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Date: 2016-01-08 Category: Draft Regulation State: Union Government Country: India

Draft amendment to CAR 66 - Licensing of Aircraft Maintenance Engineers

Issued by Ministry of Civil Aviation · Directorate General of Civil Aviation

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Okay, here is the summary of the provided document, adhering to your specifications: **Executive Summary** CAR-66 Issue II outlines the licensing requirements for aircraft maintenance engineers in India. It aims to harmonize with international standards (EASA Part 66) and details the process for obtaining, extending, and converting AME licenses. The document includes revisions to training, examination standards, and aircraft grouping provisions, becoming effective January 1, 2012, with existing CAR requirements remaining until further notice from the Director General. **Key Points / Main Content** * **General Provisions:** * CAR-66 Rev.0, dated 11th November 2011, which is primarily based on EASA Part 66 regulation is being introduced to harmonize with international requirements. * CAR-66 is based on amended Rule 61 of the Aircraft Rules, 1937. * The CAR is applicable to all personnel and organizations engaged in maintenance and/or certification of aircraft registered in India. * AME licenses in the CAR 66 pattern are available through the conversion of existing AME licenses or through the issuance of fresh licenses after passing applicable Basic Knowledge Exams. * **Licensing Requirements (Section A):** * Details scope, license categories (A, B1, B2, C), eligibility, privileges, and limitations for AME licenses. * Defines aircraft groups for rating purposes. * Requires applicants to pass 10+2 with Physics, Chemistry, and Mathematics. * Redefines syllabus for basic knowledge examination in modular pattern. * Sets experience requirements based on license category and aircraft type. * Specifies conditions for continued validity of the license (5-year renewal). * Lists the details of practical tasks to qualify an individual to obtain a type rating [Addendum II to AMC]. * **Examination and Training:** * Specifies basic knowledge requirements and examination standards in Appendix I and II, including modularisation of subjects. * Outlines type training requirements in Appendix III, including theoretical and practical elements, and requirements for On-the-Job Training (OJT). * Amends AMCs and GMs related to type / task training to Endorsement with aircraft rating. * Requires training and examinations to be completed within 10 years prior to application. * Credits expire 10 years after they were granted to the applicant by the DGCA. * **Conversion Provisions:** * Details the process for converting existing AME licenses to CAR 66 licenses, with or without limitations. * Has a provision to convert the existing AME licence to CAR 66 licence with or without limitation. **Impact Analysis** **Aircraft Maintenance Engineers (AMEs):** * **Impact:** New and existing AMEs must meet revised requirements for licensing, training, and experience. They may need to undergo additional training or examinations. * **Action Required:** AMEs must review their qualifications, identify any gaps, and take necessary steps to comply with CAR-66, including converting their licenses, completing additional training, and passing examinations. **Maintenance Organizations:** * **Impact:** Maintenance organizations must ensure their personnel meet the new licensing requirements and that their training programs align with CAR-66 standards. * **Action Required:** Organizations must adapt their training programs, update procedures to reflect CAR-66 changes, and assist employees in meeting the new licensing requirements. **Directorate General of Civil Aviation (DGCA):** * **Impact:** The DGCA is responsible for implementing and enforcing CAR-66, approving training programs, conducting examinations, and issuing licenses. * **Action Required:** DGCA must ensure its processes and resources are aligned with CAR-66, provide guidance to stakeholders, and oversee compliance.

Key Entities Referenced

CAR-66: Civil Aviation Requirement 66, which regulates the licensing of Aircraft Maintenance Engineers in India. Directorate General of Civil Aviation (DGCA): The primary aviation regulatory body in India, responsible for enforcing the CAR-66 requirements. Aircraft Rules, 1937: Referenced rule based on which CAR 66 is issued; defines certain requirements for aircraft. CAR 145: Civil Aviation Requirement 145, concerning Approved Maintenance Organisations. EASA Part 66: European standard for aircraft maintenance licensing, used as a basis for CAR-66.
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CAR-66 CAR – 66 ISSUE II LICENSING OF AIRCRAFT MAINTENANCE ENGINEERS DIRECTORATE GENERAL OF CIVIL AVIATION TECHNICAL CENTRE, OPP SAFDURJUNG AIRPORT, NEW DELHI Page 1 of 180CAR-66 Salient Features of the CAR-66 The CAR-66 (cid:45) has been drafted in line with the current Rule 61 and to harmonize the aircraft maintenance personnel licensing system with EASA Part 66 [General] (cid:45) details, requirements for qualifying an individual to obtain an Aircraft Maintenance Engineer’s Licence and extension of such licence [CAR-66] (cid:45) eliminates the system of obtaining Airframe, Engine, Electrical, Instrument and Ra- dio System Licences separately [66.A.03] (cid:45) redefines the syllabus for basic knowledge examination in modular pattern [66.A.25] (cid:45) provides for qualifying under the existing system of obtaining the licence till De- cember 2012 [66.A.70] (cid:45) provides for endorsement of an AME licence after successful completion of type training and the type training examination/type examination which shall consist of both theoretical and practical examinations [66.A.45 (c)] (cid:45) lists the details of practical tasks to qualify an individual to obtain a type rating [Ad- dendum II to AMC] (cid:45) provides for acquiring group type rating of aircraft and certification privileges 66.A.45 (a) (cid:45) has a provision to convert the existing AME licence to CAR 66 licence [66.A.70] with or without limitation Page 2 of 180 Issue II datedCAR-66 GENERAL In order to harmonize Indian requirements for licensing of aircraft maintenance engi- neers with international requirements; CAR-66 Rev.0 dated 11th November 2011, which is primarily based on EASA Part 66 regulation is being introduced. This CAR is issued on the basis of amended Rule 61(6th amendment) of the Aircraft Rules, 1937 as notified vide GSR 1001(E) dated 22ndDecember 2010. This CAR is effective from 01.01.2012. However the existing requirements of CAR Sec- tion2 Series L will also continue till the date notified by the Director General for facili- tating smooth transition of aircraft maintenance engineer licensing system into CAR 66 pattern. The CAR-66 is applicable to all personnel / Organizations engaged in maintenance and /or certification of aircraft registered in India. The Section A of CAR-66 establishes the requirements for the issue and extension of an aircraft maintenance engineer’s license, conditions of its validity and use. It also has a provision for converting the aircraft maintenance engineer’s (AME) license issued prior to the CAR-66 coming into force. The requirements are followed by Acceptable means of compliance (AMC) and Guidance Material (GM) The AME licenses in CAR 66 pattern will be available in two different ways: a) After conversion of existing AME licenses with applicable limitation. b) Issue of fresh license after passing of applicable modules of Basic Knowledge Exam to be conducted by CEO. Page 3 of 180 Issue II datedCAR-66 Record of Revisions Initial Issue (Revision 0) 11th November 2011 This CAR 66 provides requirements for the issue of an aircraft maintenance engi- neer’s licence and conditions of its validity and use for aeroplanes and helicopters. Revision 1, 23rd April 2015 The Revision-01 to CAR 66 is being issued to revise conversion of licences issued prior to CAR-66 and examination credits. The revision also revises the License for- mat. CAR 66 Issue II ------------------ The CAR 66 Issue II is being issued to harmonise with regulations of EASA Part 66 issued till November 2015. Salient features of the CAR 66 Issue II are: 1. The training, examination, knowledge and experience requirements for the issu- ance of aircraft maintenance licences and to adapt these requirements to the complexity of the different categories of aircraft amended 2. The AMCs and GMs related to a point have been brought together for easy refer- ence purposes. 3. Provision for aircraft grouping added ( 66.A.5) 4. Requirements for completing all the module for basic knowledge within 10 year (66.A.25(b) added 5. Heading of ( 66.A.45 ) is changed from type /task training to Endorsement with aircraft rating. Related AMC and GM amended. 6. Point 66. A. 50 and related AMC added to make a provision for introducing or removal of limitation from the license 7. Existing AMCs and GMs are suitable amended. 8. Appendix -1- Basic knowledge requirements amended to revise the syllabus for knowledge examination 9. Appendix -2 -Basic examination standard have been revised Page 4 of 180 Issue II datedCAR-66 10. Appendix-3- Type examination standard have been amended, minimum standard and duration for type training, course curriculum have been intro- duced, practical elements requirements to be covered during type training added, type training examinations and assessment standard have been revised, relevant AMC and GM have been also amended/added 11. Appendix-III to AMC of CAR 66 for competency assessment of assessors added. Page 5 of 180 Issue II datedCAR-66 CONTENTS Cover Page Paragraph Description Page No General 3 Record of Revisions 4 SECTION A TECHNICAL REQUIREMENTS SUBPART AIRCRAFT MAINTENANCE ENGINEER’S LICENCE AEROPLANES AND A HELICOPTERS 66.A.01 Scope 9 66.A.03 Licence Categories 9 66.A.5 Aircraft Groups 9 66.A.10 Application 10 66.A.15 Eligibility 10 66.A.20 Privileges 10 66.A.25 Basic knowledge requirements 12 66.A.30 Basic Experience Requirements 12 Continued validity of the aircraft maintenance engi- 66.A.40 13 neer’s licence 66.A.45 Endorsement with Aircraft ratings 14 66.A.50 Limitations 15 66.A.55 Evidence of qualification 16 66.A.70 Conversion provisions 16 Appendices Appendix I Basic Knowledge Requirements 18 Appendix II Basic Examination and Standard 66 Appendix III Aircraft Type training and Examination Standard - On the job training 70 Page 6 of 180 Issue II datedCAR-66 Appendix IV Experience requirements for extending a CAR-66 Aircraft Maintenance Engineer’s Licence 89 Appendix V Applications and Formats 90 Appendix VI Aircraft Maintenance Engineer’s Licence referred to in Rule 61 of the Aircraft Rules, 1937 (CAR-66) - CA Form 26 124 Acceptable Means of Compliance (AMC) and Guidance Material to SECTION A of – CAR 66 GM 66.A.3 Licence categories 128 AMC 66.A.10 Application 128 AMC . A . 15 (a) Eligibility 128 GM 66.A.20(a) Privileges 129 AMC 66.A.20(b) 2 Privilege 131 GM 66.A.20(b)2 Privileges 133 AMC 66.A.20(b)3 Privileges 133 GM 66.A.20(b)4 Privileges 135 Basic knowledge requirements 135 GM 66.A.25 (a) AMC 66.A.30(a) Experience requirements 135 AMC 66.A.30(d) Experience requirements 136 AMC 66.A.30(e) Experience requirements 136 GM 66.A.45(b) Endorsement with aircraft ratings 136 AMC 66.A.45(e) Endorsement with aircraft ratings 137 AMC 66.A.45(d), Endorsement with aircraft ratings 138 (e)3, (f)1 and (g)1 GM 66.A.45 Endorsement with aircraft ratings 138 AMC 66.A.50(b) Limitations 140 GM 66. A. 70 Conversion Provisions 140 GM 66.A.70(c) C o n v ersion provisions 141 GM 66.A.70(d) Conversion provisions 141 Page 7 of 180 Issue II datedCAR-66 AMC to Section 1 of A ircraft Type Training and Ex amination Standard 142 Appendix III to On- the- Job Training CAR-66 AMC to Paragraph “Aircraft Type Training and Ex amination Standard 144 3.1(d ) of Appendix On-the-Job Training III to CAR-66 AMC to Paragraphs “Aircraft Type Training and Ex amination Standard 147 1(b) 3.2 and 4.2 of On- the- Job Training Appendix III to CAR-66 “Aircraft Type Training and Examination Standard 148 AMC to Paragraph On-the-Job Training 1(c) of Appendix III to CAR-66 AMC to Section 5 of “Aircraft Type Training and Examination Standard 148 Appendix III to On-the-Job Training CAR-66 AMC to Section 6 of “ A i r c raft Type Training and Examination standard 148 Appendix III to . On-the-Job Training CAR-66 AMC to Appendix Aircraft Type Training and Examination Standard 150 III to CAR-66 On-the-Job Training Appendix I to AMC Aircraft type ratings 151 of CAR 66 Appendix II to AMC Aircraft type practical experience and On-the-Jo 167 of CAR 66 Training list of task Appendix III to AMC Evaluation of the competence: assessment and assessors 173 of CAR 66 Appendix IV to AMC Fuel Tank Safety training 177 Page 8 of 180 Issue II datedCAR-66 SECTION A Technical Requirements SUBPART A AIRCRAFT MAINTENANCE ENGINEER’S LICENCE AEROPLANES AND HELICOPTERS 66. A.01 Scope This section defines the aircraft maintenance engineer’s licence and establishes the requirements for application, issue and conditions of its validity (a) 66..A.3 Licence categories (a) Aircraft maintenance licences include the following categories: - Category A - Category B1 - Category B2 - Category C (b) Categories A and B1 are subdivided into subcategories relative to combinations of aeroplanes, helicopters, turbine and piston engines. The subcategories are: - A1 and B1.1 Aeroplanes Turbine - A2 and B1.2 Aeroplanes Piston - A3 and B1.3 Helicopters Turbine - A4 and B1.4 Helicopters Piston (c) RESERVED 66.A.5 Aircraft groups For the purpose of ratings on aircraft maintenance engineers licences, aircraft shall be classified in the following groups: 1. Group 1: complex motor-powered aircraft as well as multiple engine helicop- ters, aeroplanes with maximum certified operating altitude exceeding FL290, air- craft equipped with fly-by-wire systems and other aircraft requiring an aircraft type rating when defined so by the DGCA Page 9 of 180 Issue II datedCAR-66 2. Group 2: aircraft other than those in Group 1 belonging to the following sub- groups: — sub-group 2a: single turbo-propeller engine aeroplanes — sub-group 2b: single turbine engine helicopters — sub-group 2c: single piston engine helicopters. 