2 96,1 91,5 84,4 76,4 70,3 63,6 56,4 50,3 TAY620 SEL A 3 372,0 90,9 86,8 84,0 81,1 76,3 70,7 66,5 61,8 56,9 52,3 TAY620 SEL A 5 620,0 94,8 90,9 88,2 85,2 80,2 74,4 70,2 65,2 60,1 55,2 TAY620 SEL D 4 496,0 93,3 89,4 86,6 83,3 78,2 72,0 67,7 62,9 57,9 53,7 TAY620 SEL D 13 489,0 108,0 104,3 101,7 98,7 93,9 88,2 83,7 78,5 72,9 68,3 TAY650 LAmax A 3 372,0 89,3 82,9 78,6 74,0 66,7 58,8 53,1 46,9 40,4 34,3 TAY650 LAmax A 5 620,0 92,3 86,0 81,7 77,1 69,7 61,7 56,0 49,8 43,3 37,2 TAY650 LAmax D 4 496,0 91,3 84,8 80,2 75,0 67,3 58,6 53,0 47,2 41,1 35,8 TAY650 LAmax D 13 488,0 104,7 98,8 94,6 90,2 83,2 75,5 69,8 63,6 57,1 51,5 1.7.2015 EN Official Journal of the European Union L 168/783Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) TAY650 SEL A 3 372,0 91,1 87,0 84,2 81,2 76,2 70,6 66,5 61,8 56,9 52,3 TAY650 SEL A 5 620,0 94,1 90,1 87,3 84,3 79,2 73,5 69,4 64,7 59,8 55,2 TAY650 SEL D 4 496,0 93,1 88,9 85,8 82,2 76,8 70,4 66,4 62,1 57,6 53,8 TAY650 SEL D 13 488,0 106,5 102,9 100,2 97,4 92,7 87,3 83,2 78,5 73,6 69,5 TAY651 LAmax A 5 000,0 91,4 84,7 80,1 75,3 67,7 59,5 53,7 47,3 40,8 34,6 TAY651 LAmax A 7 000,0 97,9 91,2 86,7 82,0 74,4 66,0 60,1 53,4 46,6 40,1 TAY651 LAmax D 9 000,0 101,2 94,6 90,1 85,4 77,8 69,4 63,3 56,6 49,8 43,3 TAY651 LAmax D 11 000,0 104,0 97,4 92,9 88,2 80,6 72,2 66,2 59,4 52,5 45,9 TAY651 LAmax D 13 000,0 108,4 101,8 97,4 92,7 85,1 76,8 70,8 64,4 57,9 51,7 TAY651 SEL A 5 000,0 95,7 91,1 87,8 84,4 79,0 73,0 68,7 63,7 58,6 53,8 TAY651 SEL A 7 000,0 100,5 96,1 93,1 89,8 84,5 78,4 73,9 68,7 63,4 58,4 TAY651 SEL D 9 000,0 103,5 99,1 96,2 92,9 87,6 81,5 76,9 71,7 66,4 61,3 TAY651 SEL D 11 000,0 106,3 101,9 98,9 95,7 90,4 84,3 79,7 74,3 68,8 63,6 TAY651 SEL D 13 000,0 110,2 105,9 102,9 99,7 94,4 88,3 83,8 78,7 73,5 68,6 TAYGIV LAmax A 2 000,0 86,0 79,9 75,6 71,0 63,7 55,8 50,3 44,5 38,4 32,4 TAYGIV LAmax A 3 000,0 87,2 81,1 76,8 72,2 64,8 57,0 51,5 45,7 39,6 33,5 TAYGIV LAmax A 4 000,0 88,5 82,4 78,1 73,5 66,2 58,3 52,8 47,0 40,9 34,9 TAYGIV LAmax A 6 000,0 91,5 85,4 81,1 76,5 69,2 61,3 55,8 50,0 43,9 37,9 TAYGIV LAmax A 8 000,0 95,1 88,9 84,7 80,0 72,7 64,8 59,4 53,6 47,4 41,4 TAYGIV LAmax A 10 000,0 99,1 93,0 88,7 84,1 76,7 68,9 63,4 57,6 51,5 45,4 L 168/784 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) TAYGIV LAmax D 2 000,0 86,0 79,9 75,6 71,0 63,7 55,8 50,3 44,5 38,4 32,4 TAYGIV LAmax D 3 000,0 87,2 81,1 76,8 72,2 64,8 57,0 51,5 45,7 39,6 33,5 TAYGIV LAmax D 4 000,0 88,5 82,4 78,1 73,5 66,2 58,3 52,8 47,0 40,9 34,9 TAYGIV LAmax D 6 000,0 91,5 85,4 81,1 76,5 69,2 61,3 55,8 50,0 43,9 37,9 TAYGIV LAmax D 8 000,0 95,1 88,9 84,7 80,0 72,7 64,8 59,4 53,6 47,4 41,4 TAYGIV LAmax D 10 000,0 99,1 93,0 88,7 84,1 76,7 68,9 63,4 57,6 51,5 45,4 TAYGIV LAmax D 11 000,0 101,0 95,0 91,0 86,0 79,0 71,0 65,5 60,0 54,0 47,5 TAYGIV LAmax D 11 200,0 101,5 95,5 91,5 86,5 79,5 71,5 66,0 60,5 54,5 48,0 TAYGIV SEL A 2 000,0 89,9 86,0 83,0 79,6 73,9 67,3 62,6 57,4 51,8 46,2 TAYGIV SEL A 3 000,0 90,7 86,8 83,8 80,4 74,6 68,0 63,3 58,2 52,6 46,9 TAYGIV SEL A 4 000,0 91,6 87,7 84,7 81,3 75,5 69,0 64,2 59,1 53,5 47,8 TAYGIV SEL A 6 000,0 93,9 90,0 87,0 83,6 77,8 71,3 66,5 61,4 55,8 50,1 TAYGIV SEL A 8 000,0 96,8 92,9 89,9 86,5 80,8 74,2 69,5 64,3 58,7 53,1 TAYGIV SEL A 10 000,0 100,4 96,5 93,5 90,1 84,4 77,8 73,1 67,9 62,3 56,6 TAYGIV SEL D 2 000,0 89,9 86,0 83,0 79,6 73,9 67,3 62,6 57,4 51,8 46,2 TAYGIV SEL D 3 000,0 90,7 86,8 83,8 80,4 74,6 68,0 63,3 58,2 52,6 46,9 TAYGIV SEL D 4 000,0 91,6 87,7 84,7 81,3 75,5 69,0 64,2 59,1 53,5 47,8 TAYGIV SEL D 6 000,0 93,9 90,0 87,0 83,6 77,8 71,3 66,5 61,4 55,8 50,1 TAYGIV SEL D 8 000,0 96,8 92,9 89,9 86,5 80,8 74,2 69,5 64,3 58,7 53,1 TAYGIV SEL D 10 000,0 100,4 96,5 93,5 90,1 84,4 77,8 73,1 67,9 62,3 56,6 1.7.2015 EN Official Journal of the European Union L 168/785Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) TAYGIV SEL D 11 000,0 102,0 98,0 95,5 92,0 86,0 79,5 74,5 70,0 64,0 58,5 TAYGIV SEL D 11 200,0 102,5 98,5 96,0 92,5 86,5 80,0 75,0 70,5 64,5 59,0 TF7312 LAmax A 1 000,0 91,1 84,2 79,2 73,9 65,5 56,6 50,2 43,5 36,3 28,6 TF7312 LAmax A 1 500,0 96,1 89,3 84,4 79,3 71,0 61,9 55,2 48,0 40,1 31,6 TF7312 LAmax D 1 500,0 96,1 89,3 84,4 79,3 71,0 61,9 55,2 48,0 40,1 31,6 TF7312 LAmax D 2 650,0 107,5 99,8 94,4 88,9 80,1 70,3 62,9 54,6 45,3 35,0 TF7312 SEL A 1 000,0 93,7 89,0 85,6 81,8 75,6 68,9 64,1 58,8 53,1 46,9 TF7312 SEL A 1 500,0 99,3 94,8 91,4 87,8 81,8 74,9 69,7 64,0 57,6 50,6 TF7312 SEL D 1 500,0 99,3 94,8 91,4 87,8 81,8 74,9 69,7 64,0 57,6 50,6 TF7312 SEL D 2 650,0 110,5 105,0 101,1 97,1 90,6 83,0 77,1 70,3 62,5 53,8 TF7313 LAmax A 880,0 85,8 78,6 73,4 67,9 59,1 50,0 43,6 36,6 28,8 20,7 TF7313 LAmax A 2 300,0 95,2 88,6 84,1 79,3 71,7 63,4 57,3 50,1 41,6 32,2 TF7313 LAmax D 2 300,0 95,2 88,6 84,1 79,3 71,7 63,4 57,3 50,1 41,6 32,2 TF7313 LAmax D 3 000,0 101,0 94,4 89,8 85,0 77,4 69,1 63,0 55,9 47,6 38,6 TF7313 SEL A 880,0 87,1 82,9 79,8 76,4 70,8 64,3 59,3 53,8 47,6 41,0 TF7313 SEL A 2 300,0 95,9 92,0 89,3 86,3 81,3 75,4 70,8 65,1 58,1 50,2 TF7313 SEL D 2 300,0 95,9 92,0 89,3 86,3 81,3 75,4 70,8 65,1 58,1 50,2 TF7313 SEL D 3 000,0 103,4 99,4 96,4 93,8 88,8 82,9 78,3 72,7 65,9 58,3 TIO540 LAmax A 1 900,0 77,7 70,8 65,6 61,2 54,5 47,5 42,6 37,3 31,4 25,3 TIO540 LAmax A 2 300,0 83,6 77,1 72,7 68,1 60,9 53,4 48,1 42,5 36,3 29,8 L 168/786 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) TIO540 LAmax D 2 400,0 85,2 78,7 74,4 69,9 62,8 55,5 50,4 45,0 39,0 32,7 TIO540 LAmax D 2 500,0 89,5 83,1 78,8 74,3 67,3 60,1 55,1 49,7 43,7 37,4 TIO540 SEL A 1 900,0 78,6 74,8 72,3 69,7 65,9 61,7 58,6 55,1 50,9 46,4 TIO540 SEL A 2 300,0 84,3 80,8 78,4 75,9 71,8 67,3 64,0 60,3 55,7 50,6 TIO540 SEL D 2 400,0 86,0 82,5 80,1 77,5 73,5 69,0 65,7 62,1 57,7 52,9 TIO540 SEL D 2 500,0 88,9 85,4 82,9 80,4 76,4 72,0 68,8 65,2 61,0 56,2 TIO542 LAmax A 2 380,0 85,1 78,8 74,6 70,2 63,4 56,2 51,1 45,4 39,2 32,5 TIO542 LAmax A 2 400,0 86,8 80,5 76,3 71,9 65,0 57,6 52,3 46,5 40,1 33,4 TIO542 LAmax D 2 190,0 85,9 79,4 75,0 70,5 63,4 56,0 51,0 45,6 39,7 33,6 TIO542 LAmax D 2 280,0 88,2 81,7 77,4 72,8 65,7 58,1 53,0 47,4 41,4 35,0 TIO542 LAmax D 2 500,0 92,1 85,7 81,3 76,7 69,4 61,7 56,2 50,3 43,8 37,0 TIO542 SEL A 2 380,0 85,2 81,6 79,3 76,8 72,9 68,4 65,2 61,5 57,1 52,4 TIO542 SEL A 2 400,0 86,8 83,2 80,9 78,4 74,3 69,8 66,4 62,5 58,0 53,2 TIO542 SEL D 2 190,0 87,8 84,1 81,6 78,8 74,4 69,5 66,0 62,1 57,9 53,3 TIO542 SEL D 2 280,0 89,5 85,6 82,9 80,2 75,7 70,9 67,4 63,5 59,1 54,3 TIO542 SEL D 2 500,0 93,1 89,4 87,0 84,3 80,0 75,0 71,4 67,3 62,4 57,2 TPE331 LAmax A 30,0 83,9 77,6 73,4 69,0 62,1 54,6 49,0 42,8 35,6 27,0 TPE331 LAmax A 100,0 88,4 82,3 78,2 74,0 67,5 60,5 55,4 49,8 43,5 36,4 TPE331 LAmax D 30,0 83,9 77,6 73,4 69,0 62,1 54,6 49,0 42,8 35,6 27,0 TPE331 LAmax D 100,0 88,4 82,3 78,2 74,0 67,5 60,5 55,4 49,8 43,5 36,4 1.7.2015 EN Official Journal of the European Union L 168/787Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) TPE331 SEL A 30,0 84,3 