3. Group 3: piston engine aeroplanes other than those in Group 1. 66. A.10. Application a) An application for an aircraft maintenance engineer’s licence or change to such li- cence shall be made on CA Form 19-01/02 with necessary documents and fees to DGCA. b) Reserved. c) In addition to the documents required in points 66.A.10 (a) as appropriate, the ap- plicant for additional categories or sub-categories to an aircraft maintenance engi- neer’s licence shall submit his/her current original aircraft maintenance engi- neer’s licence to the DGCA together with CA Form 19-02. d) Reserved (f) Each application shall be supported by documentation to demonstrate compliance with the applicable theoretical knowledge, practical training and experience re- quirements at the time of application. 66. A.15.Eligibility a) The applicant must have passed 10+2 examination in Physics, Chemistry and Mathematics from a recognized board or university or its equivalent b) An applicant for an aircraft maintenance engineer’s licence shall be at least 18 years of age. 66. A.20 Privileges a) Subject to the compliance with paragraph (b), the following privileges shall apply: 1. A category A aircraft maintenance engineer’s licence permits the holder to is- sue certificates of release to service following minor scheduled line mainte- nance and simple defect rectification within the limits of tasks specifically en- dorsed on the authorization The certification privileges shall be restricted to Page 10 of 180 Issue II datedCAR-66 work that the licence holder has personally performed in a maintenance or- ganization approved by the DGCA. 2. A category B1 aircraft maintenance engineer’s licence shall permit the holder to issue certificates of release to service following — maintenance, performed on aircraft structure, including aircraft structure, power plant and mechanical and electrical sys- tems. Replacement of avionic line replaceable units, requiring simple tests to prove their serviceability shall also be included in the privileges. Category B1 shall automatically include the appropriate A subcategory. 3. A category B2 aircraft maintenance engineer’s licence shall permit the holder to issue certificates of release to service following maintenance on avionic and electrical systems. 4. RESERVED 5. A category C aircraft maintenance engineer’s licence shall permit the holder to issue certificates of release to service following base maintenance on air- craft. The privileges apply to the aircraft in its entirety in CAR 145 organiza- tion. Note: Category A, B1, B2 and C shall be type rated license b) The holder of Aircraft Maintenance Engineer license may not exercise certifi- cation privileges unless: 1. in compliance with the applicable requirements of CAR M and/or CAR 145 ; and 2. in the preceding two year period he/she has either acquired six months of maintenance experience in accordance with the privileges granted by the Air- craft Maintenance Engineer’s Licence or met the provision for the issue of ap- propriate privileges; and 3. he/she has the adequate competence to certify maintenance on the corre- sponding aircraft; and 4. he/she is able to read, write and communicate to an understandable level in the language(s) in which the technical documentation and procedures necessary to support the issue of the certificate of release to service are written. Page 11 of 180 Issue II datedCAR-66 66. A.25 Basic Knowledge requirements: a) An applicant for an aircraft maintenance engineer’s licence or the addition of a category or subcategory to such an aircraft maintenance engineer’s licence shall demonstrate by examination, a level of knowledge in the appropriate subject mod- ules in accordance with Appendix I to this CAR. The basic knowledge examination shall be conducted by Central Examination Organization of DGCA. b) The training courses and examinations shall be passed within 10 years prior to the application for an aircraft maintenance licence or the addition of a category or subcategory to such aircraft maintenance licence. Should this not be the case, ex- amination credits may however be obtained in accordance with point (d). (c) The applicant may apply to the DGCA for full or partial examination credit to the basic knowledge requirements for 1. :basic knowledge examinations that do not meet the requirement described in point (b) above; and ( 2 )any other technical qualification considered by the DGCA to be equivalent to the knowledge standard of CAR -66 Credits shall be granted in accordance with Subpart E of Section B of this CAR d) Credits expire 10 years after they were granted to the applicant by the DGCA. The applicant may apply for new credits after expiration. 66. A.30 Basic Experience requirements: a) An applicant for an aircraft maintenance engineer’s licence shall have acquired: 1. for category A and sub categories B1.2 and B1.4 four years of practical aircraft maintenance experience. 2. for category B2 and sub-categories B1.1 and B1.3 five years of practical aircraft maintenance experience. 3. for Category C with respect to large aircraft: i. three years of experience exercising category B1.1 or B1.3 or B2 privileges on large aircraft or as CAR 145 B1.1, B1.3 or B2 support staff, or, a combi- nation of both; or ii. five years of experience exercising category B1.2 or B1.4 privileges on large aircraft or as CAR 145 B1.2 or B1.4 support staff, or a combination of both; or Page 12 of 180 Issue II datedCAR-66 4. for category C with respect to non large aircraft: Three years of experience exercising category B1 or B2 privileges on non large air- craft or as CAR 145 B1 or B2 support staff, or a combination of both. b) An applicant for an extension to an aircraft maintenance engineer’s licence shall have a minimum civil aircraft maintenance experience requirement appropriate to the additional category or sub-category of licence applied for as defined in Appen- dix IV to this CAR. c) The experience shall be practical and involved with a representative cross section of maintenance tasks on aircraft. d) At least one year of the required experience shall be recent maintenance experi- ence on aircraft of the category/subcategory for which the initial aircraft mainte- nance engineer’s licence is sought. For subsequent category /subcategory addi- tions to an existing aircraft maintenance engineer’s licence, the additional recent maintenance experience required may be less than one year, but shall be at least three months. The required experience must be dependent upon the difference be- tween the licence category/subcategory held and applied for. Such additional ex- perience must be typical of the new licence category/subcategory sought. e) Twelve years of practical aircraft maintenance experience, gained outside a civil aircraft maintenance environment shall be accepted as equivalent to the require- ments laid down in (1) and (2) of Paragraph (a) above, in the relevant category sup- plemented by at least one year of recent experience in the civil aircraft maintenance environment; (f) Experience shall have been acquired within the 10 years preceding the application for an aircraft maintenance licence or the addition of a category or subcategory to such a licence. 66. A.40 Continued validity of the aircraft maintenance engineer’s licence (a) The aircraft maintenance engineer’s licence becomes invalid after five years of its last issue or change, unless the holder submits his/her aircraft maintenance engi- neer’s licence to the DGCA, in order to verify the information contained in the licence is the same as that contained in the DGCA records, pursuant to point 66. B. 120. (b) The holder of an aircraft maintenance engineer’s licence shall complete the CA Form 19-03 and submit it with the holder’s copy of the licence to the DGCA, unless the holder works in a maintenance organization approved in accordance with CAR 145 that has a procedure in its exposition where by such organisation may submit the necessary documentation on behalf of the aircraft maintenance engineer’s licence holder. Page 13 of 180 Issue II datedCAR-66 (c) Any certification privileges based upon an aircraft maintenance engineer’s licence becomes invalid as soon as the aircraft maintenance engineer’s licence is invalid. (d) The aircraft maintenance engineer’s licence is only valid when issued and/or changed by DGCA and when the holder has signed the document. 66. A.45 Endorsement with aircraft ratings a) In order to be entitled to exercise certification privileges on a specific aircraft type, the holder of an aircraft maintenance licence need to have his/her licence endorsed with the relevant aircraft ratings. — For category B1, B2 or C the relevant aircraft ratings are the following: 1. For group 1 aircraft, the appropriate aircraft type rating. 2. For group 2 aircraft, the appropriate aircraft type rating, manufacturer sub-group rating or full subgroup rating. 3. For group 3 aircraft, the appropriate aircraft type rating or full group rating. — Reserved b) The endorsement of aircraft type ratings requires the satisfactory completion of the relevant category B1, B2 or C aircraft type training. (c) In addition to the requirement of point (b), the endorsement of the first aircraft type rating within a given category/sub-category requires satisfactory completion of the cor- responding On the Job Training, as described in Appendix III to CAR-66 (d) By derogation from points (b) and (c), for group 2 and 3 aircraft, aircraft type ratings may also be granted after: — satisfactory completion of the relevant category B1, B2 or C aircraft type examination described in Appendix III to this Annex (CAR-66), and — in the case of B1 and B2 category, demonstration of practical experience on the air- craft type. In that case, the practical experience shall include a representative cross sec- tion of maintenance activities relevant to the licence category. (e) For group 2 aircraft: 1. the endorsement of manufacturer sub-group ratings for category B1 and C licence holders requires complying with the aircraft type rating requirements of at least two aircraft types from the same manufacturer which combined are representative of the applicable manufacturer sub-group; Page 14 of 180 Issue II datedCAR-66 2. the endorsement of full sub-group ratings for category B1 and C licence holders re- quires complying with the aircraft type rating requirements of at least three aircraft types from different manufacturers which combined are representative of the applicable sub-group; 3. the endorsement of manufacturer sub-groups and full sub-group ratings for category B2 licence holders requires demonstration of practical experience which shall include a representative cross section of maintenance activities relevant to the licence category and to the applicable aircraft sub-group. (f) For group 3 aircraft: 1. the endorsement of the full group 3 rating for category B1, B2 and C licence holders requires demonstration of practical experience, which shall include a representative cross section of maintenance activities relevant to the licence category and to the group 3. 2. for category B1, unless the applicant provides evidence of appropriate experience, the group 3 rating shall be subject to the following limitations, which shall be endorsed on the licence: — pressurised aeroplanes — metal structure aeroplanes — composite structure aeroplanes — wooden structure aeroplanes — aeroplanes with metal tubing structure covered with fabric. 