80,2 77,4 74,6 69,9 64,7 60,6 55,9 50,2 43,7 TPE331 SEL A 100,0 88,5 84,6 82,0 79,3 75,0 70,3 66,7 62,7 57,9 52,2 TPE331 SEL D 30,0 84,3 80,2 77,4 74,6 69,9 64,7 60,6 55,9 50,2 43,7 TPE331 SEL D 100,0 88,5 84,6 82,0 79,3 75,0 70,3 66,7 62,7 57,9 52,2 TPE331-5 LAmax A 300,0 85,5 78,8 74,3 69,5 61,8 53,5 47,6 41,1 33,7 26,0 TPE331-5 LAmax A 306,0 85,5 78,8 74,3 69,5 61,8 53,5 47,6 41,1 33,7 26,0 TPE331-5 LAmax A 460,0 84,2 77,5 73,0 68,2 60,5 52,2 46,2 39,5 32,1 24,5 TPE331-5 LAmax D 1 491,0 86,9 80,5 76,1 71,5 64,3 56,6 51,1 45,3 39,1 32,9 TPE331-5 LAmax D 1 791,0 88,1 81,6 77,2 72,6 65,3 57,3 51,5 45,2 38,4 31,5 TPE331-5 LAmax D 1 800,0 88,1 81,6 77,2 72,6 65,3 57,3 51,5 45,2 38,4 31,5 TPE331-5 SEL A 300,0 88,5 84,1 81,1 77,8 72,4 66,4 61,9 56,9 51,0 44,8 TPE331-5 SEL A 306,0 88,5 84,1 81,1 77,8 72,4 66,4 61,9 56,9 51,0 44,8 TPE331-5 SEL A 460,0 86,7 82,3 79,3 76,0 70,6 64,5 59,9 54,8 48,9 42,7 TPE331-5 SEL D 1 491,0 89,7 85,5 82,6 79,6 74,6 69,1 65,1 60,8 56,2 51,4 TPE331-5 SEL D 1 791,0 89,9 85,7 82,8 79,7 74,6 68,9 64,6 59,8 54,5 49,1 TPE331-5 SEL D 1 800,0 89,9 85,7 82,8 79,7 74,6 68,9 64,6 59,8 54,5 49,1 TRENT5 LAmax A 3 000,0 94,6 88,1 83,3 78,3 70,5 61,8 55,6 48,7 41,1 33,2 TRENT5 LAmax A 5 000,0 95,6 88,8 84,0 78,9 70,9 62,1 55,8 48,9 41,2 33,3 TRENT5 LAmax A 7 000,0 96,2 89,6 84,6 79,5 71,3 62,6 56,3 49,3 41,7 33,9 TRENT5 LAmax A 9 000,0 97,2 90,7 85,7 80,5 72,2 63,2 56,8 49,8 42,1 34,1 L 168/788 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) TRENT5 LAmax D 30 000,0 104,0 96,3 91,0 85,5 77,0 67,8 61,1 53,8 45,9 37,8 TRENT5 LAmax D 35 000,0 104,8 97,3 92,2 86,9 78,6 69,5 62,8 55,7 47,8 39,7 TRENT5 LAmax D 40 000,0 105,8 98,5 93,5 88,3 80,1 71,0 64,4 57,0 49,3 41,1 TRENT5 LAmax D 47 000,0 107,8 100,4 95,4 90,3 82,2 73,2 66,6 59,3 51,3 43,0 TRENT5 SEL A 3 000,0 99,0 94,3 91,0 87,7 82,3 76,1 71,5 66,3 60,4 53,9 TRENT5 SEL A 5 000,0 99,6 94,8 91,6 88,2 82,7 76,4 71,8 66,5 60,5 54,1 TRENT5 SEL A 7 000,0 100,5 95,5 92,3 88,8 83,3 76,9 72,2 66,9 60,9 54,4 TRENT5 SEL A 9 000,0 101,5 96,4 93,1 89,5 83,9 77,5 72,8 67,5 61,4 54,9 TRENT5 SEL D 30 000,0 104,9 100,0 97,0 93,6 88,2 82,0 77,4 72,0 65,9 59,0 TRENT5 SEL D 35 000,0 106,0 101,4 98,4 95,1 89,8 83,7 79,2 73,8 67,6 60,9 TRENT5 SEL D 40 000,0 107,1 102,7 99,7 96,5 91,4 85,4 80,9 75,6 69,4 62,7 TRENT5 SEL D 47 000,0 108,6 104,4 101,5 98,4 93,3 87,3 82,8 77,6 71,6 65,1 TRENT7 LAmax A 4 000,0 93,6 86,6 81,9 77,1 69,4 61,2 55,3 48,7 41,2 33,4 TRENT7 LAmax A 12 000,0 95,1 88,1 83,3 78,4 70,7 62,3 56,2 49,4 41,8 33,8 TRENT7 LAmax D 31 000,0 102,6 95,4 90,6 85,5 77,3 68,0 61,1 53,3 45,0 36,6 TRENT7 LAmax D 41 000,0 102,6 95,3 90,5 85,4 77,4 68,5 62,0 54,7 46,6 38,1 TRENT7 LAmax D 52 000,0 105,6 98,5 93,8 88,8 80,8 72,0 65,5 58,3 50,2 41,8 TRENT7 LAmax D 62 000,0 108,7 101,6 96,9 91,9 83,9 75,1 68,9 62,0 54,1 45,5 TRENT7 SEL A 4 000,0 97,4 93,0 89,8 86,6 81,5 75,7 71,4 66,3 60,5 54,1 TRENT7 SEL A 12 000,0 98,4 94,0 90,8 87,6 82,4 76,5 72,1 67,0 61,1 54,6 1.7.2015 EN Official Journal of the European Union L 168/789Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) TRENT7 SEL D 31 000,0 104,2 99,6 96,5 93,1 87,7 81,2 76,2 70,6 64,3 57,6 TRENT7 SEL D 41 000,0 104,0 99,8 96,9 93,7 88,3 82,2 77,7 72,3 66,2 59,7 TRENT7 SEL D 52 000,0 106,4 102,4 99,6 96,6 91,5 85,5 81,1 75,9 69,9 63,4 TRENT7 SEL D 62 000,0 109,1 105,1 102,4 99,5 94,6 88,9 84,5 79,4 73,4 67,3 TRENT8 LAmax A 7 000,0 93,6 85,9 80,9 75,9 68,1 59,5 53,3 46,7 39,2 30,3 TRENT8 LAmax A 14 000,0 96,4 88,7 83,6 78,3 70,1 61,2 54,9 48,2 40,6 31,8 TRENT8 LAmax A 22 000,0 98,7 90,8 85,6 80,2 71,8 62,8 56,5 49,7 42,0 33,1 TRENT8 LAmax A 28 000,0 100,2 91,9 86,7 81,3 72,9 63,8 57,5 50,8 43,2 34,4 TRENT8 LAmax D 32 000,0 100,4 93,4 88,5 83,3 74,9 65,7 59,4 52,6 44,8 35,6 TRENT8 LAmax D 42 000,0 102,1 95,3 90,6 85,5 77,2 68,1 61,9 55,3 47,7 38,6 TRENT8 LAmax D 52 000,0 103,8 97,1 92,5 87,5 79,3 70,4 64,3 57,8 50,3 41,3 TRENT8 LAmax D 62 000,0 105,7 99,0 94,4 89,6 81,6 72,9 66,9 60,4 52,8 43,8 TRENT8 LAmax D 72 000,0 107,9 101,3 96,9 92,1 84,6 76,2 70,3 63,8 56,3 47,4 TRENT8 LAmax D 80 000,0 110,5 104,0 99,6 95,1 88,0 80,3 74,4 67,9 60,5 52,0 TRENT8 SEL A 7 000,0 97,4 92,1 88,8 85,3 80,0 74,0 69,6 64,8 59,3 52,8 TRENT8 SEL A 14 000,0 99,6 94,6 91,3 87,8 82,2 75,9 71,2 66,2 60,4 53,7 TRENT8 SEL A 22 000,0 101,6 96,7 93,3 89,7 83,9 77,4 72,7 67,6 61,8 55,2 TRENT8 SEL A 28 000,0 103,1 97,9 94,5 90,8 84,9 78,3 73,6 68,6 63,0 56,6 TRENT8 SEL D 32 000,0 102,6 98,4 95,3 91,8 85,9 79,1 74,2 69,1 63,5 57,2 TRENT8 SEL D 42 000,0 104,5 100,4 97,4 94,0 88,2 81,5 76,8 71,9 66,5 60,4 L 168/790 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) TRENT8 SEL D 52 000,0 106,1 102,1 99,2 95,9 90,3 83,9 79,3 74,4 69,1 63,1 TRENT8 SEL D 62 000,0 107,6 103,8 101,0 97,8 92,4 86,2 81,7 77,0 71,6 65,3 TRENT8 SEL D 72 000,0 109,5 105,8 103,1 100,1 95,0 89,2 84,9 80,2 74,8 68,3 TRENT8 SEL D 80 000,0 111,6 108,0 105,4 102,7 98,0 92,7 88,7 84,2 78,7 72,0 TRENT9 LAmax A 4 000,0 93,1 86,6 82,2 77,5 69,9 61,4 55,3 48,6 41,2 33,5 TRENT9 LAmax A 6 000,0 93,4 86,8 82,3 77,6 70,0 61,5 55,5 48,8 41,4 33,6 TRENT9 LAmax A 9 000,0 93,9 87,2 82,6 77,9 70,3 61,8 55,7 49,1 41,6 33,9 TRENT9 LAmax A 13 000,0 94,2 87,7 83,2 78,5 71,0 62,5 56,4 49,7 42,1 34,3 TRENT9 LAmax D 40 000,0 98,9 92,4 87,8 83,0 75,1 66,4 60,2 53,3 45,6 37,4 TRENT9 LAmax D 50 000,0 101,1 94,9 90,3 85,5 77,6 68,9 62,7 55,8 48,2 40,1 TRENT9 LAmax D 60 000,0 104,1 98,0 93,5 88,6 80,8 72,0 65,7 58,7 50,9 42,7 TRENT9 LAmax D 80 000,0 107,0 101,2 97,0 92,3 84,6 76,0 69,8 62,8 55,0 46,8 TRENT9 SEL A 4 000,0 98,5 93,7 90,5 87,2 82,0 76,0 71,5 66,4 60,6 54,3 TRENT9 SEL A 6 000,0 98,7 93,8 90,6 87,3 82,1 76,1 71,6 66,6 60,8 54,5 TRENT9 SEL A 9 000,0 99,2 94,2 91,0 87,7 82,4 76,4 72,0 66,9 61,1 54,8 TRENT9 SEL A 13 000,0 99,8 95,0 91,8 88,5 83,2 77,3 72,8 67,7 61,7 55,2 TRENT9 SEL D 40 000,0 102,7 98,2 95,0 91,6 86,3 80,3 75,8 70,8 64,9 58,5 TRENT9 SEL D 50 000,0 104,7 100,4 97,4 94,1 88,9 83,0 79,0 73,6 67,8 61,4 TRENT9 SEL D 60 000,0 107,5 103,5 100,6 97,4 92,2 86,2 81,8 76,7 70,8 64,4 TRENT9 SEL D 80 000,0 110,3 106,6 103,7 100,7 95,7 89,9 85,5 80,4 74,6 68,4 1.7.2015 EN Official Journal of the European Union L 168/791Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) TSIO52 LAmax A 30,0 83,1 76,9 72,6 68,3 61,5 54,1 48,7 42,8 36,4 29,5 TSIO52 LAmax A 100,0 95,4 89,1 84,9 80,5 73,7 66,3 60,9 55,1 48,8 42,0 TSIO52 LAmax D 30,0 83,1 76,9 72,6 68,3 61,5 54,1 48,7 42,8 36,4 29,5 TSIO52 LAmax D 100,0 95,4 89,1 84,9 80,5 73,7 66,3 60,9 55,1 48,8 42,0 TSIO52 SEL A 30,0 84,6 80,6 77,9 75,1 70,5 65,3 61,4 57,1 52,2 46,8 TSIO52 SEL A 100,0 97,6 93,6 90,9 88,0 83,4 78,3 74,4 70,1 65,3 59,9 TSIO52 SEL D 30,0 84,6 80,6 77,9 75,1 70,5 65,3 61,4 57,1 52,2 46,8 TSIO52 SEL D 100,0 97,6 93,6 90,9 88,0 83,4 78,3 74,4 70,1 65,3 59,9 V2522A LAmax A 2 000,0 89,7 83,1 78,5 73,4 65,3 56,3 49,8 42,6 34,5 26,3 V2522A LAmax A 2 700,0 89,9 83,3 78,6 73,6 65,5 56,5 49,9 42,8 