66.A.50 Limitations (a) Limitations introduced on an aircraft maintenance licence are exclusions from the certification privileges and affect the aircraft in its entirety. (b) For limitations referred to in point 66.A.45, limitations shall be removed upon: 1. demonstration of appropriate experience; or after a satisfactory practical assessment performed by the DGCA. c) For limitations referred to in point 66.A.70, limitations shall be removed upon satis- factory completion of examination on those modules/subjects defined in the applicable conversion report referred to in point 66.B.300 Page 15 of 180 Issue II datedCAR-66 6. A.55 Evidence of qualification Personnel exercising certification privileges as well as support staff must produce their licence as evidence of qualification, if required by an authorized person of DGCA, within 24 hours. 66. A.70 Conversion provisions- a) The holder of a valid Aircraft Maintenance Engineer’s Licence on the date of com- ing into force of this CAR may continue to exercise the privileges of his licence and shall be issued, with or without limitation and without further examination, an Aircraft Maintenance Engineer’s Licence in the appropriate category subject to such conditions specified in Section B Subpart D b) A person undergoing a qualification process, prior to the GSR No. 1001(E) dated 22.12.2010 regarding the Rule 61 of the Aircraft Rules, 1937 shall continue to be qualified till date as specified by the Director General. The holder of a qualification gained following such qualification process may be issued an aircraft maintenance engineer’s licence subject to the conditions specified in . Section B Subpart D c) Where necessary, the aircraft maintenance engineer’s licence shall contain limita- tions in accordance with point 66. A.50 to reflect the differences between (i) the scope of the certifying staff qualification (ii) the basic knowledge requirements and the basic examination standards laid down in Appendix I and II to this CAR 66. d) Aircraft Maintenance Engineer’s Licences issued prior to this CAR coming into force in category “A” to cover Gliders, Balloons and in category “B”, “D” and “X” to cover Aircraft, Engine, propeller and items of equipment to carryout maintenance and issue ‘Certificate of Release to Service’ that could not be transferred to CAR- 66 licence ‘Type Rating’ shall be transferred to the CAR-66 licence section XIV (a) without altering the privileges hitherto exercised by the holder. Page 16 of 180 Issue II datedCAR-66 SUBPART B AIRCRAFT OTHER THAN AEROPLANES AND HELICOPTERS 66. A.100 General Until such time as this CAR specifies a requirement for certifying staff of aircraft other than aeroplanes and helicopters, the existing regulation shall apply. SUBPART C COMPONENTS 66. A. 200 General Until such time as this CAR specifies a requirement for certifying components, the exist- ing regulation shall apply. Page 17 of 180 Issue II datedCAR-66 Appendix I - Basic Knowledge Requirements 1. KNOWLEDGE LEVELS - CATEGORY A, B1, B2 AND C AIRCRAFT MAINTENANCE ENGINEER’s LICENCE Basic knowledge for categories A, B1 and B2 are indicated by the allocation of knowledge levels indicators (1, 2 or 3) against each applicable subject. Category C appli- cant must shall meet either category B1 or B2 basic knowledge level. The knowledge level indicators are defined as follows: LEVEL 1 Familiarization with the principal elements of the subject. Objectives: (a) The applicant should be familiar with the basic elements of the subject. (b) The applicant should be able to give a simple description of the whole subject, using common words and examples. ( c) The applicant should be able to use typical terms. LEVEL 2 A general knowledge of the theoretical and practical aspects of the subject and an ability to apply that knowledge. Objectives: (a ) The applicant should be able to understand theoretical fundamentals of the subject. (b) The applicant should be able to give a general description of the subject using as appropriate, typical examples. ( c) The applicant should be able to use mathematical formulae in conjunction with physical laws describing the subject. (d) The applicant should be able to read and understand sketches, drawings and schematics describing the subject. (e) The applicant should be able to apply his knowledge in a practical manner using detailed procedures. LEVEL 3 A detailed knowledge of the theoretical and practical aspects of the subject and a capacity to combine and apply the separate elements of knowledge in a logical and comprehensive manner. Objectives: (a) The applicant should know the theory of the subject and interrelationship with other subjects. (b) The applicant should be able to give a detailed description of the subject using theoretical fundamentals and specific examples. Page 18 of 180 Issue II datedCAR-66 (c ) The applicant should understand and be able to use mathematical formulae related to the subject. (d) The applicant should be able to read, understand and prepare sketches, simple drawings and schematics describing the subject. (e) The applicant should be able to apply his knowledge in a practical manner using manufacturer's instructions. (f) The applicant should be able to interpret results from various sources and measurements and apply corrective action where appropriate. Page 19 of 180 Issue II datedCAR-66 2. MODULARISATION Qualification on basic subjects for each CAR 66 aircraft maintenance engineer’s licence category or subcategory should be in accordance with the following matrix. Applicable subjects are indicated by an ‘X’: Subject A or B1 aeroplane with A or B1 helicopter with B2 Modules Turbine en- Piston Turbine en- Piston Avionics gine (s) engine (s) gine (s) engine (s) A1 B1.1 A2 B1.2 A3 B1.3 A4 B1.4 1 Not Applicable 2 Not Applicable 3 X X X X X X X X X 4 X X X X X 5 X X X X X X X X X 6 X X X X X X X X X 7 X X X X X X X X X 8 X X X X X X X X X 9 X X X X X X X X X 10 X X X X X X X X X 11A X X 11B X X 12 X X X X 13 X 14 X 15 X X X X 16 X X X X 17 X X X X Page 20 of 180 Issue II datedCAR-66 LEVEL MODULES & SYLLABUS A B1 B2 MODULE 1. Reserved - - - MODULE 2. Reserved - - - LEVEL MODULE 3. ELECTRICAL FUNDAMENTALS A B1 B2 3.1 Electron Theory 1 1 1 Structure and distribution of electrical charges within: atoms, molecules, ions, compounds; Molecular structure of conductors, semiconductors and insulators. 3.2 Static Electricity and Conduction 1 2 2 Static electricity and distribution of electrostatic charges; Electrostatic laws of attraction and repulsion; Units of charge, Coulomb's Law; Conduction of electricity in solids, liquids, gases and a vacuum. 3.3 Electrical Terminology 1 2 2 The following terms, their units and factors affecting them: potential differ- ence, electromotive force, voltage, current, resistance, conductance, charge, conventional current flow, electron flow. 3.4 Generation of Electricity 1 1 1 Production of electricity by the following methods: light, heat, friction, pres- sure, chemical action, magnetism and motion. 3.5 DC Sources of Electricity 1 2 2 Construction and basic chemical action of: primary cells, secondary cells, lead acid cells, nickel cadmium cells, other alkaline cells; Cells connected in series and parallel; Internal resistance and its effect on a battery; Construction, materials and operation of thermocouples; Operation of photo-cells. 3.6 DC Circuits - 2 2 Ohms Law, Kirchoff's Voltage and Current Laws; Calculations using the above laws to find resistance, voltage and current; Significance of the internal resistance of a supply. 3.7 Resistance/Resistor (a) - 2 2 Resistance and affecting factors; Specific resistance; Resistor colour code, values and tolerances, preferred values, wattage rat- ings; Resistors in series and parallel; Page 21 of 180 Issue II datedCAR-66 LEVEL MODULE 3. ELECTRICAL FUNDAMENTALS A B1 B2 Calculation of total resistance using series, parallel and series parallel com- binations; Operation and use of potentiometers and rheostats; Operation of Wheatstone Bridge. (b) - 1 1 Positive and negative temperature coefficient conductance; Fixed resistors, stability, tolerance and limitations, methods of construction; Variable resistors, thermistors, voltage dependent resistors; Construction of potentiometers and rheostats; Construction of Wheatstone Bridge; 3.8 Power - 2 2 Power, work and energy (kinetic and potential); Dissipation of power by a resistor; Power formula; Calculations involving power, work and energy. 3.9 Capacitance/Capacitor - 2 2 Operation and function of a capacitor; Factors affecting capacitance area of plates, distance between plates, num- ber of plates, dielectric and dielectric constant, working voltage, voltage rat- ing; Capacitor types, construction and function; Capacitor colour coding; Calculations of capacitance and voltage in series and parallel circuits; Exponential charge and discharge of a capacitor, time constants; Testing of capacitors. 3.10 Magnetism (a) - 2 2 Theory of magnetism; Properties of a magnet Action of a magnet suspended in the Earth's magnetic field; Magnetisation and demagnetisation; Magnetic shielding; Various types of magnetic material; Electromagnets construction and principles of operation; Hand clasp rules to determine: magnetic field around current carrying con- ductor. (b) - 2 2 Magnetomotive force, field strength, magnetic flux density, permeability, hysteresis loop, retentivity, coercive force reluctance, saturation point, eddy currents; Precautions for care and storage of magnets. Page 22 of 18 0 Issue II datedCAR-66 LEVEL MODULE 3. ELECTRICAL FUNDAMENTALS A B1 B2 3.11 Inductance/Inductor - 2 2 Faraday's Law; Action of inducing a voltage in a conductor moving in a magnetic field; Induction principles; Effects of the following on the magnitude of an induced voltage: magnetic field strength, rate of change of flux, number of conductor turns; Mutual induction; The effect the rate of change of primary current and mutual inductance has on induced voltage; Factors affecting mutual inductance: number of turns in coil, physical size of coil, permeability of coil, position of coils with respect to each other; Lenz's Law and polarity determining rules; Back emf, self induction; Saturation point; Principle uses of inductors; 3.12 DC Motor/Generator Theory - 2 2 Basic motor and generator theory; Construction and purpose of components in DC generator; Operation of, and factors affecting output and direction of current flow in DC generators; Operation of, and factors affecting output power, torque, speed and direc- tion of rotation of DC motors; Series wound, shunt wound and compound motors; Starter Generator construction. 3.13 AC Theory 1 2 2 Sinusoidal waveform: phase, period, frequency, cycle; Instantaneous, average, root mean square, peak, peak to peak current values and calculations of these values, in relation to voltage, current and power Triangular/Square waves; Single/3 phase principles. 3.14 Resistive (R), Capacitive (C) and Inductive (L) Circuits - 2 2 Phase relationship of voltage and current in L, C and R circuits, parallel, se- ries and series parallel; Power dissipation in L, C and R circuits; Impedance, phase angle, power factor and current calculations; True power, apparent power and reactive power calculations. 3.15 Transformers - 2 2 Transformer construction principles and operation; Transformer losses and methods for overcoming them; Transformer action under load and no-load conditions; Power transfer, efficiency, polarity markings; Page 23 of 180 Issue II datedCAR-66 LEVEL MODULE 3. ELECTRICAL FUNDAMENTALS A B1 B2 Calculation of line and phase voltages and currents; Calculation of power in a three phase system; Primary and Secondary current, voltage, turns ratio, power, efficiency; Auto transformers. 3.16 Filters - 1 1 Operation, application and uses of the following filters: low pass, high pass, band pass, band stop. 3.17 AC Generators - 2 2 Rotation of loop in a magnetic field and waveform produced; Operation and construction of revolving armature and revolving field type AC generators; Single phase, two phase and three phase alternators; Three phase star and delta connections advantages and uses; Permanent Magnet Generators. 3.18 AC Motors - 2 2 Construction, principles of operation and characteristics of: AC synchronous and induction motors both single and polyphase; Methods of speed control and direction of rotation; Methods of producing a rotating field: capacitor, inductor, shaded or split pole. LEVEL MODULE 4. ELECTRONIC FUNDAMENTALS A B1 B2 4.1 Semiconductors 4.1.1 Diodes (a) - 2 2 Diode symbols; Diode characteristics and properties; Diodes in series and parallel; Main characteristics and use of silicon controlled rectifiers (thyristors), light emitting diode, photo conductive diode, varistor, rectifier diodes; Functional testing of diodes. (b) - - 2 Materials, electron configuration, electrical properties; P and N type materials: effects of impurities on conduction, majority and mi- nority characters; PN junction in a semiconductor, development of a potential across a PN junc- tion in unbiased, forward biased and reverse biased conditions; Diode parameters: peak inverse voltage, maximum forward current, tempera- ture, frequency, leakage current, power dissipation; Page 24 of 180 Issue II datedCAR-66 LEVEL MODULE 4. ELECTRONIC FUNDAMENTALS A B1 B2 Operation and function of diodes in the following circuits: clippers, clampers, full and half wave rectifiers, bridge rectifiers, voltage doublers and triplers; Detailed operation and characteristics of the following devices: silicon con- trolled rectifier (thyristor), light emitting diode, Shottky diode, photo conduc- tive diode, varactor diode, varistor, rectifier diodes, Zener diode. 4.1.2 Transistors (a) - 1 2 Transistor symbols; Component description and orientation; Transistor characteristics and properties. (b) - - 2 Construction and operation of PNP and NPN transistors; Base, collector and emitter configurations; Testing of transistors. Basic appreciation of other transistor types and their uses. Application of transistors: classes of amplifier (A, B, C); Simple circuits including: bias, decoupling, feedback and stabilisation; Multistage circuit principles: cascades, push-pull, oscillators, multivibrators, flip-flop circuits. 4.1.3 Integrated Circuits (a) - 1 - Description and operation of logic circuits and linear circuits/operational amplifiers. (b) - - 2 Description and operation of logic circuits and linear circuits; Introduction to operation and function of an operational amplifier used as: integrator, differentiator, voltage follower, comparator; Operation and amplifier stages connecting methods: resistive capacitive, in- ductive (transformer), inductive resistive (IR), direct; Advantages and disadvantages of positive and negative feedback. 4.2 Printed Circuit Boards - 1 2 Description and use of printed circuit boards. 4.3 Servomechanisms (a) - 1 - Understanding of the following terms: Open and closed loop systems, feed- back, follow up, analogue transducers; Principles of operation and use of the following synchro system compo- nents/features: resolvers, differential, control and torque, transformers, in- ductance and capacitance transmitters. Page 25 of 180 Issue II datedCAR-66 LEVEL MODULE 4. ELECTRONIC FUNDAMENTALS A B1 B2 (b) - - 2 Understanding of the following terms: Open and closed loop, follow up, servo- mechanism, analogue, transducer, null, damping, feedback, deadband; Construction operation and use of the following synchro system components: resolvers, differential, control and torque, E and I transformers, inductance transmitters, capacitance transmitters, synchronous transmitters; Servomechanism defects, reversal of synchro leads, hunting. LEVEL MODULE 5. DIGITAL TECHNIQUES ELECTRONIC INSTRUMENT B1.1 B1.2 SYSTEMS A B1.3 B1.4 B2 5.1 Electronic Instrument Systems 1 2 2 3 Typical systems arrangements and cockpit layout of electronic in- strument systems. 5.2 Numbering Systems - 1 - 2 Numbering systems: binary, octal and hexadecimal; Demonstration of conversions between the decimal and binary, octal and hexadecimal systems and vice versa. 5.3 Data Conversion - 1 - 2 Analogue Data, Digital Data; Operation and application of analogue to digital, and digital to ana- logue converters, inputs and outputs, limitations of various types. 5.4 Data Buses - 2 - 2 Operation of data buses in aircraft systems, including knowledge of ARINC and other specifications. 5.5 Logic Circuits (a) - 2 - 2 Identification of common logic gate symbols, tables and equivalent circuits; Applications used for aircraft systems, schematic diagrams. (b)Interpretation of logic diagrams. - - - 2 5.6 Basic Computer Structure (a) 1 2 - - Computer terminology (including bit, byte, software, hardware, CPU, IC, and various memory devices such as RAM, ROM, PROM); Computer technology (as applied in aircraft systems). (b) - - - 2 Computer related terminology; Operation, layout and interface of the major components in a micro computer including their associated bus systems; Page 26 of 180 Issue II datedCAR-66 LEVEL MODULE 5. DIGITAL TECHNIQUES ELECTRONIC INSTRUMENT B1.1 B1.2 SYSTEMS A B1.3 B1.4 B2 Information contained in single and multi address instruction words; Memory associated terms; Operation of typical memory devices; Operation, advantages and disadvantages of the various data storage systems. 5.7 Microprocessors - - - 2 Functions performed and overall operation of a microprocessor; Basic operation of each of the following microprocessor elements: control and processing unit, clock, register, arithmetic logic unit. 5.8 Integrated Circuits - - - 2 Operation and use of encoders and decoders Function of encoder types Uses of medium, large and very large scale integration. 5.9 Multiplexing - - - 2 Operation, application and identification in logic diagrams of multi- plexers and demultiplexers. 5.10 Fibre Optics - 1 1 2 Advantages and disadvantages of fibre optic data transmission over electrical wire propagation; Fibre optic data bus; Fibre optic related terms; Terminations; Couplers, control terminals, remote terminals; Application of fibre optics in aircraft systems. 5.11 Electronic Displays - 2 - 2 Principles of operation of common types of displays used in modern aircraft, including Cathode Ray Tubes, Light Emitting Diodes and Liquid Crystal Display. 5.12 Electrostatic Sensitive Devices 1 2 2 2 Special handling of components sensitive to electrostatic discharges; Awareness of risks and possible damage, component and personnel anti-static protection devices. 5.13 Software Management Control - 2 1 2 Awareness of restrictions, airworthiness requirements and possible catastrophic effects of unapproved changes to software programmes. Page 27 of 18 0 Issue II datedCAR-66 LEVEL MODULE 5. DIGITAL TECHNIQUES ELECTRONIC INSTRUMENT B1.1 B1.2 SYSTEMS A B1.3 B1.4 B2 5.14 Electromagnetic Environment - 2 2 2 Influence of the following phenomena on maintenance practices for electronic system: EMC-Electromagnetic Compatibility EMI-Electromagnetic Interference HIRF-High Intensity Radiated Field Lightning/lightning protection 5.15 Typical Electronic/Digital Aircraft Systems - 2 2 2 General arrangement of typical electronic/digital aircraft systems and associated BITE (Built In Test Equipment) testing such as: ACARS-ARINC Communication and Addressing and Reporting System ECAM-Electronic Centralised Aircraft Monitoring EFIS-Electronic Flight Instrument System EICAS-Engine Indication and Crew Alerting System FBW-Fly by Wire FMS-Flight Management System GPS-Global Positioning System IRS-Inertial reference system TCAS-Traffic Collission Avoidance system Integrated modular Avionica Cabin System Information system LEVEL MODULE 6. MATERIALS AND HARDWARE A B1 B2 6.1 Aircraft Materials — Ferrous (a) 1 2 1 Characteristics, properties and identification of common alloy steels used in aircraft; Heat treatment and application of alloy steels; (b) - 1 1 Testing of ferrous materials for hardness, tensile strength, fatigue strength and impact resistance. 6.2 Aircraft Materials — Non-Ferrous (a) 1 2 1 Characteristics, properties and identification of common non-ferrous materi- als used in aircraft; Heat treatment and application of non-ferrous materials; (b) - 1 1 Page 28 of 180 Issue II datedCAR-66 LEVEL MODULE 6. MATERIALS AND HARDWARE A B1 B2 Testing of non-ferrous material for hardness, tensile strength, fatigue strength and impact resistance. 6.3 Aircraft Materials - Composite and Non- Metallic 6.3.1 Composite and non-metallic other than wood and fabric (a) Characteristics, properties and identification of common composite and non- 1 2 2 metallic materials, other than wood, used in aircraft; Sealant and bonding agents. (b) 1 2 - The detection of defects/deterioration in composite and non-metallic materi- al. Repair of composite and non-metallic material. 6.3.2 Wooden structures 1 2 - Construction methods of wooden airframe structures; Characteristics, properties and types of wood and glue used in aeroplanes; Preservation and maintenance of wooden structure; Types of defects in wood material and wooden structures; The detection of defects in wooden structure; Repair of wooden structure. 6.3.3 Fabric covering 1 2 - Characteristics, properties and types of fabrics used in aeroplanes; Inspections methods for fabric; Types of defects in fabric; Repair of fabric covering. 6.4 Corrosion (a) 1 1 1 Chemical fundamentals; Formation by, galvanic action process, microbiological, stress; (b) 2 3 2 Types of corrosion and their identification; Causes of corrosion; Material types, susceptibility to corrosion. 6.5 Fasteners 6.5.1 Screw threads 2 2 2 Screw nomenclature; Thread forms, dimensions and tolerances for standard threads used in air- craft; Measuring screw threads; Page 29 of 180 Issue II datedCAR-66 LEVEL MODULE 6. MATERIALS AND HARDWARE A B1 B2 6.5.2 Bolts, studs and screws 2 2 2 Bolt types: specification, identification and marking of aircraft bolts, interna- tional standards; Nuts: self locking, anchor, standard types; Machine screws: aircraft specifications; Studs: types and uses, insertion and removal; Self tapping screws, dowels. 6.5.3 Locking devices 2 2 2 Tab and spring washers, locking plates, split pins, palnuts, wire locking, quick release fasteners, keys, circlips, cotter pins. 6.5.4 Aircraft rivets 1 2 1 Types of solid and blind rivets: specifications and identification, heat treat- ment. 6.6 Pipes and Unions (a) 2 2 2 Identification of, and types of rigid and flexible pipes and their connectors used in aircraft; (b) 2 2 1 Standard unions for aircraft hydraulic, fuel, oil, pneumatic and air system pipes. 6.7 Springs - 2 1 Types of springs, materials, characteristics and applications. 6.8 Bearings 1 2 2 Purpose of bearings, loads, material, construction; Types of bearings and their application. 6.9 Transmissions 1 2 2 Gear types and their application; Gear ratios, reduction and multiplication gear systems, driven and driving gears, idler gears, mesh patterns; Belts and pulleys, chains and sprockets. 6.10 Control Cables 1 2 1 Types of cables; End fittings, turnbuckles and compensation devices; Pulleys and cable system components; Bowden cables; Aircraft flexible control systems. 6.11 Electrical Cables and Connectors 1 2 2 Cable types, construction and characteristics; Page 30 of 180 Issue II datedCAR-66 LEVEL MODULE 6. MATERIALS AND HARDWARE A B1 B2 High tension and co-axial cables; Crimping; Connector types, pins, plugs, sockets, insulators, current and voltage rating, coupling, identification codes. LEVEL MODULE 7. MAINTENANCE PRACTICES A B1 B2 7.1 Safety Precautions-Aircraft and Workshop 3 3 3 Aspects of safe working practices including precautions to take when working with electricity, gases especially oxygen, oils and chemicals. Also, instruction in the remedial action to be taken in the event of a fire or another accident with one or more of these hazards including knowledge on extinguishing agents. 7.2 Workshop Practices 3 3 3 Care of tools, control of tools, use of workshop materials; Dimensions, allowances and tolerances, standards of workmanship; Calibration of tools and equipment, calibration standards. 7.3 Tools 3 3 3 Common hand tool types; Common power tool types; Operation and use of precision measuring tools; Lubrication equipment and methods. Operation, function and use of electrical general test equipment; 7.4 Avionic General Test Equipment - 2 3 Operation, function and use of avionic general test equipment. 7.5 Engineering Drawings, Diagrams and Standards 1 2 2 Drawing types and diagrams, their symbols, dimensions, tolerances and pro- jections; Identifying title block information Microfilm, microfiche and computerised presentations; Specification 100 of the Air Transport Association (ATA) of America; Aeronautical and other applicable standards including ISO, AN, MS, NAS and MIL; Wiring diagrams and schematic diagrams. 7.6 Fits and Clearances 1 2 1 Drill sizes for bolt holes, classes of fits; Common system of fits and clearances; Schedule of fits and clearances for aircraft and engines; Page 31 of 180 Issue II datedCAR-66 LEVEL MODULE 7. MAINTENANCE PRACTICES A B1 B2 Limits for bow, twist and wear; Standard methods for checking shafts, bearings and other parts. 7.7 Electrical Wiring Interconnection System (EWIS) 1 3 3 Continuity, insulation and bonding techniques and testing; Use of crimp tools: hand and hydraulic operated; Testing of crimp joints; Connector pin removal and insertion; Co-axial cables: testing and installation precautions; Identification of wire types, their inspection criteria and damage tolerance. Wiring protection techniques: Cable looming and loom support, cable clamps, protective sleeving techniques including heat shrink wrapping, shielding. EWIS installations, inspection, repair, maintenance and cleanliness standards. 7.8 Riveting 1 2 - Riveted joints, rivet spacing and pitch; Tools used for riveting and dimpling; Inspection of riveted joints. 7.9 Pipes and Hoses 1 2 - Bending and belling/flaring aircraft pipes; Inspection and testing of aircraft pipes and hoses; Installation and clamping of pipes. 7.10 Springs 1 2 - Inspection and testing of springs. 7.11 Bearings 1 2 - Testing, cleaning and inspection of bearings; Lubrication requirements of bearings; Defects in bearings and their causes. 7.12 Transmissions 1 2 - Inspection of gears, backlash; Inspection of belts and pulleys, chains and sprockets; Inspection of screw jacks, lever devices, push-pull rod systems. 