34,7 26,6 V2522A LAmax A 6 000,0 91,8 85,0 80,0 74,8 66,6 57,6 51,0 43,7 35,5 27,2 V2522A LAmax D 10 000,0 94,8 86,3 80,5 74,7 66,4 57,4 50,9 43,8 36,0 27,9 V2522A LAmax D 14 000,0 96,6 88,4 83,2 78,2 70,3 61,5 55,1 47,9 39,8 31,5 V2522A LAmax D 18 000,0 101,4 93,9 89,1 84,0 76,1 67,2 60,8 53,6 46,0 37,7 V2522A LAmax D 21 000,0 103,1 95,8 91,0 86,1 78,2 69,4 63,2 56,3 48,6 40,5 V2522A SEL A 2 000,0 93,7 89,5 86,3 82,8 77,0 70,6 65,6 60,2 53,9 47,2 V2522A SEL A 2 700,0 93,9 89,7 86,4 82,9 77,1 70,7 65,8 60,4 54,0 47,4 V2522A SEL A 6 000,0 95,6 91,3 87,9 84,1 78,2 71,5 66,7 61,2 54,7 47,9 V2522A SEL D 10 000,0 94,9 90,1 86,7 83,3 77,9 71,7 67,0 61,7 55,7 49,1 V2522A SEL D 14 000,0 98,2 94,0 90,9 87,6 82,1 75,7 71,0 65,4 59,2 52,6 L 168/792 EN Official Journal of the European Union 1.7.2015Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) V2522A SEL D 18 000,0 102,6 98,6 95,6 92,5 87,2 81,1 76,6 71,3 65,3 58,9 V2522A SEL D 21 000,0 103,9 100,0 97,1 94,1 89,0 83,0 78,7 73,6 67,8 61,7 V2525 LAmax A 3 000,0 89,2 83,0 78,2 73,7 66,0 57,5 51,0 44,1 36,5 28,3 V2525 LAmax A 6 950,0 91,0 84,5 80,0 75,0 67,7 58,9 53,0 46,0 38,2 30,0 V2525 LAmax D 10 500,0 93,1 86,5 82,0 77,2 69,9 61,1 55,3 48,7 41,2 33,4 V2525 LAmax D 13 150,0 95,2 88,8 84,0 79,5 72,1 63,5 57,9 51,0 43,8 36,0 V2525 LAmax D 18 500,0 100,0 93,4 88,8 84,0 76,7 68,1 62,2 56,0 48,6 40,8 V2525 LAmax D 23 000,0 104,8 98,5 93,9 89,0 81,8 73,3 67,8 61,0 53,5 45,4 V2525 SEL A 3 000,0 91,9 88,5 85,4 81,9 76,7 71,2 66,9 61,7 55,7 49,1 V2525 SEL A 6 950,0 94,3 90,2 86,6 83,5 78,3 72,8 68,4 63,7 57,5 51,5 V2525 SEL D 10 500,0 95,8 91,6 88,5 85,3 80,2 74,7 70,2 65,7 59,5 54,1 V2525 SEL D 13 150,0 98,1 94,0 91,0 87,9 82,7 76,9 72,7 68,2 62,7 56,7 V2525 SEL D 18 500,0 102,4 98,5 95,7 92,7 87,7 82,2 78,2 73,2 67,8 61,7 V2525 SEL D 23 000,0 106,2 102,7 99,7 97,0 92,2 86,7 82,7 78,0 72,7 66,5 V2527A LAmax A 2 000,0 89,3 82,8 78,2 73,4 65,8 57,4 51,2 44,4 36,7 28,6 V2527A LAmax A 2 700,0 89,5 83,0 78,3 73,5 65,8 57,4 51,3 44,4 36,7 28,6 V2527A LAmax A 6 000,0 91,6 84,7 79,5 74,2 66,5 58,0 51,9 45,0 37,2 29,1 V2527A LAmax D 10 000,0 94,8 86,3 80,5 74,8 66,5 57,6 51,1 44,0 36,2 28,2 V2527A LAmax D 14 000,0 96,7 88,6 83,5 78,4 70,5 61,7 55,3 48,1 40,1 31,8 V2527A LAmax D 19 000,0 101,2 93,9 89,0 84,0 76,1 67,3 61,1 54,1 46,3 38,2 1.7.2015 EN Official Journal of the European Union L 168/793Power setting (the ‘Power Parameter’ Noise field in the ‘Aircraft’ NPD_ID Op type L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric table specifies the power setting type and unit) V2527A LAmax D 23 000,0 104,0 96,9 92,2 87,3 79,4 70,8 64,7 57,9 50,3 42,0 V2527A SEL A 2 000,0 93,1 89,1 86,1 82,9 77,7 71,7 67,1 61,9 55,8 49,2 V2527A SEL A 2 700,0 93,3 89,2 86,2 83,0 77,7 71,8 67,2 62,0 55,8 49,3 V2527A SEL A 6 000,0 94,7 90,5 87,4 83,9 78,5 72,3 67,7 62,5 56,3 49,7 V2527A SEL D 10 000,0 95,0 90,2 86,8 83,5 78,1 71,8 67,2 61,9 55,9 49,4 V2527A SEL D 14 000,0 98,3 93,9 90,9 87,6 82,1 75,8 71,1 65,6 59,4 52,8 V2527A SEL D 19 000,0 102,5 98,4 95,5 92,3 87,2 81,1 76,7 71,5 65,7 59,4 V2527A SEL D 23 000,0 104,6 100,7 98,0 95,0 90,0 84,3 80,0 75,1 69,5 63,3 V2530 LAmax A 2 000,0 91,8 84,4 79,6 74,5 66,3 57,2 50,5 43,2 35,2 26,9 V2530 LAmax A 6 000,0 93,3 86,1 81,2 75,9 67,6 58,5 51,8 44,4 36,2 27,8 V2530 LAmax D 13 000,0 96,8 88,3 83,2 78,2 70,3 61,4 54,9 47,6 39,6 31,3 V2530 LAmax D 18 000,0 99,6 92,1 87,3 82,3 74,3 65,4 59,0 51,9 44,1 35,9 V2530 LAmax D 22 000,0 103,3 96,1 91,4 86,4 78,5 69,8 63,6 56,9 49,2 41,1 V2530 LAmax D 27 000,0 107,0 100,0 95,3 90,4 82,6 74,2 68,1 61,5 54,0 45,8 V2530 SEL A 2 000,0 94,6 90,2 86,9 83,4 77,7 71,2 66,2 60,5 54,3 47,6 V2530 SEL A 6 000,0 96,0 91,4 88,1 84,6 78,8 72,3 67,4 61,7 55,4 48,6 V2530 SEL D 13 000,0 98,3 94,3 91,2 87,8 82,2 75,8 71,0 65,5 59,2 52,5 V2530 SEL D 18 000,0 100,8 96,8 93,8 90,7 85,4 79,4 74,8 69,5 63,6 57,1 V2530 SEL D 22 000,0 104,1 100,1 97,3 94,3 89,3 83,5 79,1 74,0 68,4 62,2 V2530 SEL D 27 000,0 107,5 103,5 100,9 98,0 93,2 87,6 83,4 78,6 73,0 67,1 L 168/794 EN Official Journal of the European Union 1.7.2015Table I-10 Spectral classes Spectral Op Type Description Class ID zH05_L zH36_L zH08_L zH001_L zH521_L zH061_L zH002_L zH052_L zH513_L zH004_L zH005_L 101 Departure 2/3-Engine.LowByPass.Tfan 59,5 61,6 62,8 73,1 80,8 78,3 72,3 75,8 75,9 73,6 71,8 102 Departure 2-Engine.HighByPass.Tfan 59,7 60,0 68,5 73,0 73,8 70,4 67,6 71,4 68,7 72,8 73,2 103 Departure 2-Engine.HighByPass.Tfan 56,7 66,1 70,1 72,8 76,6 73,0 74,5 77,0 75,3 72,2 72,2 104 Departure 2-Engine.Low/MidByPass.Tfan 57,3 56,3 61,5 67,7 71,4 73,7 67,0 72,1 73,8 74,1 71,3 105 Departure 2-Engine.HighByPass.Tfan 66,5 60,4 67,1 75,0 78,2 79,3 71,5 76,7 74,4 74,6 72,3 106 Departure 4-Engine.Tfan+Supersonic 62,5 57,4 66,9 73,7 75,5 74,0 71,4 73,4 73,4 75,7 75,8 107 Departure 4-Engine.Tfan 58,6 62,7 69,1 74,1 76,0 74,3 74,1 74,4 74,0 73,6 73,2 108 Departure 4-Engine.Tfan 66,2 66,2 66,2 72,2 80,8 67,9 67,6 72,0 70,0 70,7 71,1 109 Departure 2-Engine.Tprop+1/2-Engine.Piston 64,7 67,1 73,1 89,4 84,5 76,3 89,3 80,7 79,3 79,3 81,6 110 Departure 2-Engine.Tprop+4-Engine.Piston 71,4 69,9 79,9 87,4 76,5 80,9 86,2 86,0 85,6 81,2 76,8 111 Departure 2-Engine.Tprop 78,0 76,0 90,0 103,0 82,0 85,0 97,0 89,0 94,0 80,0 79,0 1.7.2015 EN Official Journal of the European Union L 168/795Spectral Op Type Description Class ID zH05_L zH36_L zH08_L zH001_L zH521_L zH061_L zH002_L zH052_L zH513_L zH004_L zH005_L 112 Departure 2/4-Engine.Tprop 74,0 95,0 92,0 75,0 96,0 90,0 74,9 78,0 75,0 75,0 74,1 113 Departure 2-Engine.Tjet+Tfan.Business 58,5 57,9 60,7 67,0 71,2 72,6 70,3 72,7 72,9 73,5 72,8 136 Departure 2-Engine.Tfan.Business 59,7 60,0 68,5 73,0 73,8 70,4 67,6 71,4 68,7 72,8 73,2 137 Departure 2-Engine.Tfan.Business 58,6 62,7 69,1 74,1 76,0 74,3 74,1 74,4 74,0 73,6 73,2 138 Departure 2-Engine.Tfan.Business 66,2 66,2 66,2 72,2 80,8 67,9 67,6 72,0 70,0 70,7 71,1 201 Approach 2/3-Engine.LowByPass.Tfan 64,9 65,5 66,2 66,7 73,0 77,6 74,8 70,7 76,6 72,5 74,4 202 Approach 2-Engine.Low/HighByPass.Tfan 68,5 68,5 68,5 68,4 68,5 70,9 73,3 67,3 72,6 72,5 72,1 203 Approach 2-Engine.HighByPass.Tfan+Business 67,3 68,9 69,6 70,0 70,2 74,0 74,7 73,1 71,3 74,1 72,9 204 Approach 2-Engine.Low/MidByPass.Tfan 58,8 57,1 59,4 68,0 72,8 73,7 69,1 72,3 74,8 75,6 73,6 205 Approach 2-Engine.HighByPass.Tfan 68,3 60,7 64,6 67,4 78,4 74,8 71,4 72,4 72,0 72,4 71,6 206 Approach 4-Engine.Tjet+Tfan 63,3 65,4 64,1 63,2 66,0 66,6 69,6 70,1 71,5 67,1 71,0 207 Approach 4-Engine.Tfan 67,0 61,1 62,7 64,1 70,4 74,4 71,8 68,4 76,3 72,3 73,5 L 168/796 EN Official Journal of the European Union 1.7.2015Spectral Op Type Description Class ID zH05_L zH36_L zH08_L zH001_L zH521_L zH061_L zH002_L zH052_L zH513_L zH004_L zH005_L 208 Approach 4-Engine.Tjet+Tfan 66,7 65,0 61,7 65,4 72,9 76,2 73,0 68,1 72,7 70,7 72,1 209 Approach 4-Engine.Tfan 60,0 59,0 60,0 69,0 71,0 70,0 69,0 69,0 69,0 69,0 70,0 210 Approach 2-Engine.Tprop 