7.13 Control Cables 1 2 - Swaging of end fittings; Inspection and testing of control cables; Bowden cables; aircraft flexible control systems. 7.14 Material handling 7.14.1 Sheet Metal - 2 - Page 32 of 180 Issue II datedCAR-66 LEVEL MODULE 7. MAINTENANCE PRACTICES A B1 B2 Marking out and calculation of bend allowance; Sheet metal working, including bending and forming; Inspection of sheet metal work. 7.14.2 Composite and non-metallic - 2 - Bonding practices; Environmental conditions Inspection methods 7.15 Welding, Brazing, Soldering and Bonding (a) - 2 2 Soldering methods; inspection of soldered joints. (b) - 2 - Welding and brazing methods; Inspection of welded and brazed joints; Bonding methods and inspection of bonded joints. 7.16 Aircraft Weight and Balance (a) - 2 2 Centre of Gravity/Balance limits calculation: use of relevant documents; (b) - 2 - Preparation of aircraft for weighing; Aircraft weighing; 7.17 Aircraft Handling and Storage 2 2 2 Aircraft taxiing/towing and associated safety precautions; Aircraft jacking, chocking, securing and associated safety precautions; Aircraft storage methods; Refuelling/defuelling procedures; De-icing/anti-icing procedures; Electrical, hydraulic and pneumatic ground supplies. Effects of environmental conditions on aircraft handling and operation. 7.18 Disassembly, Inspection, Repair and Assembly Techniques (a) 2 3 2 Types of defects and visual inspection techniques. Corrosion removal, assessment and reprotection. (b) - 2 - General repair methods, Structural Repair Manual; Ageing, fatigue and corrosion control programmes; (c) - 2 1 Non destructive inspection techniques including, penetrant, radiographic, ed- dy current, ultrasonic and boroscope methods. 2 2 2 Page 33 of 180 Issue II datedCAR-66 LEVEL MODULE 7. MAINTENANCE PRACTICES A B1 B2 (d) Disassembly and re-assembly techniques. (e) - 2 2 Trouble shooting techniques 7.19 Abnormal Events (a) 2 2 2 Inspections following lightning strikes and HIRF penetration. (b) 2 2 - Inspections following abnormal events such as heavy landings and flight through turbulence. 7.20 Maintenance Procedures 1 2 2 Maintenance planning; Modification procedures; Stores procedures; Certification/release procedures; Interface with aircraft operation; Maintenance Inspection/Quality Control/Quality Assurance; Additional maintenance procedures. Control of life limited components LEVEL MODULE 8. BASIC AERODYNAMICS A B1 B2 8.1 Physics of the Atmosphere 1 2 2 International Standard Atmosphere (ISA), application to aerodynamics. 8.2 Aerodynamics 1 2 2 Airflow around a body; Boundary layer, laminar and turbulent flow, free stream flow, relative airflow, upwash and downwash, vortices, stagnation; The terms: camber, chord, mean aerodynamic chord, profile (parasite) drag, induced drag, centre of pressure, angle of attack, wash in and wash out, fine- ness ratio, wing shape and aspect ratio; Thrust, Weight, Aerodynamic Resultant; Generation of Lift and Drag: Angle of Attack, Lift coefficient, Drag coefficient, polar curve, stall; Aerofoil contamination including ice, snow, frost. 8.3 Theory of Flight 1 2 2 Relationship between lift, weight, thrust and drag; Glide ratio; Steady state flights, performance; Theory of the turn; Page 34 of 180 Issue II datedCAR-66 Influence of load factor: stall, flight envelope and structural limitations; Lift augmentation. 8.4 Flight Stability and Dynamics 1 2 2 Longitudinal, lateral and directional stability (active and passive). LEVEL MODULE 9. HUMAN FACTORS A B1 B2 9.1 General 1 2 2 The need to take human factors into account; Incidents attributable to human factors/human error; ‘Murphy's’ law. 9.2 Human Performance and Limitations 1 2 2 Vision; Hearing; Information processing; Attention and perception; Memory; Claustrophobia and physical access. 9.3 Social Psychology 1 1 1 Responsibility: individual and group; Motivation and de-motivation; Peer pressure; ‘Culture’ issues; Team working; Management, supervision and leadership 9.4 Factors Affecting Performance 2 2 2 Fitness/health; Stress: domestic and work related; Time pressure and deadlines; Workload: overload and underload; Sleep and fatigue, shiftwork; Alcohol, medication, drug abuse. 9.5 Physical Environment 1 1 1 Noise and fumes; Illumination; Climate and temperature; Motion and vibration; Working environment. 9.6 Tasks 1 1 1 Physical work; Page 35 of 180 Issue II datedCAR-66 LEVEL MODULE 9. HUMAN FACTORS A B1 B2 Repetitive tasks; Visual inspection; Complex systems. 9.7 Communication 2 2 2 Within and between teams; Work logging and recording; Keeping up to date, currency; Dissemination of information. 9.8 Human Error 1 2 2 Error models and theories; Types of error in maintenance tasks; Implications of errors (i.e accidents) Avoiding and managing errors. 9.9 Hazards in the Workplace 1 2 2 Recognising and avoiding hazards; Dealing with emergencies. LEVEL MODULE 10. AVIATION LEGISLATION A B1 B2 10.1 Regulatory Framework 1 1 1 Role of International Civil Aviation Organisation; The Aircraft Act and Rules made there under Role of the DGCA; Relationship between CAR-21, CAR-M, CAR-145, CAR-66, CAR 147 The Aircraft Rules ( Applicable to Aircraft Maintenance and Release) Aeronautical Information Circulars ( Applicable to Aircraft Maintenance and Release) CAR Sections 1 and 2 10.2 CAR-66 Certifying Staff - Maintenance 2 2 2 Detailed understanding of CAR-66. 10.3 CAR-145 — Approved Maintenance Organisations 2 2 2 Detailed understanding of CAR-145 and CAR M Subpart F 10.4 Aircraft Operations 1 1 1 Commercial Air Transport/Commercial Operations Air Operators Certificates; Operators Responsibilities, in particular regarding continuing airworthiness and maintenance; Documents to be carried on board; Page 36 of 180 Issue II datedCAR-66 LEVEL MODULE 10. AVIATION LEGISLATION A B1 B2 Aircraft Placarding (Markings); 10.5 Aircraft Certification (a) General - 1 1 Certification rules: such as FAA & EACS 23/25/27/29; Type Certification; Supplemental Type Certification; CAR-21 Design/Production Organisation Approvals. Aircraft Modifications and repairs approval and certification Permit to fly requirements (b) Documents - 2 2 Certificate of Airworthiness; Certificate of Registration; Noise Certificate; Weight Schedule; Radio Station Licence and Approval. 10.6 CAR-M Detail understanding of CAR 21 provisions related to Continuing 2 2 2 Airworthiness Detailed understanding of CAR-M. 10.7 Applicable National and International Requirements (a) 1 2 2 Maintenance Programme, Maintenance checks and inspections; Master Minimum Equipment Lists, Minimum Equipment List, Dispatch Deviation Lists; Airworthiness Directives; Service Bulletins, manufacturers service information; Modifications and repairs; Maintenance documentation: maintenance manuals, structural repair manual, illustrated parts catalogue, etc.; (b) - 1 1 Continuing airworthiness; Test flights; ETOPS /EDTO , maintenance and dispatch requirements; RVSM, maintenance and dispatch requirements RNP, MNPS Operations All Weather Operations, Category 2/3 operations and minimum equipment requirements. 10.8 Safety Management System 2 2 2 State Safety Programme Basic Safety Concepts Hazards & Safety Risks Page 37 of 180 Issue II datedCAR-66 LEVEL MODULE 10. AVIATION LEGISLATION A B1 B2 SMS Operation SMS Safety performance Safety Assurance 10.9 Fuel Tank Safety 2 2 2 Special Federal Aviation Regulations (SFARs) from 14 CFR SFAR 88 of the FAA and of JAA TGL 47 Concept of CDCCL, Airworthiness Limitations Items (ALI) MODULE 11A. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYS- LEVEL TEMS A1 B1.1 11.1 Theory of Flight 11.1.1 Aeroplane Aerodynamics and Flight Controls 1 2 Operation and effect of: — roll control: ailerons and spoilers; — pitch control: elevators, stabilators, variable incidence stabilisers and canards; — yaw control, rudder limiters; Control using elevons, ruddervators; High lift devices, slots, slats, flaps, flaperons; Drag inducing devices, spoilers, lift dumpers, speed brakes; Effects of wing fences, saw tooth leading edges; Boundary layer control using, vortex generators, stall wedges or leading edge de- vices; Operation and effect of trim tabs, balance and antibalance (leading) tabs, servo tabs, spring tabs, mass balance, control surface bias, aerodynamic balance panels; 11.1.2 High Speed Flight 1 2 Speed of sound, subsonic flight, transonic flight, supersonic flight, Mach number, critical Mach number, compressibility buffet, shock wave, aerody- namic heating, area rule; Factors affecting airflow in engine intakes of high speed aircraft; Effects of sweepback on critical Mach number. 11.2 Airframe Structures — General Concepts (a) 2 2 Airworthiness requirements for structural strength; Structural classification, primary, secondary and tertiary; Fail safe, safe life, damage tolerance concepts; Zonal and station identification systems; Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue; Drains and ventilation provisions; System installation provisions; Lightning strike protection provision. Aircraft bonding Page 38 of 18 0 Issue II datedCAR-66 MODULE 11A. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYS- LEVEL TEMS A1 B1.1 (b) 1 2 Construction methods of: stressed skin fuselage, formers, stringers, longerons, bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, methods of skinning, anti-corrosive protection, wing, empennage and engine at- tachments; Structure assembly techniques: riveting, bolting, bonding Methods of surface protection, such as chromating, anodising, painting; Surface cleaning. Airframe symmetry: methods of alignment and symmetry checks. 11.3 Airframe Structures — Aeroplanes 11.3.1 Fuselage (ATA 52/53/56) 1 2 Construction and pressurisation sealing; Wing, stabiliser, pylon and undercarriage attachments; Seat installation and cargo loading system; Doors and emergency exits: construction, mechanisms, operation and safety devic- es; Windows and windscreen construction and mechanisms. 11.3.2 Wings (ATA 57) 1 2 Construction; Fuel storage; Landing gear, pylon, control surface and high lift/drag attachments. 11.3.3 Stabilisers (ATA 55) 1 2 Construction; Control surface attachment. 11.3.4 Flight Control Surfaces (ATA 55/57) 1 2 Construction and attachment; Balancing — mass and aerodynamic. 11.3.5 Nacelles/Pylons (ATA 54) 1 2 Construction; Firewalls; Engine mounts. 11.4 Air Conditioning and Cabin Pressurisation (ATA 21) 11.4.1 Air supply 1 2 Sources of air supply including engine bleed, APU and ground cart; 11.4.2 Air Conditioning 1 3 Air conditioning systems; Page 39 of 18 0 Issue II datedCAR-66 MODULE 11A. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYS- LEVEL TEMS A1 B1.1 Air cycle and vapour cycle machines Distribution systems; Flow, temperature and humidity control system. 11.4.3 Pressurisation 1 3 Pressurisation systems; Control and indication including control and safety valves; Cabin pressure controllers. 11.4.4 Safety and warning devices 1 3 Protection and warning devices. 11.5 Instruments/Avionic Systems 11.5.1 Instrument Systems (ATA 31) 1 2 Pitot static: altimeter, air speed indicator, vertical speed indicator; Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal situa- tion indicator, turn and slip indicator, turn coordinator; Compasses: direct reading, remote reading; Angle of attack indication, stall warning systems; Glass Cockpit Other aircraft system indication. 11.5.2 Avionic Systems 1 1 Fundamentals of system lay-outs and operation of; Auto Flight (ATA 22); Communications (ATA 23); Navigation Systems (ATA 34). 11.6 Electrical Power (ATA 24) 1 3 Batteries Installation and Operation; DC power generation; AC power generation; Emergency power generation; Voltage regulation; Power distribution; Inverters, transformers, rectifiers; Circuit protection. External/Ground power; 11.7 Equipment and Furnishings (ATA 25) (a) 2 2 Emergency equipment requirements; Seats, harnesses and belts. Page 40 of 180 Issue II datedCAR-66 MODULE 11A. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYS- LEVEL TEMS A1 B1.1 (b) 1 1 Cabin lay-out; Equipment lay-out; Cabin Furnishing Installation; Cabin entertainment equipment; Galley installation; Cargo handling and retention equipment; Airstairs. 11.8 Fire Protection (ATA 26) (a) 1 3 Fire and smoke detection and warning systems; Fire extinguishing systems; System tests. (b) 1 1 Portable fire extinguisher 11.9 Flight Controls (ATA 27) 1 3 Primary controls: aileron, elevator, rudder, spoiler; Trim control; Active load control; High lift devices; Lift dump, speed brakes; System operation: manual, hydraulic, pneumatic, electrical, fly-by-wire; Artificial feel, Yaw damper, Mach trim, rudder limiter, gust locks systems; Balancing and rigging; Stall protection/warning system. 11.10 Fuel Systems (ATA 28) 1 3 System lay-out; Fuel tanks; Supply systems; Dumping, venting and draining; Cross-feed and transfer; Indications and warnings; Refuelling and defuelling; Longitudinal balance fuel systems. 11.11 Hydraulic Power (ATA 29) 1 3 System lay-out; Hydraulic fluids; Hydraulic reservoirs and accumulators; Pressure generation: electric, mechanical, pneumatic; Emergency pressure generation; Filters Page 41 of 180 Issue II datedCAR-66 MODULE 11A. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYS- LEVEL TEMS A1 B1.1 Pressure Control; Power distribution; Indication and warning systems; Interface with other systems. 11.12 Ice and Rain Protection (ATA 30) 1 3 Ice formation, classification and detection; Anti-icing systems: electrical, hot air and chemical; De-icing systems: electrical, hot air, pneumatic and chemical; Rain repellant; Probe and drain heating. Wiper systems 11.13 Landing Gear (ATA 32) 2 3 Construction, shock absorbing; Extension and retraction systems: normal and emergency; Indications and warning; Wheels, brakes, antiskid and autobraking; Tyres; Steering. Air-ground sensing 11.14 Lights (ATA 33) 2 3 External: navigation, anti-collision, landing, taxiing, ice; Internal: cabin, cockpit, cargo; Emergency. 11.15 Oxygen (ATA 35) 1 3 System lay-out: cockpit, cabin; Sources, storage, charging and distribution; Supply regulation; Indications and warnings; 11.16 Pneumatic/Vacuum (ATA 36) 1 3 System lay-out; Sources: engine/APU, compressors, reservoirs, ground supply; Pressure control; Distribution; Indications and warnings; Interfaces with other systems. 11.17 Water/Waste (ATA 38) 2 3 Water system lay-out, supply, distribution, servicing and draining; Toilet system lay-out, flushing and servicing; Corrosion aspects. Page 42 of 180 Issue II datedCAR-66 MODULE 11A. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYS- LEVEL TEMS A1 B1.1 11.18 On Board Maintenance Systems (ATA 45) 1 2 Central maintenance computers; Data loading system; Electronic library system; 1 2 Printing; Structure monitoring (damage tolerance monitoring). 1 2 11.19 Integrated Modular Avionics (ATA42 ) Functions that may be typically integrated in the Integrated Modular Avionic (IMA) modules are, among others: Bleed Management, Air Pressure Control, Air Ventila- tion and Control, Avionics and Cockpit Ventilation Control, Temperature Control, Air Traffic Communication, Avionics Communication Router, Electrical Load Man- agement, Circuit Breaker Monitoring, Electrical System BITE, Fuel Management, Braking Control, Steering Control, Landing Gear Extension and Retraction, Tyre Pressure Indication, Oleo Pressure Indication, Brake Temperature Monitoring, etc. 11.20 Cabin Systems (ATA44) The units and components which furnish a means of entertaining the passengers and providing communication within the aircraft (Cabin Intercommunication Data 1 2 System) and between the aircraft cabin and ground stations (Cabin Network Ser- vice). Includes voice, data, music and video transmissions. The Cabin Intercommunication Data System provides an interface between cock- pit/cabin crew and cabin systems. These systems support data exchange of the dif- ferent related LRU's and they are typically operated via Flight Attendant Panels. The Cabin Network Service typically consists on a server, typically interfacing with, among others, the following systems: — Data/Radio Communication, In-Flight Entertainment System. The Cabin Network Service may host functions such as: — Access to pre-departure/departure reports, — E-mail/intranet/Internet access, — Passenger database; Cabin Core System; In-flight Entertainment System; External Communication System; Cabin Mass Memory System; Cabin Monitoring System; Miscellaneous Cabin System. 11.21 Information Systems (ATA46) The units and components which furnish a means of storing, updating and retriev- ing digital information traditionally provided on paper, microfilm or microfiche. 1 2 Includes units that are dedicated to the information storage and retrieval function Page 43 of 180 Issue II datedCAR-66 MODULE 11A. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYS- LEVEL TEMS A1 B1.1 such as the electronic library mass storage and controller. Does not include units or components installed for other uses and shared with other systems, such as flight deck printer or general use display. Typical examples include Air Traffic and Information Management Systems and Network Server Systems Aircraft General Information System; Flight Deck Information System; Maintenance Information System; Passenger Cabin Information System; Miscellaneous Information System. MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYS- LEVELL TEMS A2 B1.2 Note: The scope of this Module should reflect the technology of aeroplanes pertinent to the A2 and B1.2 subcategory. 11.1 Theory of Flight 11.1.1 Aeroplane Aerodynamics and Flight Controls 1 2 Operation and effect of: — roll control: ailerons and spoilers; — pitch control: elevators, stabilators, variable incidence stabilisers and canards; — yaw control, rudder limiters; Control using elevons, ruddervators; High lift devices, slots, slats, flaps, flaperons; Drag inducing devices, spoilers, lift dumpers, speed brakes; Effects of wing fences, saw tooth leading edges; Boundary layer control using, vortex generators, stall wedges or leading edge de- vices; Operation and effect of trim tabs, balance and antibalance (leading) tabs, servo tabs, spring tabs, mass balance, control surface bias, aerodynamic balance panels; 11.1.2 High Speed Flight — N/A — - - 11.2 Airframe Structures — General Concepts (a) 2 2 Airworthiness requirements for structural strength; Structural classification, primary, secondary and tertiary; Fail safe, safe life, damage tolerance concepts; Zonal and station identification systems; Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue; Page 44 of 180 Issue II datedCAR-66 MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYS- LEVELL TEMS A2 B1.2 Drains and ventilation provisions; System installation provisions; Lightning strike protection provision. Aircraft bonding (b) 1 2 Construction methods of: stressed skin fuselage, formers, stringers, longerons, bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, methods of skinning, anti-corrosive protection, wing, empennage and engine at- tachments; Structure assembly techniques: riveting, bolting, bonding; Methods of surface protection, such as chromating, anodising, painting; Surface cleaning; Airframe symmetry: methods of alignment and symmetry checks. 11.3 Airframe Structures — Aeroplanes 11.3.1 Fuselage (ATA 52/53/56) 1 2 Construction and pressurisation sealing; Wing, tail-plane pylon and undercarriage attachments; Seat installation; Doors and emergency exits: construction and operation; Window and windscreen attachment. 11.3.2 Wings (ATA 57) 1 2 Construction; Fuel storage; Landing gear, pylon, control surface and high lift/drag attachments. 11.3.3 Stabilisers (ATA 55) 1 2 Construction; Control surface attachment. 11.3.4 Flight Control Surfaces (ATA 55/57) 1 2 Construction and attachment; Balancing — mass and aerodynamic. 11.3.5 Nacelles/Pylons (ATA 54) (a) 1 2 Nacelles/Pylons: — Construction; — Firewalls; — Engine mounts. 11.4 Air Conditioning and Cabin Pressurisation (ATA 21) 1 3 Page 45 of 180 Issue II datedCAR-66 MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYS- LEVELL TEMS A2 B1.2 Pressurisation and air conditioning systems; Cabin pressure controllers, protection and warning devices Heating Systems 11.5 Instruments/Avionic Systems 11.5.1 Instrument Systems (ATA 31) 1 2 Pitot static: altimeter, air speed indicator, vertical speed indicator; Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal situa- tion indicator, turn and slip indicator, turn coordinator; Compasses: direct reading, remote reading; Angle of attack indication, stall warning systems. Glass cockpit; Other aircraft system indication. 11.5.2 Avionic Systems 1 1 Fundamentals of system lay-outs and operation of: — Auto Flight (ATA 22); — Communications (ATA 23); — Navigation Systems (ATA 34). 11.6 Electrical Power (ATA 24) 1 3 Batteries Installation and Operation; DC power generation; Voltage regulation; Power distribution; Circuit protection; Inverters, transformers. 11.7 Equipment and Furnishings (ATA 25) (a) 2 2 Emergency equipment requirements; Seats, harnesses and belts. (b) 1 1 Cabin lay-out; Equipment lay-out; Cabin Furnishing Installation (level 2); Cabin entertainment equipment; Galley installation; Cargo handling and retention equipment; Airstairs. 11.8 Fire Protection (ATA 26) (a) 1 3 Page 46 of 180 Issue II datedCAR-66 MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYS- LEVELL TEMS A2 B1.2 Fire extinguishing systems; Fire and smoke detection and warning systems; System tests. (b) 1 3 Portable fire extinguisher. 11.9 Flight Controls (ATA 27) 1 3 Primary controls: aileron, elevator, rudder; Trim tabs; High lift devices; System operation: manual; Gust locks; Balancing and rigging; Stall warning system. 11.10 Fuel Systems (ATA 28) 1 3 System lay-out; Fuel tanks; Supply systems; Cross-feed and transfer; Indications and warnings; Refuelling and defuelling. 11.11 Hydraulic Power (ATA 29) 1 3 System lay-out; Hydraulic fluids; Hydraulic reservoirs and accumulators; Pressure generation: electric, mechanical; Filters Pressure Control; Power distribution; Indication and warning systems. 11.12 Ice and Rain Protection (ATA 30) 1 3 Ice formation, classification and detection; De-icing systems: electrical, hot air, pneumatic and chemical; Probe and drain heating; Wiper systems. 11.13 Landing Gear (ATA 32) 2 3 Construction, shock absorbing; Extension and retraction systems: normal and emergency; Indications and warning; Wheels, brakes, antiskid and auto braking; Page 47 of 180 Issue II datedCAR-66 MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYS- LEVELL TEMS A2 B1.2 Tyres; Steering. Air-ground sensing 11.14 Lights (ATA 33) 2 2 External: navigation, anti collision, landing, taxiing, ice; Internal: cabin, cockpit, cargo; Emergency. 11.15 Oxygen (ATA 35) 1 3 System lay-out: cockpit, cabin; Sources, storage, charging and distribution; Supply regulation; Indications and warnings; 11.16 Pneumatic/Vacuum (ATA 36) 1 3 System lay-out; Sources: engine/APU, compressors, reservoirs, ground supply; Pressure control; Distribution; Indications and warnings; Interfaces with other systems. 11.17 Water/Waste (ATA 38) 2 3 Water system lay-out, supply, distribution, servicing and draining; Toilet system lay-out, flushing and servicing; Corrosion aspects. LEVEL MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS A3 A4 B1.3 B1.4 12.1 Theory of Flight — Rotary Wing Aerodynamics 1 2 Terminology; Effects of gyroscopic precession; Torque reaction and directional control; Dissymmetry of lift, Blade tip stall; Translating tendency and its correction; Coriolis effect and compensation; Vortex ring state, power settling, overpitching; Auto-rotation; Ground effect. 12.2 Flight Control Systems 2 3 Cyclic control; Page 48 of 180 Issue II datedCAR-66 LEVEL MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS A3 A4 B1.3 B1.4 Collective control; Swashplate; Yaw control: Anti-Torque Control, Tail rotor, bleed air; Main Rotor Head: Design and Operation features; Blade Dampers: Function and construction; Rotor Blades: Main and tail rotor blade construction and attachment; Trim control, fixed and adjustable stabilisers; System operation: manual, hydraulic, electrical and flyby-wire; Artificial feel; Balancing and Rigging. 12.3 Blade Tracking and Vibration Analysis 1 3 Rotor alignment; Main and tail rotor tracking; Static and dynamic balancing; Vibration types, vibration reduction methods; Ground resonance. 12.4 Transmissions 1 3 Gear boxes, main and tail rotors; Clutches, free wheel units and rotor brake. Tail rotor drive shafts, flexible couplings, bearings, vibration dampers and bearing hangers 12.5 Airframe Structures (a) 2 2 Airworthiness requirements for structural strength; Structural classification, primary, secondary and tertiary; Fail safe, safe life, damage tolerance concepts; Zonal and station identification systems; Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue; Drains and ventilation provisions; System installation provisions; Lightning strike protection provision. (b) 1 2 Construction methods of: stressed skin fuselage, formers, stringers, longerons, bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, methods of skinning and anti-corrosive protection. Pylon, stabiliser and undercarriage attachments; Seat installation; Doors: construction, mechanisms, operation and safety devices; Windows and windscreen construction; Fuel storage; Firewalls; Page 49 of 180 Issue II datedCAR-66 LEVEL MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS A3 A4 B1.3 B1.4 Engine mounts; Structure assembly techniques: riveting, bolting, bonding; Methods of surface protection, such as chromating, anodising, painting; Surface cleaning. Airframe symmetry: methods of alignment and symmetry checks. 12.6 Air Conditioning (ATA 21) 12.6.1 Air supply 1 2 Sources of air supply including engine bleed and ground cart; 12.6.2 Air Conditioning 1 3 Air conditioning systems; Distribution systems; Flow and temperature control systems; Protection and warning devices. 12.7 Instruments/Avionic Systems 12.7.1 Instrument Systems (ATA 31) 1 2 Pitot static:altimeter, air speed indicator, vertical speed indicator; Gyroscopic:artificial horizon, attitude director, direction indicator, horizontal situa- tion indicator, turn and slip indicator, turn coordinator; Compasses: direct reading, remote reading; Vibration indicating systems — HUMS; Glass Cockpit Other aircraft system indication. 