65,0 70,0 65,0 72,0 77,0 68,0 78,0 85,0 86,0 79,0 73,0 211 Approach 2-Engine.Tprop 71,3 65,4 74,7 88,1 77,1 80,3 86,9 80,0 86,8 78,2 75,5 212 Approach 2-Engine.Tprop 72,0 68,0 79,0 71,0 73,0 84,0 74,0 75,0 73,0 72,0 71,0 213 Approach 4-Engine.Tprop+Piston 64,0 73,0 76,0 71,0 82,0 83,0 67,0 71,0 70,0 69,0 69,0 214 Approach 2/4-Engine.Tprop 61,8 69,8 61,8 58,8 67,8 70,8 62,8 59,8 62,8 60,8 60,8 215 Approach 1/2-Engine.Piston 83,0 98,0 83,0 79,0 91,0 80,0 85,0 76,0 75,0 73,0 72,0 216 Approach 2-Engine.Tjet+Tfan 68,0 63,1 64,7 71,2 74,3 75,0 70,3 72,6 72,1 73,3 71,3 235 Approach 2-Engine.Tfan.Business 67,3 68,9 69,6 70,0 70,2 74,0 74,7 73,1 71,3 74,1 72,9 236 Approach 2-Engine.Tfan.Business 62,7 64,8 63,5 62,6 65,4 66,0 69,0 69,5 70,8 66,5 70,4 237 Approach 2-Engine.Tfan.Business 67,0 61,1 62,7 64,1 70,4 74,4 71,8 68,4 76,3 72,3 73,5 238 Approach 2-Engine.Tfan.Business 60,0 59,0 60,0 69,0 71,0 70,0 69,0 69,0 69,0 69,0 70,0 1.7.2015 EN Official Journal of the European Union L 168/797Spec­ tral Op Type Description Class ID zH05_L zH36_L zH08_L zH001_L zH521_L zH061_L zH002_L zH052_L zH513_L zH004_L zH005_L zH036_L zH008_L zH0001_L zH0521_L zH0061_L zH0002_L zH0052_L zH0513_L zH0004_L zH0005_L zH0036_L zH0008_L zH00001_L 101 Departure 2/3-Engine.Low­ 59,5 61,6 62,8 73,1 80,8 78,3 72,3 75,8 75,9 73,6 71,8 71,6 72,3 70,0 68,3 66,6 64,2 61,4 58,6 54,8 50,9 45,7 43,9 40,9 ByPass.Tfan 102 Departure 2-Engine.HighBy­ 59,7 60,0 68,5 73,0 73,8 70,4 67,6 71,4 68,7 72,8 73,2 73,0 72,9 70,0 68,0 67,3 62,3 61,4 58,0 58,8 58,7 46,7 44,2 44,1 Pass.Tfan 103 Departure 2-Engine.HighBy­ 56,7 66,1 70,1 72,8 76,6 73,0 74,5 77,0 75,3 72,2 72,2 71,2 70,2 70,0 69,6 71,1 70,6 67,1 63,4 63,5 58,2 51,5 42,3 37,7 Pass.Tfan 104 Departure 2-Engine.Low/ 57,3 56,3 61,5 67,7 71,4 73,7 67,0 72,1 73,8 74,1 71,3 70,4 70,9 70,0 68,2 67,3 63,4 60,9 56,6 53,2 47,8 40,5 31,7 27,9 MidByPass.Tfan 105 Departure 2-Engine.HighBy­ 66,5 60,4 67,1 75,0 78,2 79,3 71,5 76,7 74,4 74,6 72,3 71,9 71,1 70,0 69,0 68,8 67,0 65,5 63,4 59,2 53,8 50,0 44,7 38,2 Pass.Tfan 106 Departure 4-Engine.Tfan 62,5 57,4 66,9 73,7 75,5 74,0 71,4 73,4 73,4 75,7 75,8 74,1 71,6 70,0 68,9 68,2 66,4 63,5 62,5 62,5 59,2 53,7 48,1 41,2 +Supersonic 107 Departure 4-Engine.Tfan 58,6 62,7 69,1 74,1 76,0 74,3 74,1 74,4 74,0 73,6 73,2 72,3 71,7 70,0 69,1 69,4 69,6 73,6 67,7 63,1 58,3 51,5 44,2 34,7 108 Departure 4-Engine.Tfan 66,2 66,2 66,2 72,2 80,8 67,9 67,6 72,0 70,0 70,7 71,1 68,9 71,1 70,0 68,3 67,5 65,4 63,6 63,9 64,8 62,1 59,3 54,6 47,3 109 Departure 2-Engine.Tprop 64,7 67,1 73,1 89,4 84,5 76,3 89,3 80,7 79,3 79,3 81,6 80,3 76,4 70,0 65,0 61,9 59,8 57,3 55,6 52,7 50,9 44,8 36,3 28,4 +1/2-Engine.Pis­ ton L 168/798 EN Official Journal of the European Union 1.7.2015Spec­ tral Op Type Description Class ID zH05_L zH36_L zH08_L zH001_L zH521_L zH061_L zH002_L zH052_L zH513_L zH004_L zH005_L zH036_L zH008_L zH0001_L zH0521_L zH0061_L zH0002_L zH0052_L zH0513_L zH0004_L zH0005_L zH0036_L zH0008_L zH00001_L 110 Departure 2-Engine.Tprop 71,4 69,9 79,9 87,4 76,5 80,9 86,2 86,0 85,6 81,2 76,8 74,5 73,2 70,0 69,5 69,2 67,2 65,4 63,2 60,2 58,4 51,4 40,4 29,0 +4-Engine.Piston 111 Departure 2-Engine.Tprop 78,0 76,0 90,0 103,0 82,0 85,0 97,0 89,0 94,0 80,0 79,0 79,0 75,0 70,0 68,0 64,0 62,0 58,0 57,0 53,0 48,0 43,0 38,0 33,0 112 Departure 2/4-Engine.Tprop 74,0 95,0 92,0 75,0 96,0 90,0 74,9 78,0 75,0 75,0 74,1 74,0 72,0 70,0 71,0 72,0 71,0 70,0 66,0 64,0 60,0 54,0 46,0 39,9 113 Departure 2-Engine.Tjet 58,5 57,9 60,7 67,0 71,2 72,6 70,3 72,7 72,9 73,5 72,8 72,0 71,3 70,0 68,9 67,1 64,5 63,0 60,2 55,8 52,1 45,1 38,8 29,6 +Tfan.Business 136 Departure 2-Engine.Tfan. 59,7 60,0 68,5 73,0 73,8 70,4 67,6 71,4 68,7 72,8 73,2 73,0 72,9 70,0 68,0 67,3 62,3 61,4 58,0 58,8 58,7 46,7 44,2 44,1 Business 137 Departure 2-Engine.Tfan. 58,6 62,7 69,1 74,1 76,0 74,3 74,1 74,4 74,0 73,6 73,2 72,3 71,7 70,0 69,1 69,4 69,6 73,6 67,7 63,1 58,3 51,5 44,2 34,7 Business 138 Departure 2-Engine.Tfan. 66,2 66,2 66,2 72,2 80,8 67,9 67,6 72,0 70,0 70,7 71,1 68,9 71,1 70,0 68,3 67,5 65,4 63,6 63,9 64,8 62,1 59,3 54,6 47,3 Business 201 Approach 2/3-Engine.Low­ 64,9 65,5 66,2 66,7 73,0 77,6 74,8 70,7 76,6 72,5 74,4 73,6 70,9 70,0 69,2 67,8 66,5 68,0 63,0 60,0 57,6 56,3 54,6 45,8 ByPass.Tfan 202 Approach 2-Engine.Low/ 68,5 68,5 68,5 68,4 68,5 70,9 73,3 67,3 72,6 72,5 72,1 75,4 75,4 70,0 68,9 68,3 65,8 64,7 63,5 62,1 60,2 57,8 48,6 38,8 HighByPass.Tfan 1.7.2015 EN Official Journal of the European Union L 168/799Spec­ tral Op Type Description Class ID zH05_L zH36_L zH08_L zH001_L zH521_L zH061_L zH002_L zH052_L zH513_L zH004_L zH005_L zH036_L zH008_L zH0001_L zH0521_L zH0061_L zH0002_L zH0052_L zH0513_L zH0004_L zH0005_L zH0036_L zH0008_L zH00001_L 203 Approach 2-Engine.HighBy­ 67,3 68,9 69,6 70,0 70,2 74,0 74,7 73,1 71,3 74,1 72,9 73,1 71,6 70,0 70,4 67,4 67,4 70,8 69,7 72,1 64,2 56,4 49,6 38,9 Pass.Tfan+Busi­ ness 204 Approach 2-Engine.Low/ 58,8 57,1 59,4 68,0 72,8 73,7 69,1 72,3 74,8 75,6 73,6 72,1 72,1 70,0 66,3 63,6 59,9 57,5 54,8 51,8 48,8 45,8 42,8 39,8 MidByPass.Tfan 205 Approach 2-Engine.HighBy­ 68,3 60,7 64,6 67,4 78,4 74,8 71,4 72,4 72,0 72,4 71,6 72,0 71,0 70,0 68,9 67,2 65,8 64,4 63,0 62,0 60,6 54,4 48,5 39,0 Pass.Tfan 206 Approach 4-Engine.Tjet 63,3 65,4 64,1 63,2 66,0 66,6 69,6 70,1 71,5 67,1 71,0 70,4 71,8 70,0 69,6 66,6 62,9 62,0 62,7 59,1 58,8 53,3 50,2 40,6 +Tfan 207 Approach 4-Engine.Tfan 67,0 61,1 62,7 64,1 70,4 74,4 71,8 68,4 76,3 72,3 73,5 71,2 70,5 70,0 68,7 67,1 67,5 69,4 71,1 72,5 65,7 59,3 52,2 45,6 208 Approach 4-Engine.Tjet 66,7 65,0 61,7 65,4 72,9 76,2 73,0 68,1 72,7 70,7 72,1 70,1 69,0 70,0 70,9 70,2 70,6 81,3 73,7 62,8 62,6 56,0 49,6 37,9 +Tfan 209 Approach 4-Engine.Tfan 60,0 59,0 60,0 69,0 71,0 70,0 69,0 69,0 69,0 69,0 70,0 69,0 69,0 70,0 72,0 77,0 72,0 72,0 70,0 66,0 63,0 57,0 49,0 38,0 210 Approach 2-Engine.Tprop 65,0 70,0 65,0 72,0 77,0 68,0 78,0 85,0 86,0 79,0 73,0 76,0 71,0 70,0 68,0 68,0 65,0 63,0 60,0 56,0 53,0 52,0 42,0 28,0 211 Approach 2-Engine.Tprop 71,3 65,4 74,7 88,1 77,1 80,3 86,9 80,0 86,8 78,2 75,5 75,2 71,6 70,0 70,7 69,6 68,6 67,5 67,0 63,9 59,9 53,0 45,7 40,0 212 Approach 2-Engine.Tprop 72,0 68,0 79,0 71,0 73,0 84,0 74,0 75,0 73,0 72,0 71,0 77,0 73,0 70,0 77,0 75,0 72,0 70,0 71,0 83,0 75,0 57,0 54,0 45,0 L 168/800 EN Official Journal of the European Union 1.7.2015Spec­ tral Op Type Description Class ID zH05_L zH36_L zH08_L zH001_L zH521_L zH061_L zH002_L zH052_L zH513_L zH004_L zH005_L zH036_L zH008_L zH0001_L zH0521_L zH0061_L zH0002_L zH0052_L zH0513_L zH0004_L zH0005_L zH0036_L zH0008_L zH00001_L 213 Approach 4-Engine.Tprop 64,0 73,0 76,0 71,0 82,0 83,0 67,0 71,0 70,0 69,0 69,0 68,0 67,0 70,0 69,0 67,0 64,0 60,0 57,0 54,0 49,0 42,0 32,0 20,0 +Piston 214 Approach 2/4-Engine.Tprop 61,8 69,8 61,8 58,8 67,8 70,8 62,8 59,8 62,8 60,8 60,8 59,8 60,8 70,0 67,8 61,8 59,8 56,8 52,8 49,8 47,8 45,8 35,8 27,8 215 Approach 1/2-Engine.Piston 83,0 98,0 83,0 79,0 91,0 80,0 85,0 76,0 75,0 73,0 72,0 73,0 71,0 70,0 68,0 66,0 65,0 64,0 60,0 57,0 53,0 49,0 43,0 32,0 216 Approach 2-Engine.Tjet 68,0 63,1 64,7 71,2 74,3 75,0 70,3 72,6 72,1 73,3 71,3 70,7 70,3 70,0 69,3 68,0 67,8 66,3 64,4 62,0 57,2 52,2 43,5 33,1 +Tfan 235 Approach 2-Engine.Tfan. 67,3 68,9 69,6 70,0 70,2 74,0 74,7 73,1 71,3 74,1 72,9 73,1 71,6 70,0 70,4 67,4 67,4 70,8 69,7 72,1 64,2 56,4 49,6 38,9 Business 236 Approach 2-Engine.Tfan. 62,7 64,8 63,5 62,6 65,4 66,0 69,0 69,5 70,8 66,5 70,4 69,8 71,2 69,4 68,9 66,0 62,3 61,4 62,1 58,5 58,2 52,7 49,6 40,0 Business 237 Approach 2-Engine.Tfan. 67,0 61,1 62,7 64,1 70,4 74,4 71,8 68,4 76,3 72,3 73,5 71,2 70,5 70,0 68,7 67,1 67,5 69,4 71,1 72,5 65,7 59,3 52,2 45,6 Business 238 Approach 2-Engine.Tfan. 60,0 59,0 60,0 69,0 71,0 70,0 69,0 69,0 69,0 69,0 70,0 69,0 69,0 70,0 72,0 77,0 72,0 72,0 70,0 66,0 63,0 57,0 49,0 38,0 Business 1.7.2015 EN Official Journal of the European Union L 168/801This section introduces complementary data for general aviation aircraft. GASEPF and GASEPV data Table I-11 GASEPF and GASEPV aircraft types Numb Max Max Sea Level Approach Departure Lateral Engine Weight Owner MGTOW Noise Power ACFTID Description of MGLW (lb) Landing Static Thrust NPD_ID Spectral Spectral Directivity Type Class Category (lb) Chapter Parameter Engines Dist (ft) (lb) Class ID Class ID Identifier GASEPF Single-engine fixed pitch Piston 1 Small General 2 200 2 200 1 160 560 0 GASEPF Percent 215 109 Prop propeller aircraft Aviation GASEPV Single-engine variable pitch Piston 1 Small General 3 000 3 000 1 111 790 0 GASEPV Percent 215 109 Prop propeller aircraft Aviation (the associated spectral data are available in the ANP ‘Spectral Classes’ table) Table I-12 Departure and Arrival flight profile data for GASEPF and GASEPV aircraft Percentage of Max ACFTID Op type Profile_ID Stage length Point number Distance (ft) Altitude AFE (ft) TAS (kt) Static Thrust (%) GASEPF A APP_3_DEG 1 1 – 114 486,8 6 000,0 109,4 34,21 GASEPF A APP_3_DEG 1 2 – 57 243,4 3 000,0 71,8 37,57 GASEPF A APP_3_DEG 1 3 – 28 621,7 1 500,0 60,0 40,59 GASEPF A APP_3_DEG 1 4 – 19 081,1 1 000,0 59,6 39,85 GASEPF A APP_3_DEG 1 5 0,0 0,0 58,7 38,43 GASEPF A APP_3_DEG 1 6 47,2 0,0 55,7 27,20 L 168/802 EN Official Journal of the European Union 1.7.2015Percentage of Max ACFTID Op type Profile_ID Stage length Point number Distance (ft) Altitude AFE (ft) TAS (kt) Static Thrust (%) GASEPF A APP_3_DEG 1 7 472,0 0,0 30,0 10,00 GASEPF A APP_5_DEG 1 1 – 68 580,3 6 000,0 109,4 18,03 GASEPF A APP_5_DEG 1 2 – 34 290,2 3 000,0 71,8 22,59 GASEPF A APP_5_DEG 1 3 – 17 145,1 1 500,0 60,0 26,14 GASEPF A APP_5_DEG 1 4 – 11 430,1 1 000,0 59,6 25,67 GASEPF A APP_5_DEG 1 5 0,0 0,0 58,7 24,75 GASEPF A APP_5_DEG 1 6 47,2 0,0 55,7 27,20 GASEPF A APP_5_DEG 1 7 472,0 0,0 30,0 10,00 GASEPF D DEFAULT_DEP 1 1 0,0 0,0 0,0 113,06 GASEPF D DEFAULT_DEP 1 2 972,8 0,0 62,1 113,06 GASEPF D DEFAULT_DEP 1 3 2 077,9 51,4 73,1 96,32 GASEPF D DEFAULT_DEP 1 4 13 665,7 1 000,0 74,1 98,31 GASEPF D DEFAULT_DEP 1 5 16 079,7 1 097,7 84,3 86,65 GASEPF D DEFAULT_DEP 1 6 17 079,7 1 155,4 84,4 81,16 GASEPF D DEFAULT_DEP 1 7 49 057,1 3 000,0 86,8 84,60 GASEPF D DEFAULT_DEP 1 8 97 253,2 5 500,0 90,1 89,42 GASEPF D DEFAULT_DEP 1 9 140 694,0 7 500,0 92,9 93,53 GASEPF D DEFAULT_DEP 1 10 202 700,4 10 000,0 96,6 99,04 GASEPV A APP_3_DEG 1 1 – 114 486,8 6 000,0 109,4 24,34 GASEPV A APP_3_DEG 1 2 – 57 243,4 3 000,0 79,4 26,37 GASEPV A APP_3_DEG 1 3 – 28 621,7 1 500,0 67,5 45,05 1.7.2015 EN Official Journal of the European Union L 168/803Percentage of Max ACFTID Op type Profile_ID Stage length Point number Distance (ft) Altitude AFE (ft) TAS (kt) Static Thrust (%) GASEPV A APP_3_DEG 1 4 – 19 081,1 1 000,0 67,0 44,24 GASEPV A APP_3_DEG 1 5 0,0 0,0 66,0 42,66 GASEPV A APP_3_DEG 1 6 42,8 0,0 62,6 31,00 GASEPV A APP_3_DEG 1 7 428,0 0,0 30,0 10,00 GASEPV A APP_5_DEG 1 1 – 68 580,3 6 000,0 109,4 8,70 GASEPV A APP_5_DEG 1 2 – 34 290,2 3 000,0 79,4 12,04 GASEPV A APP_5_DEG 1 3 – 17 145,1 1 500,0 67,5 31,28 GASEPV A APP_5_DEG 1 4 – 11 430,1 1 000,0 67,0 30,72 GASEPV A APP_5_DEG 1 5 0,0 0,0 66,0 29,62 GASEPV A APP_5_DEG 1 6 42,8 0,0 62,6 31,00 GASEPV A APP_5_DEG 1 7 428,0 0,0 30,0 10,00 GASEPV D DEFAULT_DEP 1 1 0,0 0,0 0,0 163,92 GASEPV D DEFAULT_DEP 1 2 861,8 0,0 55,6 163,92 GASEPV D DEFAULT_DEP 1 3 1 302,6 42,7 66,0 138,25 GASEPV D DEFAULT_DEP 1 4 2 963,7 172,0 90,2 101,67 GASEPV D DEFAULT_DEP 1 5 9 389,6 1 000,0 91,3 103,50 GASEPV D DEFAULT_DEP 1 6 10 985,9 1 102,9 101,6 93,36 GASEPV D DEFAULT_DEP 1 7 11 985,9 1 200,6 101,8 86,89 GASEPV D DEFAULT_DEP 1 8 30 407,6 3 000,0 104,5 90,57 GASEPV D DEFAULT_DEP 1 9 57 858,2 5 500,0 108,5 95,72 GASEPV D DEFAULT_DEP 1 10 81 543,2 7 500,0 111,9 100,13 GASEPV D DEFAULT_DEP 1 11 113 618,2 10 000,0 116,4 106,03 L 168/804 EN Official Journal of the European Union 1.7.2015Table I-13 NPD data for GASEPF and GASEPV aircraft Power setting — Per­ Noise NPD_ID Op type centage of Maximum L_200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft metric Static Thrust (%) GASEPF LAmax A 30,00 72,2 65,9 61,6 57,2 50,3 43,1 38,0 32,7 27,0 20,9 GASEPF LAmax A 100,00 84,9 78,6 74,4 70,0 63,2 55,8 50,4 44,6 38,3 31,5 GASEPF LAmax D 30,00 72,2 65,9 61,6 57,2 50,3 43,1 38,0 32,7 27,0 20,9 GASEPF LAmax D 100,00 84,9 78,6 74,4 70,0 63,2 55,8 50,4 44,6 38,3 31,5 GASEPF SEL A 30,00 74,2 70,1 67,3 64,4 59,8 54,8 51,2 47,4 43,2 38,6 GASEPF SEL A 100,00 87,1 83,1 80,4 77,5 72,9 67,8 63,9 59,6 54,8 49,4 GASEPF SEL D 30,00 74,2 70,1 67,3 64,4 59,8 54,8 51,2 47,4 43,2 38,6 GASEPF SEL D 100,00 87,1 83,1 80,4 77,5 72,9 67,8 63,9 59,6 54,8 49,4 GASEPV LAmax A 30,00 82,8 73,9 69,6 65,2 58,3 51,1 46,0 40,7 35,0 28,9 GASEPV LAmax A 100,00 92,4 86,1 81,9 77,5 70,7 63,3 57,9 52,1 45,8 39,0 GASEPV LAmax D 30,00 82,8 73,9 69,6 65,2 58,3 51,1 46,0 40,7 35,0 28,9 GASEPV LAmax D 100,00 92,4 86,1 81,9 77,5 70,7 63,3 57,9 52,1 45,8 39,0 GASEPV SEL A 30,00 81,7 77,6 74,8 71,9 67,3 62,3 58,7 54,9 50,7 46,1 GASEPV SEL A 100,00 94,6 90,6 87,9 85,0 80,4 75,3 71,4 67,1 62,3 56,9 GASEPV SEL D 30,00 81,7 77,6 74,8 71,9 67,3 62,3 58,7 54,9 50,7 46,1 GASEPV SEL D 100,00 94,6 90,6 87,9 85,0 80,4 75,3 71,4 67,1 62,3 56,9 1.7.2015 EN Official Journal of the European Union L 168/805Aircraft classes data Aircraft group Examples of aircraft types (maximum take-off mass) P 1.0 Dewald Sunny, Flightstar II, Ikarus C42, Quicksilver MXL II, Sherpa, Stratos, Tecnam P92 Echo P 1.1 DG-400 (500 kg), Grob 109B (900 kg), H 36 Dimona (800 kg), Scheibe SF 25C (700 kg) P 1.2 DR 400/180R (1 000 kg), H 36 Dimona (800 kg), PZL-104 ‘Wilga 35’ (1 200 kg), Scheibe SF 25 (700 kg) P 1.3 DR 400/180R (1 000 kg), Cessna 172N (1 000 kg), Piper PA-28- 181 (1 200 kg), Piper PA-34- 200 (1 900 kg) Aircraft Noise and Performance data for the four classes are presented in the following tables: Table I-14 Noise group data for P 1.0, P 1.1, P 1.2, P 1.3 aircraft classes NOISE_ID,C,12 THRSET_TYP,C,1 MODEL_TYPE,C,1 