12.7.2 Avionic Systems 1 1 Fundamentals of system layouts and operation of: Auto Flight (ATA 22); Communications (ATA 23); Navigation Systems (ATA 34). 12.8 Electrical Power (ATA 24) 1 3 Batteries Installation and Operation; DC power generation, AC power generation; Emergency power generation; Voltage regulation, Circuit protection. Power distribution; Inverters, transformers, rectifiers; External/Ground power. 12.9 Equipment and Furnishings (ATA 25) (a) 2 2 Emergency equipment requirements; Seats, harnesses and belts; Page 50 of 180 Issue II datedCAR-66 LEVEL MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS A3 A4 B1.3 B1.4 Lifting systems. (b) 1 1 Emergency flotation systems; Cabin lay-out, cargo retention; Equipment lay-out; Cabin Furnishing Installation. 12.10 Fire Protection (ATA 26) 1 3 Fire and smoke detection and warning systems; Fire extinguishing systems; System tests. 12.11 Fuel Systems (ATA 28) 1 3 System lay-out; Fuel tanks; Supply systems; Dumping, venting and draining; Cross-feed and transfer; Indications and warnings; Refuelling and defuelling. 12.12 Hydraulic Power (ATA 29) 1 3 System lay-out; Hydraulic fluids; Hydraulic reservoirs and accumulators; Pressure generation: electric, mechanical, pneumatic; Emergency pressure generation; Filters Pressure Control; Power distribution; Indication and warning systems; Interface with other systems. 12.13 Ice and Rain Protection (ATA 30) 1 3 Ice formation, classification and detection; Anti-icing and de-icing systems: electrical, hot air and chemical; Rain repellant and removal; Probe and drain heating. Wiper system 12.14 Landing Gear (ATA 32) 2 3 Construction, shock absorbing; Extension and retraction systems: normal and emergency; Page 51 of 180 Issue II datedCAR-66 LEVEL MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS A3 A4 B1.3 B1.4 Indications and warning; Wheels, tyres, brakes; Steering; Air-ground sensing Skids, floats. 12.15 Lights (ATA 33) 2 3 External: navigation, landing, taxiing, ice; Internal: cabin, cockpit, cargo; Emergency. 12.16 Pneumatic/Vacuum (ATA 36) 1 3 System lay-out; Sources: engine, compressors, reservoirs, ground supply.; Pressure control; Distribution; Indications and warnings; Interfaces with other systems. 12.17 Integrated Modular Avionics (ATA42) 1 2 Functions that may be typically integrated in the Integrated Modular Avionic (IMA) modules are, among others: Bleed Management, Air Pressure Control, Air Ventilation and Control, Avionics and Cockpit Ventilation Control, Temperature Control, Air Traffic Communication, Avi- onics Communication Router, Electrical Load Management, Circuit Breaker Moni- toring, Electrical System BITE, Fuel Management, Braking Control, Steering Control, Landing Gear Extension and Retraction, Tyre Pressure Indication, Oleo Pressure Indication, Brake Temperature Monitoring, etc. Core System; Network Components. 12.18 On Board Maintenance Systems (ATA45) 1 2 Central maintenance computers; Data loading system; Electronic library system; Printing; Structure monitoring (damage tolerance monitoring). 12.19 Information Systems (ATA46) The units and components which furnish a means of storing, updating and retriev- ing digital information traditionally provided on paper, microfilm or microfiche. 1 2 Includes units that are dedicated to the information storage and retrieval function such as the electronic library mass storage and controller. Does not include units or components installed for other uses and shared with other systems, such as flight deck printer or general use display. Typical examples include Air Traffic and Information Management Systems and Network Server Systems. Page 52 of 180 Issue II datedCAR-66 LEVEL MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS A3 A4 B1.3 B1.4 Aircraft General Information System; Flight Deck Information System; Maintenance Information System; Passenger Cabin Information System; Miscellaneous Information System. LEVEL MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS B2 13.1 Theory of Flight (a) Aeroplane Aerodynamics and Flight Controls 1 Operation and effect of: — roll control: ailerons and spoilers; — pitch control: elevators, stabilators, variable incidence stabilisers and canards; — yaw control, rudder limiters; Control using elevons, ruddervators; High lift devices: slots, slats, flaps; Drag inducing devices: spoilers, lift dumpers, speed brakes; Operation and effect of trim tabs, servo tabs, control surface bias. (b) High Speed Flight 1 Speed of sound, subsonic flight, transonic flight, supersonic flight, Mach number, critical Mach number. (c) Rotary Wing Aerodynamics 1 Terminology; Operation and effect of cyclic, collective and anti-torque controls. 13.2 Structures — General Concepts (a) 1 Fundamentals of structural systems. (b) 2 Zonal and station identification systems; Electrical bonding; Lightning strike protection provision. 13.3 Autoflight (ATA 22) 3 Fundamentals of automatic flight control including working principles and current terminology; Command signal processing; Modes of operation: roll, pitch and yaw channels; Yaw dampers; Page 53 of 180 Issue II datedCAR-66 LEVEL MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS B2 Stability Augmentation System in helicopters; Automatic trim control; Autopilot navigation aids interface; Autothrottle systems. Automatic Landing Systems: principles and categories, modes of operation, approach, glideslope, land, goaround, system monitors and failure conditions. 13.4 Communication/Navigation (ATA 23/34) 3 Fundamentals of radio wave propagation, antennas, transmission lines, communication, re- ceiver and transmitter; Working principles of following systems: — Very High Frequency (VHF) communication; — High Frequency (HF) communication; — Audio; — Emergency Locator Transmitters; — Cockpit Voice Recorder; — Very High Frequency omnidirectional range (VOR); — Automatic Direction Finding (ADF); — Instrument Landing System (ILS); — Microwave Landing System (MLS); — Flight Director systems; Distance Measuring Equipment (DME); — Very Low Frequency and hyperbolic navigation(VLF/Omega); — Doppler navigation; — Area navigation, RNAV systems; — Flight Management Systems; — Global Positioning System (GPS), Global Navigation Satellite Systems (GNSS); — Inertial Navigation System; — Air Traffic Control transponder, secondary surveillance radar; — Traffic Alert and Collision Avoidance System(TCAS); — Weather avoidance radar; — Radio altimeter; — ARINC communication and reporting; 13.5 Electrical Power (ATA 24) 3 Batteries Installation and Operation; DC power generation; AC power generation; Emergency power generation; Voltage regulation; Power distribution; Page 54 of 180 Issue II datedCAR-66 LEVEL MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS B2 Inverters, transformers, rectifiers; Circuit protection; External/Ground power. 13.6 Equipment and Furnishings (ATA 25) 3 Electronic emergency equipment requirements; Cabin entertainment equipment. 13.7 Flight Controls (ATA 27) 2 (a) Primary controls: aileron, elevator, rudder, spoiler; Trim control; Active load control; High lift devices; Lift dump, speed brakes; System operation: manual, hydraulic, pneumatic; Artificial feel, Yaw damper, Mach trim, rudder limiter, gust locks. Stall protection systems. (b) System operation: electrical, fly by wire. 13.8 Instrument Systems (ATA 31) 3 Classification; Atmosphere; Terminology; Pressure measuring devices and systems; Pitot static systems; Altimeters; Vertical speed indicators; Airspeed indicators; Machmeters; Altitude reporting/alerting systems; Air data computers; Instrument pneumatic systems; Direct reading pressure and temperature gauges; Temperature indicating systems; Fuel quantity indicating systems; Gyroscopic principles; Artificial horizons; Slip indicators; Directional gyros; Ground Proximity Warning Systems; Page 55 of 180 Issue II datedCAR-66 LEVEL MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS B2 Compass systems; Flight Data Recording systems; Electronic Flight Instrument Systems; Instrument warning systems including master warning systems and centralised warning panels; Stall warning systems and angle of attack indicating systems; Vibration measurement and indication. Glass Cockpit 13.9 Lights (ATA 33) 3 External: navigation, landing, taxiing, ice; Internal: cabin, cockpit, cargo; Emergency. 13.10 On board Maintenance Systems (ATA 45) 3 Central maintenance computers; Data loading system; Electronic library system; Printing; Structure monitoring (damage tolerance monitoring). 13.11 Air Conditioning and Cabin Pressurisation (ATA21) 13.11.1. Air supply Sources of air supply including engine bleed, APU and ground cart 13.11.2. Air Conditioning Air conditioning systems; Air cycle and vapour cycle machines; Distribution systems; Flow, temperature and humidity control system. 13.11.3. Pressurisation Pressurisation systems; Control and indication including control and safety valves; Cabin pressure controllers 13.11.4. Safety and warning devices Protection and warning devices 13.12 Fire Protection (ATA 26) (a) Fire and smoke detection and warning systems; Fire extinguishing systems; System tests; (b) Portable fire extinguisher. Page 56 of 180 Issue II datedCAR-66 LEVEL MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS B2 13.13 Fuel Systems (ATA 28) System lay-out; Fuel tanks; Supply systems; Dumping, venting and draining; Cross-feed and transfer; Indications and warnings; Refuelling and defuelling; Longitudinal balance fuel systems 13.14 Hydraulic Power (ATA 29 System lay-out; Hydraulic fluids; Hydraulic reservoirs and accumulators; Pressure generation: electrical, mechanical, pneumatic; Emergency pressure generation; Filters; Pressure control; Power distribution; Indication and warning systems; Interface with other systems. 13.15 Ice and Rain Protection (ATA 30) Ice formation, classification and detection; Anti-icing systems: electrical, hot air and chemical; De-icing systems: electrical, hot air, pneumatic, chemical; Rain repellent; Probe and drain heating; Wiper Systems. 13.16 Landing Gear (ATA 32) Construction, shock absorbing; Extension and retraction systems: normal and emergency; Indications and warnings; Wheels, brakes, antiskid and autobraking; Tyres; Steering; Air-ground sensing. 13.17 Oxygen (ATA 35) System lay-out: cockpit, cabin; Sources, storage, charging and distribution; Supply regulation; Indications and warnings. 3 13.18 Pneumatic/Vacuum (ATA 36) Page 57 of 180 Issue II datedCAR-66 LEVEL MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS B2 System lay-out; Sources: engine/APU, compressors, reservoirs, ground supply; Pressure control; Distribution; Indications and warnings; Interfaces with other systems. 3 13.19 Water/Waste (ATA 38) Water system lay-out, supply, distribution, servicing and draining; Toilet system lay-out, flushing and servicing. 13.20 Integrated Modular Avionics (ATA42) Functions that may be typically integrated in the Integrated Modular Avionic (IMA) mod- ules are, among others: Bleed Management, Air Pressure Control, Air Ventilation and Control, Avionics and Cockpit Ventilation Control, Temperature Control, Air Traffic Communication, Avionics Communica- tion Router, Electrical Load Management, Circuit Breaker Monitoring, Electrical System BITE, Fuel Management, Braking Control, Steering Control, Landing Gear Extension and Re- traction, Tyre Pressure Indication, Oleo Pressure Indication, Brake Temperature Monitor- ing, etc.; Core System; Network Components. 13.21 Cabin Systems (ATA44) The units and components which furnish a means of entertaining the passengers and providing communication within the aircraft (Cabin Intercommunication Data System) and between the aircraft cabin and ground stations (Cabin Network Service). Includes voice, da- ta, music and video transmissions. The Cabin Intercommunication Data System provides an interface between cockpit/cabin crew and cabin systems. These systems support data exchange of the different related LRU's and they are typically operated via Flight Attendant Panels. The Cabin Network Service typically consists on a server, typically interfacing with, among others, the following systems : — Data/Radio Communication, In-Flight Entertainment System. — The Cabin Network Service may host functions such as: — Access to pre-departure/departure reports, — E-mail/intranet/Internet access, — Passenger database; Cabin Core System; In-flight Entertainment System; External Communication System; Cabin Mass Memory System; Cabin Monitoring System; Miscellaneous Cabin System. 