SPECT_APP,N,3,0 SPECT_DEP,N,3,0 SPECT_AFB,N,3,0 P1.0 P I 215 109 0 P1.1 P I 215 109 0 P1.2 P I 215 109 0 P1.3 P I 215 109 0 THR_ THR_ ACFT_ WGT_CAT, OWNER_ ENG_ NOISE_ NOISE_ID, NUMB_ MX_GW_ MX_GW_ MX_DS_ COEFF_ ACFT_DESCR,C,40 RESTOR, STATIC, ID,C,12 C,1 CAT,C,1 TYPE,C,1 CAT,C,1 C,12 ENG,N,1,0 TKO,N,7,0 LND,N,7,0 STOP,N,5,0 TYPE,C,1 C,1 N,6,0 P1.0 Ultralights S G P 0 P1.0 1 N 0 0 0 P 100 P1.1 Motorgliders S G P 0 P1.1 1 N 0 0 0 P 100 P1.2 Prop MTOM <= 2 t S G P 0 P1.2 1 N 0 0 0 P 100 towing gliders P1.3 Prop MTOM <= 2 t S G P 0 P1.3 1 N 0 0 0 P 100 L 168/806 EN Official Journal of the European Union 1.7.2015Table I-15 Arrival and Departure flight profile data for P 1.0, P 1.1, P 1.2, P 1.3 aircraft classes ACFT_ID,C,12 OP_TYPE,C,1 PROF_ID1,C,8 PROF_ID2,C,1 WEIGHT,N,7,0 P1.0 A DEFAULT 1 100 P1.0 D DEFAULT 1 100 P1.1 A DEFAULT 1 100 P1.1 D DEFAULT 1 100 P1.2 A DEFAULT 1 100 P1.2 D DEFAULT 1 100 P1.3 A DEFAULT 1 100 P1.3 D DEFAULT 1 100 Table I-16 Noise Profile points data for P 1.0, P 1.1, P 1.2, P 1.3 aircraft classes ACFT_ID,C,12 OP_TYPE,C,1 PROF_ID1,C,8 PROF_ID2,C,1 PT_NUM,N,3,0 DISTANCE,N,10,1 ALTITUDE,N,7,1 SPEED,N,5,1 THR_SET,N,9,2 OP_MODE,C,1 P1.0 A DEFAULT 1 1 – 114 486 6 000 50,5 70 A P1.0 A DEFAULT 1 2 – 18 917,1 1 000 50,5 70 A P1.0 A DEFAULT 1 3 – 15 636,3 828,1 50,5 70 A P1.0 A DEFAULT 1 4 164 0 50,5 70 A P1.0 A DEFAULT 1 5 656,2 0 19,4 30 A P1.0 D DEFAULT 1 1 0 0 19,4 100 D P1.0 D DEFAULT 1 2 328,1 0 62,2 100 D P1.0 D DEFAULT 1 3 12 986,3 1 000 62,2 100 D 1.7.2015 EN Official Journal of the European Union L 168/807ACFT_ID,C,12 OP_TYPE,C,1 PROF_ID1,C,8 PROF_ID2,C,1 PT_NUM,N,3,0 DISTANCE,N,10,1 ALTITUDE,N,7,1 SPEED,N,5,1 THR_SET,N,9,2 OP_MODE,C,1 P1.0 D DEFAULT 1 4 42 000 3 000 65 100 D P1.0 D DEFAULT 1 5 200 000 10 000 68 100 D P1.1 A DEFAULT 1 1 – 114 486 6 000 50,5 70 A P1.1 A DEFAULT 1 2 – 18 589 1 000 50,5 70 A P1.1 A DEFAULT 1 3 – 15 308,2 828,1 50,5 70 A P1.1 A DEFAULT 1 4 492,1 0 50,5 70 A P1.1 A DEFAULT 1 5 656,2 0 19,4 30 A P1.1 D DEFAULT 1 1 0 0 19,4 100 D P1.1 D DEFAULT 1 2 656,2 0 66,1 100 D P1.1 D DEFAULT 1 3 13 314,4 1 000 66,1 100 D P1.1 D DEFAULT 1 4 43 000 3 000 70 100 D P1.1 D DEFAULT 1 5 200 000 10 000 73,9 100 D P1.2 A DEFAULT 1 1 – 114 486 6 000 60,3 70 A P1.2 A DEFAULT 1 2 – 18 589 1 000 60,3 70 A P1.2 A DEFAULT 1 3 – 15 308,2 828,1 60,3 70 A P1.2 A DEFAULT 1 4 492,1 0 60,3 70 A P1.2 A DEFAULT 1 5 1 476,4 0 19,4 30 A P1.2 D DEFAULT 1 1 0 0 19,4 100 D P1.2 D DEFAULT 1 2 1 312,3 0 62,2 100 D P1.2 D DEFAULT 1 3 17 705,8 1 000 62,2 100 D P1.2 D DEFAULT 1 4 50 000 3 000 64 100 D P1.2 D DEFAULT 1 5 200 000 10 000 66,1 100 D L 168/808 EN Official Journal of the European Union 1.7.2015ACFT_ID,C,12 OP_TYPE,C,1 PROF_ID1,C,8 PROF_ID2,C,1 PT_NUM,N,3,0 DISTANCE,N,10,1 ALTITUDE,N,7,1 SPEED,N,5,1 THR_SET,N,9,2 OP_MODE,C,1 P1.3 A DEFAULT 1 1 – 114 486 6 000 60,3 70 A P1.3 A DEFAULT 1 2 – 18 589 1 000 60,3 70 A P1.3 A DEFAULT 1 3 – 15 308,2 828,1 60,3 70 A P1.3 A DEFAULT 1 4 492,1 0 60,3 70 A P1.3 A DEFAULT 1 5 1 476,4 0 19,4 30 A P1.3 D DEFAULT 1 1 0 0 19,4 100 D P1.3 D DEFAULT 1 2 820,2 0 70 100 D P1.3 D DEFAULT 1 3 10 344 1 000 70 100 D P1.3 D DEFAULT 1 4 40 000 3 000 75 100 D P1.3 D DEFAULT 1 5 200 000 10 000 83 100 D Table I-17 NPD data for P 1.0, P 1.1, P 1.2, P 1.3 aircraft classes NOISE_ID, NOISE_ OP_MODE, THR_SET, L_1000, L_2000, L_4000, L_6300, L_10000, L_16000, L_25000, L_200,N,5,1 L_400,N,5,1 L_630,N,5,1 C,12 TYPE,C,1 C,1 N,9,2 N,5,1 N,5,1 N,5,1 N,5,1 N,5,1 N,5,1 N,5,1 P1.0 M A 30 55,2 49 44,8 40,4 33,6 26,3 21,2 15,6 9,3 2,8 P1.0 M A 70 65,2 59 54,8 50,4 43,6 36,3 31,2 25,6 19,3 12,8 P1.0 M D 88 71,2 65 60,8 56,4 49,6 42,3 37,2 31,6 25,3 18,8 P1.0 M D 100 75,2 69 64,8 60,4 53,6 46,3 41,2 35,6 29,3 22,8 P1.0 S A 30 54,7 51,4 49,1 46,7 42,8 38,4 35,2 31,4 27,1 22,3 P1.0 S A 70 64,7 61,4 59,1 56,7 52,8 48,4 45,2 41,4 37,1 32,3 P1.0 S D 88 70,7 67,4 65,1 62,7 58,8 54,4 51,2 47,4 43,1 38,3 1.7.2015 EN Official Journal of the European Union L 168/809NOISE_ID, NOISE_ OP_MODE, THR_SET, L_1000, L_2000, L_4000, L_6300, L_10000, L_16000, L_25000, L_200,N,5,1 L_400,N,5,1 L_630,N,5,1 C,12 TYPE,C,1 C,1 N,9,2 N,5,1 N,5,1 N,5,1 N,5,1 N,5,1 N,5,1 N,5,1 P1.0 S D 100 74,7 71,4 69,1 66,7 62,8 58,4 55,2 51,4 47,1 42,3 P1.1 M A 30 60,2 54 49,8 45,4 38,6 31,3 26,2 20,6 14,3 7,8 P1.1 M A 70 70,2 64 59,8 55,4 48,6 41,3 36,2 30,6 24,3 17,8 P1.1 M D 82 74,2 68 63,8 59,4 52,6 45,3 40,2 34,6 28,3 21,8 P1.1 M D 100 80,2 74 69,8 65,4 58,6 51,3 46,2 40,6 34,3 27,8 P1.1 S A 30 59,7 56,4 54,1 51,7 47,8 43,4 40,2 36,4 32,1 27,3 P1.1 S A 70 69,7 66,4 64,1 61,7 57,8 53,4 50,2 46,4 42,1 37,3 P1.1 S D 82 73,7 70,4 68,1 65,7 61,8 57,4 54,2 50,4 46,1 41,3 P1.1 S D 100 79,7 76,4 74,1 71,7 67,8 63,4 60,2 56,4 52,1 47,3 P1.2 M A 30 64,4 58,2 53,9 49,5 42,6 35,1 29,8 24 17,5 10,6 P1.2 M A 70 74,4 68,2 63,9 59,5 52,6 45,1 39,8 34 27,5 20,6 P1.2 M D 76 76,4 70,2 65,9 61,5 54,6 47,1 41,8 36 29,5 22,6 P1.2 M D 100 84,4 78,2 73,9 69,5 62,6 55,1 49,8 44 37,5 30,6 P1.2 S A 30 63,9 60,5 58,2 55,8 51,8 47,2 43,8 39,8 35,2 30,1 P1.2 S A 70 73,9 70,5 68,2 65,8 61,8 57,2 53,8 49,8 45,2 40,1 P1.2 S D 76 75,9 72,5 70,2 67,8 63,8 59,2 55,8 51,8 47,2 42,1 P1.2 S D 100 83,9 80,5 78,2 75,8 71,8 67,2 63,8 59,8 55,2 50,1 P1.3 M A 30 66,4 60,2 55,9 51,5 44,6 37,1 31,8 26 19,5 12,6 P1.3 M A 70 76,4 70,2 65,9 61,5 54,6 47,1 41,8 36 29,5 22,6 P1.3 M D 76 78,4 72,2 67,9 63,5 56,6 49,1 43,8 38 31,5 24,6 P1.3 M D 100 86,4 80,2 75,9 71,5 64,6 57,1 51,8 46 39,5 32,6 P1.3 S A 30 65,9 62,5 60,2 57,8 53,8 49,2 45,8 41,8 37,2 32,1 L 168/810 EN Official Journal of the European Union 1.7.2015NOISE_ID, NOISE_ OP_MODE, THR_SET, L_1000, L_2000, L_4000, L_6300, L_10000, L_16000, L_25000, L_200,N,5,1 L_400,N,5,1 L_630,N,5,1 C,12 TYPE,C,1 C,1 N,9,2 N,5,1 N,5,1 N,5,1 N,5,1 N,5,1 N,5,1 N,5,1 P1.3 S A 70 75,9 72,5 70,2 67,8 63,8 59,2 55,8 51,8 47,2 42,1 P1.3 S D 76 77,9 74,5 72,2 69,8 65,8 61,2 57,8 53,8 49,2 44,1 P1.3 S D 100 85,9 82,5 80,2 77,8 73,8 69,2 65,8 61,8 57,2 52,1 Helicopter Noise and Performance Data Set 1 This includes data for five helicopters classes, based on helicopter MTOM: Table I-18 Helicopter Data Set 1 Description Table Number Max Max Sea Level Approach Departure Lateral Dir­ Weight Owner MGTOW MGLW Noise NPD_ ACFT_ID Description EngineTYPE of Landing Static Thrust Power Parameter Spectral Spectral ectivity Class Category (lb) (lb) Chapter ID Engines Dist (ft) (lb) Class ID Class ID Indentifier H1.0 Helicopters with Propeller 0 0 Helicopter 0 0 0 100 0 H1.0 SHP (% of Max 215 109 Prop MTOM <= 1 t Static Thrust) H1.1 Helicopters with Propeller 0 0 Helicopter 0 0 0 100 0 H1.1 SHP (% of Max 215 109 Prop MTOM 1-3 t Static Thrust) H1.2 Helicopters with Propeller 0 0 Helicopter 0 0 0 100 0 H1.2 SHP (% of Max 215 109 Prop MTOM 3-5 t Static Thrust) H2.1 Helicopters with Propeller 0 0 Helicopter 0 0 0 100 0 H2.1 SHP (% of Max 215 109 Prop MTOM 5-10 t Static Thrust) H2.2 Helicopters with Propeller 0 0 Helicopter 0 0 0 100 0 H2.2 SHP (% of Max 215 109 Prop MTOM > 10 t Static Thrust) 1.7.2015 EN Official Journal of the European Union L 168/811Table I-19 Helicopter Data Set 1 Departure Profiles ACFT_ID OP_TYPE PROF_ID1 PROF_ID2 PT_NUM DISTANCE (ft) ALTITUDE (ft) SPEED (kt) THR_SET (%) OP_MODE H1.0 D H1.0_S 1 1 0,0 0,0 3,9 100,00 D H1.0 D H1.0_S 1 2 9,8 6,6 5,8 100,00 D H1.0 D H1.0_S 1 3 32,8 16,4 9,7 100,00 D H1.0 D H1.0_S 1 4 295,3 49,2 40,8 100,00 D H1.0 D H1.0_S 1 5 5 687,5 1 000,0 60,3 100,00 D H1.0 D H1.0_S 1 6 8 968,3 1 000,0 64,1 100,00 D H1.0 D H1.0_S 1 7 200 000,0 1 000,0 64,1 100,00 D H1.1 D H1.1_S 1 1 0,0 0,0 3,9 100,00 D H1.1 D H1.1_S 1 2 9,8 6,6 5,8 100,00 D H1.1 D H1.1_S 1 3 32,8 16,4 9,7 100,00 D H1.1 D H1.1_S 1 4 295,3 49,2 40,8 100,00 D H1.1 D H1.1_S 1 5 6 298,3 1 000,0 64,1 100,00 D H1.1 D H1.1_S 1 6 9 579,2 1 000,0 70,0 100,00 D H1.1 D H1.1_S 1 7 200 000,0 1 000,0 70,0 100,00 D H1.2 D H1.2_S 1 1 0,0 0,0 3,9 100,00 D H1.2 D H1.2_S 1 2 9,8 6,6 5,8 100,00 D H1.2 D H1.2_S 1 3 32,8 16,4 9,7 100,00 D H1.2 D H1.2_S 1 4 295,3 49,2 40,8 100,00 D H1.2 D H1.2_S 1 5 6 298,3 1 000,0 70,0 100,00 D H1.2 D H1.2_S 1 6 9 579,2 1 000,0 75,8 100,00 D L 168/812 EN Official Journal of the European Union 1.7.2015ACFT_ID OP_TYPE PROF_ID1 PROF_ID2 PT_NUM DISTANCE (ft) ALTITUDE (ft) SPEED (kt) THR_SET (%) OP_MODE H1.2 D H1.2_S 1 7 200 000,0 1 000,0 75,8 100,00 D H2.1 D H2.1_S 1 1 0,0 0,0 3,9 100,00 D H2.1 D H2.1_S 1 2 9,8 6,6 5,8 100,00 D H2.1 D H2.1_S 1 3 32,8 16,4 9,7 100,00 D H2.1 D H2.1_S 1 4 295,3 49,2 40,8 100,00 D H2.1 D H2.1_S 1 5 6 298,3 1 000,0 70,0 100,00 D H2.1 D H2.1_S 1 6 9 579,2 1 000,0 75,8 100,00 D H2.1 D H2.1_S 1 7 200 000,0 1 000,0 75,8 100,00 D H2.2 D H2.2_S 1 1 0,0 0,0 3,9 100,00 D H2.2 D H2.2_S 1 2 9,8 0,0 5,8 100,00 D H2.2 D H2.2_S 1 3 32,8 16,4 9,7 100,00 D H2.2 D H2.2_S 1 4 295,3 49,2 40,8 100,00 D H2.2 D H2.2_S 1 5 6 298,3 1 000,0 70,0 100,00 D H2.2 D H2.2_S 1 6 9 579,2 1 000,0 75,8 100,00 D H2.2 D H2.2_S 1 7 200 000,0 1 000,0 75,8 100,00 D Table I-20 Helicopter Data Set 1 Arrival Profiles ACFT_ID OP_TYPE PROF_ID1 PROF_ID2 PT_NUM DISTANCE ALTITUDE SPEED THR_SET OP_MODE H1.0 A H1.0_L 1 1 – 200 000,0 1 000,0 64,1 100,00 A H1.0 A H1.0_L 1 2 – 10 836,6 1 000,0 64,1 100,00 A H1.0 A H1.0_L 1 3 – 7 555,8 1 000,0 60,3 100,00 A H1.0 A H1.0_L 1 4 – 295,3 44,1 40,8 100,00 A 1.7.2015 EN Official Journal of the European Union L 168/813ACFT_ID OP_TYPE PROF_ID1 PROF_ID2 PT_NUM DISTANCE ALTITUDE SPEED THR_SET OP_MODE H1.0 A H1.0_L 1 5 – 32,8 9,6 9,7 100,00 A H1.0 A H1.0_L 1 6 – 9,8 6,6 5,8 100,00 A H1.0 A H1.0_L 1 7 0,0 0,0 3,9 100,00 A H1.1 A H1.1_L 1 1 – 200 000,0 1 000,0 70,0 100,00 A H1.1 A H1.1_L 1 2 – 8 401,5 1 000,0 70,0 100,00 A H1.1 A H1.1_L 1 3 – 5 120,6 1 000,0 64,1 100,00 A H1.1 A H1.1_L 1 4 – 295,3 62,0 40,8 100,00 A H1.1 A H1.1_L 1 5 – 32,8 11,0 9,7 100,00 A H1.1 A H1.1_L 1 6 – 9,8 6,6 5,8 100,00 A H1.1 A H1.1_L 1 7 0,0 0,0 3,9 100,00 A H1.2 A H1.2_L 1 1 – 200 000,0 1 000,0 75,8 100,00 A H1.2 A H1.2_L 1 2 – 9 563,0 1 000,0 75,8 100,00 A H1.2 A H1.2_L 1 3 – 6 282,2 1 000,0 70,0 100,00 A H1.2 A H1.2_L 1 4 – 295,3 51,8 40,8 100,00 A H1.2 A H1.2_L 1 5 – 32,8 10,2 9,7 100,00 A H1.2 A H1.2_L 1 6 – 9,8 6,6 5,8 100,00 A H1.2 A H1.2_L 1 7 0,0 0,0 3,9 100,00 A H2.1 A H2.1_L 1 1 – 200 000,0 1 000,0 75,8 100,00 A H2.1 A H2.1_L 1 2 – 9 563,0 1 000,0 75,8 100,00 A H2.1 A H2.1_L 1 3 – 6 282,2 1 000,0 70,0 100,00 A H2.1 A H2.1_L 1 4 – 295,3 51,8 40,8 100,00 A H2.1 A H2.1_L 1 5 – 32,8 10,2 9,7 100,00 A H2.1 A H2.1_L 1 6 – 9,8 6,6 5,8 100,00 A L 168/814 EN Official Journal of the European Union 1.7.2015ACFT_ID OP_TYPE PROF_ID1 PROF_ID2 PT_NUM DISTANCE ALTITUDE SPEED THR_SET OP_MODE H2.1 A H2.1_L 1 7 0,0 0,0 3,9 100,00 A H2.2 A H2.2_L 1 1 – 200 000,0 1 000,0 75,8 100,00 A H2.2 A H2.2_L 1 2 – 9 604,4 1 000,0 75,8 100,00 A H2.2 A H2.2_L 1 3 – 6 323,6 1 000,0 70,0 100,00 A H2.2 A H2.2_L 1 4 – 295,3 45,2 40,8 100,00 A H2.2 A H2.2_L 1 5 – 32,8 3,6 9,7 100,00 A H2.2 A H2.2_L 1 6 – 9,8 0,0 5,8 100,00 A H2.2 A H2.2_L 1 7 0,0 0,0 3,9 100,00 A Table I-21 Noise Characteristic data for Helicopter Data Set 1 NOISE_ID THRSET_TYP MODEL_TYPE SPECT_APP SPECT_DEP SPECT_AFB H1.0 Propeller I 215 109 0 H1.1 Propeller I 215 109 0 H1.2 Propeller I 215 109 0 H2.1 Propeller I 215 109 0 H2.2 Propeller I 215 109 0 1.7.2015 EN Official Journal of the European Union L 168/815Table I-22 Noise Power Distance (NPD) data for Helicopter Data Set 1 NOISE_ NOISE_ID OP_MODE THR_SET L_200 L_400 L_630 L_1000 L_2000 L_4000 L_6300 L_10000 L_16000 L_25000 TYPE H1.0 M A 80,00 81,3 75,0 70,7 66,3 59,2 51,4 45,6 39,1 31,5 23,1 H1.0 M A 100,00 84,3 78,0 73,7 69,3 62,2 54,4 48,6 42,1 34,5 26,1 H1.0 M D 80,00 81,3 75,0 70,7 66,3 59,2 51,4 45,6 39,1 31,5 23,1 H1.0 M D 100,00 84,3 78,0 73,7 69,3 62,2 54,4 48,6 42,1 34,5 26,1 H1.0 S A 80,00 82,0 78,6 76,2 73,6 69,2 64,1 60,1 55,3 49,4 42,8 H1.0 S A 100,00 85,0 81,6 79,2 76,6 72,2 67,1 63,1 58,3 52,4 45,8 H1.0 S D 80,00 82,0 78,6 76,2 73,6 69,2 64,1 60,1 55,3 49,4 42,8 H1.0 S D 100,00 85,0 81,6 79,2 76,6 72,2 67,1 63,1 58,3 52,4 45,8 H1.1 M A 80,00 86,5 80,2 75,9 71,5 64,4 56,6 50,8 44,3 36,7 28,3 H1.1 M A 100,00 89,5 83,2 78,9 74,5 67,4 59,6 53,8 47,3 39,7 31,3 H1.1 M D 80,00 86,5 80,2 75,9 71,5 64,4 56,6 50,8 44,3 36,7 28,3 H1.1 M D 100,00 89,5 83,2 78,9 74,5 67,4 59,6 53,8 47,3 39,7 31,3 H1.1 S A 80,00 87,2 83,8 81,4 78,8 74,4 69,3 65,3 60,5 54,6 48,0 H1.1 S A 100,00 90,2 86,8 84,4 81,8 77,4 72,3 68,3 63,5 57,6 51,0 H1.1 S D 80,00 87,2 83,8 81,4 78,8 74,4 69,3 65,3 60,5 54,6 48,0 H1.1 S D 100,00 90,2 86,8 84,4 81,8 77,4 72,3 68,3 63,5 57,6 51,0 H1.2 M A 80,00 89,1 82,8 78,5 74,1 67,0 59,2 53,4 46,9 39,3 30,9 H1.2 M A 100,00 92,1 85,8 81,5 77,1 70,0 62,2 56,4 49,9 42,3 33,9 H1.2 M D 80,00 89,1 82,8 78,5 74,1 67,0 59,2 53,4 46,9 39,3 30,9 H1.2 M D 100,00 92,1 85,8 81,5 77,1 70,0 62,2 56,4 49,9 42,3 33,9 H1.2 S A 80,00 89,8 86,4 84,0 81,4 77,0 71,9 67,9 63,1 57,2 50,6 H1.2 S A 100,00 92,8 89,4 87,0 84,4 80,0 74,9 70,9 66,1 60,2 53,6 L 168/816 EN Official Journal of the European Union 1.7.2015NOISE_ NOISE_ID OP_MODE THR_SET L_200 L_400 L_630 L_1000 L_2000 L_4000 L_6300 L_10000 L_16000 L_25000 TYPE H1.2 S D 80,00 89,8 86,4 84,0 81,4 77,0 71,9 67,9 63,1 57,2 50,6 H1.2 S D 100,00 92,8 89,4 87,0 84,4 80,0 74,9 70,9 66,1 60,2 53,6 H2.1 M A 80,00 91,3 85,0 80,7 76,3 69,2 61,4 55,6 49,1 41,5 33,1 H2.1 M A 100,00 94,3 88,0 83,7 79,3 72,2 64,4 58,6 52,1 44,5 36,1 H2.1 M D 80,00 91,3 85,0 80,7 76,3 69,2 61,4 55,6 49,1 41,5 33,1 H2.1 M D 100,00 94,3 88,0 83,7 79,3 72,2 64,4 58,6 52,1 44,5 36,1 H2.1 S A 80,00 92,0 88,6 86,2 83,6 79,2 74,1 70,1 65,3 59,4 52,8 H2.1 S A 100,00 95,0 91,6 89,2 86,6 82,2 77,1 73,1 68,3 62,4 55,8 H2.1 S D 80,00 92,0 88,6 86,2 83,6 79,2 74,1 70,1 65,3 59,4 52,8 H2.1 S D 100,00 95,0 91,6 89,2 86,6 82,2 77,1 73,1 68,3 62,4 55,8 H2.2 M A 80,00 94,3 88,0 83,7 79,3 72,2 64,4 58,6 52,1 44,5 36,1 H2.2 M A 100,00 97,3 91,0 86,7 82,3 75,2 67,4 61,6 55,1 47,5 39,1 H2.2 M D 80,00 94,3 88,0 83,7 79,3 72,2 64,4 58,6 52,1 44,5 36,1 H2.2 M D 100,00 97,3 91,0 86,7 82,3 75,2 67,4 61,6 55,1 47,5 39,1 H2.2 S A 80,00 95,0 91,6 89,2 86,6 82,2 77,1 73,1 68,3 62,4 55,8 H2.2 S A 100,00 98,0 94,6 92,2 89,6 85,2 80,1 76,1 71,3 65,4 58,8 H2.2 S D 80,00 95,0 91,6 89,2 86,6 82,2 77,1 73,1 68,3 62,4 55,8 H2.2 S D 100,00 98,0 94,6 92,2 89,6 85,2 80,1 76,1 71,3 65,4 58,8 Helicopter Noise and Performance Data Set 2 Data is provided for three helicopter classes, based on maximum take-off mass: 1. Light helicopter (LHEL) MTOM < 3 000 kg 2. Medium helicopter (MHEL) 3 000 kg < MTOM < 6 000 kg 3. Heavy helicopter (THEL) MTOM > 6 000 kg 1.7.2015 EN Official Journal of the European Union L 168/817Default arrival and departure flight profiles are provided as fixed point profiles. Default departure flight profiles assume climb to a level flight altitude of 1 000 ft (305 m) for each helicopter class. Where the level flight portion on departure or arrival differs locally from these values, it is recommended that the default profiles are adapted to reflect local circum­ stances. Table I-23 Helicopter Data Set 2 Description Table Number Max Max Sea Level Approach Departure Lateral Dir­ Weight Owner MGTOW MGLW Noise NPD_ ACFT_ID Description EngineTYPE of Landing Static Thrust Power Parameter Spectral Spectral ectivity Class Category (lb) (lb) Chapter ID Engines Dist (ft) (lb) Class ID Class ID Indentifier LHEL Helicopters with Turboprop 0 0 Helicopter 0 0 0 100 0 LHEL SHP (% of Max 215 112 Prop MTOM ≤ 1 t Static Thrust) MHEL Helicopters with Turboprop 0 0 Helicopter 0 0 0 100 0 MHEL SHP (% of Max 215 112 Prop MTOM 1-3 t Static Thrust) THEL Helicopters with Turboprop 0 0 Helicopter 0 0 0 100 0 THEL SHP (% of Max 215 112 Prop MTOM 3-5 t Static Thrust) Table I-24 Helicopter Data Set 2 Departure Profiles Corrected Net ACFT_ID Op Type Profile ID Stage Length Point Number Distance (ft) Altitude (ft) TAS (kt) OP_MODE Thrust (%) LHEL D DEFAULT 1 1 0 0 1 50 X LHEL D DEFAULT 1 2 10 0 3 50 X LHEL D DEFAULT 1 3 20 16 5 50 X LHEL D DEFAULT 1 4 102 16 5 60 D LHEL D DEFAULT 1 5 561 30 50 60 D LHEL D DEFAULT 1 6 2 297 515 70 60 D LHEL D DEFAULT 1 7 4 032 1 001 90 70 D L 168/818 EN Official Journal of the European Union 1.7.2015Corrected Net ACFT_ID Op Type Profile ID Stage Length Point Number Distance (ft) Altitude (ft) TAS (kt) OP_MODE Thrust (%) LHEL D DEFAULT 1 8 7 014 1 001 100 70 D LHEL D DEFAULT 1 9 10 000 1 001 110 70 D MHEL D DEFAULT 1 1 0 0 1 50 D MHEL D DEFAULT 1 2 10 0 2 50 D MHEL D DEFAULT 1 3 20 16 3 50 D MHEL D DEFAULT 1 4 102 16 30 50 D MHEL D DEFAULT 1 5 561 30 60 50 D MHEL D DEFAULT 1 6 4 032 1 001 65 75 D MHEL D DEFAULT 1 7 6 785 1 001 100 75 D MHEL D DEFAULT 1 8 10 000 1 001 126 75 D THEL D DEFAULT 1 1 0 0 1 100 X THEL D DEFAULT 1 2 10 0 2 100 X THEL D DEFAULT 1 3 20 16 3 50 D THEL D DEFAULT 1 4 102 16 30 50 D THEL D DEFAULT 1 5 1 001 151 60 50 D THEL D DEFAULT 1 5 4 679 1 000 65 75 D THEL D DEFAULT 1 5 6 681 1 000 83 75 D THEL D DEFAULT 1 5 8 679 1 000 100 75 D THEL D DEFAULT 1 5 13 679 1 000 113 75 D THEL D DEFAULT 1 5 18 679 1 000 126 75 D 1.7.2015 EN Official Journal of the European Union L 168/819Table I-25 Helicopter Data Set 2 Arrival Profiles Corrected Net ACFT_ID Op Type Profile ID Stage Length Point Number Distance (ft) Altitude (ft) TAS (kt) OP_MODE Thrust (%) LHEL D DEFAULT 1 3 – 50 003 1 000 115 70 X LHEL D DEFAULT 1 4 – 9 332 1 000 113 70 X LHEL D DEFAULT 1 5 – 6 340 686 110 80 A LHEL D DEFAULT 1 6 – 4 029 443 95 80 A LHEL D DEFAULT 1 7 – 1 686 197 80 80 A LHEL D DEFAULT 1 8 – 843 108 60 80 A LHEL D DEFAULT 1 9 0 20 5 80 A LHEL D DEFAULT 1 9 102 0 3 80 A LHEL D DEFAULT 1 9 121 0 1 80 A MHEL D DEFAULT 1 2 – 40 229 1 000 135 75 X MHEL D DEFAULT 1 3 – 36 322 1 000 123 75 X MHEL D DEFAULT 1 4 – 32 411 1 000 112 75 X MHEL D DEFAULT 1 5 – 28 504 1 000 100 75 X MHEL D DEFAULT 1 6 – 22 145 1 000 90 75 X MHEL D DEFAULT 1 7 – 15 784 1 000 80 75 X MHEL D DEFAULT 1 8 – 9 426 1 000 70 75 X MHEL D DEFAULT 1 8 – 5 153 551 60 60 A MHEL D DEFAULT 1 8 – 750 89 50 60 A MHEL D DEFAULT 1 8 – 62 16 20 60 A MHEL D DEFAULT 1 8 0 10 5 60 A MHEL D DEFAULT 1 8 102 0 2 60 A L 168/820 EN Official Journal of the European Union 1.7.2015Corrected Net ACFT_ID Op Type Profile ID Stage Length Point Number Distance (ft) Altitude (ft) TAS (kt) OP_MODE Thrust (%) MHEL D DEFAULT 1 8 121 0 1 60 A MHEL D DEFAULT 1 8 – 40 229 1 000 135 75 X MHEL D DEFAULT 1 8 – 36 322 1 000 123 75 X MHEL D DEFAULT 1 8 – 32 411 1 000 112 75 X MHEL D DEFAULT 1 8 – 28 504 1 000 100 75 X MHEL D DEFAULT 1 8 – 22 145 1 000 90 75 X MHEL D DEFAULT 1 8 – 15 784 1 000 80 75 X MHEL D DEFAULT 1 8 – 9 426 1 000 70 75 X MHEL D DEFAULT 1 8 – 5 153 551 60 60 A MHEL D DEFAULT 1 8 – 750 89 50 60 A MHEL D DEFAULT 1 8 – 62 16 20 60 A MHEL D DEFAULT 1 8 0 10 5 60 A MHEL D DEFAULT 1 8 102 0 2 60 A MHEL D DEFAULT 1 8 121 0 1 60 A Table I-26 Noise Characteristic data for Helicopter Data Set 2 NOISE_ID THRSET_TYP MODEL_TYPE SPECT_APP SPECT_DEP SPECT_AFB LHEL P I 215 109 0 MHEL P I 215 109 0 THEL P I 215 109 0 1.7.2015 EN Official Journal of the European Union L 168/821Table I-27 Noise Power Distance (NPD) data for three helicopter classes NPD Identi­ Noise Power Op Mode L _200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft fier Descriptor Setting LHEL MAX 80 A 84,6 79,1 75,7 71,6 65,8 60,1 56 48,8 41,6 34,4 LHEL MAX 70 X 88,4 82,9 79,5 75,6 70,3 65 61,6 55,4 49,2 43 LHEL MAX 60 D 83,6 78,2 75,1 70,3 66,5 61,7 58,9 53,3 47,7 42,1 LHEL MAX 50 S 91,7 85,3 81,5 76,5 69,4 61,5 56,5 49,6 42,7 35,8 LHEL SEL 80 A 90,5 87,1 84,9 82,1 77,6 72,1 67,9 62,4 56,9 51,4 LHEL SEL 70 X 90,4 87 84,7 81,9 77,5 72 68,1 62,9 57,7 52,5 LHEL SEL 60 D 85,9 82,5 80,4 77,7 73,4 68,4 64,6 59,6 54,6 49,6 LHEL SEL 50 S 85,9 82,5 80,4 77,7 73,4 68,4 64,6 59,6 54,6 49,6 MHEL MAX 50 D 91,8 85,2 80,6 75,7 67,5 58,1 51,2 42,6 34 25,4 MHEL MAX 60 A 90,2 83,9 80 75,3 68,4 60,9 55,8 49,5 43,2 36,9 MHEL MAX 75 X 92,4 86 82 77,2 70 62,3 57,1 50,8 44,5 38,2 MHEL SEL 50 D 91,2 87,2 84,8 80,8 75 68,1 63,7 57,6 51,5 45,4 MHEL SEL 60 A 94,2 90,1 88,1 84,7 80 74,7 71,3 66 60,7 55,4 MHEL SEL 75 X 89,3 85,3 82,8 78,9 73,1 66,6 62,6 57 51,4 45,8 THEL MAX 50 D 91,2 85,2 81,7 76,3 68,8 60,4 54,9 46 37,1 28,2 THEL MAX 60 A 90 84,1 80,7 75,5 68,5 60,6 55,3 48 40,7 33,4 THEL MAX 75 X 92,4 86,4 82,9 77,5 70,1 61,6 55,7 48,1 40,5 32,9 THEL MAX 100 S 100,2 93,8 90,3 84,9 77,5 69,3 64,3 56,5 48,7 40,9 THEL SEL 50 D 92,8 89,3 87,4 84 79,2 73,5 69,6 63,7 57,8 51,9 L 168/822 EN Official Journal of the European Union 1.7.2015NPD Identi­ Noise Power Op Mode L _200ft L_400ft L_630ft L_1000ft L_2000ft L_4000ft L_6300ft L_10000ft L_16000ft L_25000ft fier Descriptor Setting THEL SEL 60 A 91,6 88,2 86,4 83,2 78,8 73,7 70 64,7 59,4 54,1 THEL SEL 75 X 94 90,5 88,6 85,2 80,5 74,7 70,4 64,8 59,2 53,6 THEL SEL 100 S 92,8 89,3 87,4 84 79,2 73,5 69,6 63,7 57,8 51,9 1.7.2015 EN Official Journal of the European Union L 168/823