13.22 Information Systems (ATA46) The units and components which furnish a means of storing, updating and retrieving digital Page 58 of 180 Issue II datedCAR-66 LEVEL MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS B2 information traditionally provided on paper, microfilm or microfiche. Includes units that are dedicated to the information storage and retrieval function such as the electronic library mass storage and controller. Does not include units or components installed for other uses and shared with other systems, such as flight deck printer or general use display. Typical examples include Air Traffic and Information Management Systems and Network Server Systems. Aircraft General Information System; Flight Deck Information System; Maintenance Information System; Passenger Cabin Information System; Miscellaneous Information System. LEVEL MODULE 14 PR..OPULSION B2 14.1 Turbine Engines (a) 1 Constructional arrangement and operation of turbojet, turbofan, turboshaft and turbopropeller engines; (b) 2 Electronic Engine control and fuel metering systems (FADEC). 14.2 Engine Indicating Systems 2 Exhaust gas temperature/Interstage turbine temperature systems; Engine speed; Engine Thrust Indication: Engine Pressure Ratio, engine turbine discharge pressure or jet pipe pressure systems; Oil pressure and temperature; Fuel pressure, temperature and flow; Manifold pressure; Engine torque; Propeller speed. 14.3 Starting and Ignition Systems Operation of engine start systems and components; Ignition systems and components; Maintenance safety requirements LEVEL MODULE 15. GAS TURBINE ENGINE A1 B1.1 A3 B1.3 15.1 Fundamentals 1 2 Potential energy, kinetic energy, Newton's laws of motion, Brayton cycle; The relationship between force, work, power, energy, velocity, acceleration; Page 59 of 180 Issue II datedCAR-66 LEVEL MODULE 15. GAS TURBINE ENGINE A1 B1.1 A3 B1.3 Constructional arrangement and operation of turbojet, turbofan, turboshaft, turbo- prop. 15.2 Engine Performance X 2 Gross thrust, net thrust, choked nozzle thrust, thrust distribution, resultant thrust, thrust horsepower, equivalent shaft horsepower, specific fuel consumption; Engine efficiencies; By-pass ratio and engine pressure ratio; Pressure, temperature and velocity of the gas flow; Engine ratings, static thrust, influence of speed, altitude and hot climate, flat rating, limitations. 15.3 Inlet 2 2 Compressor inlet ducts Effects of various inlet configurations; Ice protection. 15.4 Compressors 1 2 Axial and centrifugal types; Constructional features and operating principles and applications; Fan balancing; Operation: Causes and effects of compressor stall and surge; Methods of air flow control: bleed valves, variable inlet guide vanes, variable stator vanes, rotating stator blades; Compressor ratio. 15.5 Combustion Section 1 2 Constructional features and principles of operation. 15.6 Turbine Section 2 2 Operation and characteristics of different turbine blade types; Blade to disk attachment; Nozzle guide vanes; Causes and effects of turbine blade stress and creep. 15.7 Exhaust 1 2 Constructional features and principles of operation; Convergent, divergent and variable area nozzles; Engine noise reduction; Thrust reversers. 15.8 Bearings and Seals X 2 Constructional features and principles of operation. 15.9 Lubricants and Fuels Page 60 of 180 Issue II datedCAR-66 LEVEL MODULE 15. GAS TURBINE ENGINE A1 B1.1 A3 B1.3 Properties and specifications; Fuel additives; Safety precautions. 15.10 Lubrication Systems 1 2 System operation/lay-out and components. 15.11 Fuel Systems 1 2 Operation of engine control and fuel metering systems including electronic engine control (FADEC); Systems lay-out and components. 15.12 Air Systems 1 2 Operation of engine air distribution and anti-ice control systems, including internal cooling, sealing and external air services. 15.13 Starting and Ignition Systems 1 2 Operation of engine start systems and components; Ignition systems and components; Maintenance safety requirements. 15.14 Engine Indication Systems 1 2 Exhaust Gas Temperature/Interstage Turbine Temperature; Engine Thrust Indication: Engine Pressure Ratio, engine turbine discharge pressure or jet pipe pressure systems; Oil pressure and temperature; Fuel pressure and flow; Engine speed; Vibration measurement and indication; Torque; Power. 15.15 Power Augmentation Systems - 1 Operation and applications; Water injection, water methanol; Afterburner systems. 15.16 Turbo-prop Engines 1 2 Gas coupled/free turbine and gear coupled turbines; Reduction gears; Integrated engine and propeller controls; Overspeed safety devices. 15.17 Turbo-shaft engines 1 2 Page 61 of 180 Issue II datedCAR-66 LEVEL MODULE 15. GAS TURBINE ENGINE A1 B1.1 A3 B1.3 Arrangements, drive systems, reduction gearing, couplings, control systems. 15.18 Auxiliary Power Units (APUs) 1 2 Purpose, operation, protective systems. 15.19 Powerplant Installation 1 2 Configuration of firewalls, cowlings, acoustic panels, engine mounts, anti-vibration mounts, hoses, pipes, feeders, connectors, wiring looms, control cables and rods, lifting points and drains. 15.20 Fire Protection Systems 1 2 Operation of detection and extinguishing systems. 15.21 Engine Monitoring and Ground Operation 1 3 Procedures for starting and ground run-up; Interpretation of engine power output and parameters; Trend (including oil analysis, vibration and boroscope) monitoring; Inspection of engine and components to criteria, tolerances and data specified by engine manufacturer; Compressor washing/cleaning; Foreign Object Damage. 15.22 Engine Storage and Preservation - 2 Preservation and depreservation for the engine and accessories/ systems. LEVEL MODULE 16. PISTON ENGINE A2 B1.2 A4 B1.4 16.1 Fundamentals 1 2 Mechanical, thermal and volumetric efficiencies; Operating principles — 2 stroke, 4 stroke, Otto and Diesel; Piston displacement and compression ratio; Engine configuration and firing order. 16.2 Engine Performance 1 2 Power calculation and measurement; Factors affecting engine power; Mixtures/leaning, pre-ignition. 16.3 Engine Construction 1 2 Crank case, crank shaft, cam shafts, sumps; Accessory gearbox; Cylinder and piston assemblies; Page 62 of 180 Issue II datedCAR-66 LEVEL MODULE 16. PISTON ENGINE A2 B1.2 A4 B1.4 Connecting rods, inlet and exhaust manifolds; Valve mechanisms; Propeller reduction gearboxes. 16.4 Engine Fuel Systems 16.4.1 Carburetors 1 2 Types, construction and principles of operation; Icing and heating. 16.4.2 Fuel injection systems 1 2 Types, construction and principles of operation. 16.4.3 Electronic engine control 1 2 Operation of engine control and fuel metering systems including electronic engine control (FADEC); Systems lay-out and components. 16.5 Starting and Ignition Systems 1 2 Starting systems, pre-heat systems; Magneto types, construction and principles of operation; Ignition harnesses, spark plugs; Low and high tension systems. 16.6 Induction, Exhaust and Cooling Systems 1 2 Construction and operation of: induction systems including alternate air systems; Exhaust systems, engine cooling systems — air and liquid. 16.7 Supercharging/Turbocharging 1 2 Principles and purpose of supercharging and its effects on engine parameters; Construction and operation of supercharging/turbocharging systems; System terminology; Control systems; System protection. 16.8 Lubricants and Fuels 1 2 Properties and specifications; Fuel additives; Safety precautions. 16.9 Lubrication Systems 1 2 System operation/lay-out and components. 16.10 Engine Indication Systems 1 2 Engine speed; Page 63 of 180 Issue II datedCAR-66 LEVEL MODULE 16. PISTON ENGINE A2 B1.2 A4 B1.4 Cylinder head temperature; Coolant temperature; Oil pressure and temperature; Exhaust Gas Temperature; Fuel pressure and flow; Manifold pressure. 16.11 Powerplant Installation 1 2 Configuration of firewalls, cowlings, acoustic panels, engine mounts, anti-vibration mounts, hoses, pipes, feeders, connectors, wiring looms, control cables and rods, lifting points and drains. 16.12 Engine Monitoring and Ground Operation 1 3 Procedures for starting and ground run-up; Interpretation of engine power output and parameters; Inspection of engine and components: criteria, tolerances, and data specified by engine manufacturer. 16.13 Engine Storage and Preservation - 2 Preservation and depreservation for the engine and accessories/ systems LEVEL MODULE 17. PROPELLER A1 B1.1 A2 B1.2 17.1 Fundamentals 1 2 Blade element theory; High/low blade angle, reverse angle, angle of attack, rotational speed; Propeller slip; Aerodynamic, centrifugal, and thrust forces; Torque; Relative airflow on blade angle of attack; Vibration and resonance. 17.2 Propeller Construction 1 2 Construction methods and materials used in wooden, composite and metal propellers; Blade station, blade face, blade shank, blade back and hub assembly; Fixed pitch, controllable pitch, constant speeding propeller; Propeller/spinner installation. 17.3 Propeller Pitch Control 1 2 Speed control and pitch change methods, mechanical and electrical/electronic; Feathering and reverse pitch; Overspeed protection. Page 64 of 180 Issue II datedCAR-66 17.4 Propeller Synchronising - 2 Synchronising and synchrophasing equipment. 17.5 Propeller Ice Protection 1 2 Fluid and electrical de-icing equipment. 17.6 Propeller Maintenance 1 3 Static and dynamic balancing; Blade tracking; Assessment of blade damage, erosion, corrosion, impact damage, delamination; Propeller treatment/repair schemes; Propeller engine running. 17.7 Propeller Storage and Preservation 1 2 Propeller preservation and depreservation Page 65 of 180 Issue II datedCAR-66 Appendix II –Basic Examination Standard 1. General 1.1 All basic examinations must be carried out using the multiple choice question. 1.2 Each multiple choice questions must have more than two alternative answers of which only one must be the correct answer and the candidate must be al- lowed a time per module which is based upon a nominal average of 75 seconds per question. 1.3 The pass mark for CAR-66 module and sub-module multiple choice part of the examination is 75%. 1.4 Penalty marking systems is not used to determine whether a candidate has passed. 1.5 A failed module may not be retaken for at least 90 days following the date of the failed module examination. 1.6 The time periods required by point 66.A.25 apply to each individual module examination, with the exception of those module examinations which were passed as part of another category licence, where the licence has already been issued 1.7 The maximum number of consecutive attempts for each module is three. Fur- ther sets of three attempts are allowed with a 1 year waiting period between sets. 1.8 The applicant shall confirm in writing to the DGCA for an examination, the number and dates of attempts during the last year where these attempts took place. The CEO is responsible for checking the number of attempts within the applicable timeframes Page 66 of 180 Issue II datedCAR-66 2. Question Numbers and Examination Duration for the CAR-66 Appendix I Modules Module Multiple Time allowed Category choice Ques- (Minutes) No. Subject tions 1 Mathematics All Categories Not Applicable 2 Physics All Categories Not Applicable A 20 25 3 Electrical Fundamentals B1 52 65 B2 52 65 A Not Applicable 4 Electronic Fundamentals B1 20 25 B2 40 50 A 16 20 B1.1, B1.3 40 50 Digital Techniques/Electronic 5 Instrument Systems B1.2,B1.4 20 25 B2 72 90 A 52 65 6 Materials and Hardware B1 72 90 B2 60 75 A 72 90 7 Maintenance Practices B1 80 100 B2 60 75 A 20 25 8 Basic Aerodynamics B1 20 25 B2 20 25 A 20 25 9 Human factors B1 20 25 B2 20 25 Page 67 of 180 Issue II datedCAR-66 Module Multiple Time allowed Category choice Ques- (Minutes) No. Subject tions A 32 40 10 Aviation Legislation B1 40 50 B2 40 50 A1 108 135 Turbine Aeroplane Aerody- 11A namics, Structures and Sys- B1.1 140 175 tems B2 0 0 A2 72 90 Piston Aeroplane Aerodynam- 11B B1.2 100 125 ics, Structures and Systems B2 0 0 A3 / A4 100 125 Helicopter Aerodynamics, 12 B1.3 / B1.4 128 160 Structures and Systems B2 0 0 A 0 0 13 Aircraft Aerodynamics, Struc- B1 0 0 tures and Systems B2 180 225 A 0 0 14 Propulsion B1 0 0 B2 24 30 A 60 75 15 Gas Turbine Engine B1 92 115 B2 0 0 A 52 65 16 Piston Engine B1 72 90 B2 0 0 A 20 25 17 Propeller B1 32 40 B2 0 0 Page 68 of 180 Issue II datedCAR-66 3. ISSUANCE OF CERTIFICATE Applicants who have passed all basic knowledge examination modules in respect of a particular category/ sub-category of AME licence may apply to CEO, DGCA on Form CA 19-11 for the issuance of Basic Knowledge Examination Certificate. Page 69 of 180 Issue II datedCAR-66 Appendix III - Type training and Examination Standard On the job training 1. General Aircraft type training shall consist of theoretical training and examination, and, except for the category C ratings, practical training and assessment. (a) Theoretical training and examination shall comply with the following requirements: (i) Shall be conducted by a maintenance training organisation appropriately approved in accordance with CAR-147 or, when conducted by other organisations, as directly ap- proved by the DGCA. (ii) Shall comply, except as permitted by the differences training described in point (c), with: the relevant elements defined in the mandatory part of the operational suitability data established in accordance with CAR 66 or the standard described in point 3.1 of this Appendix, and the type training examination standard described in point 4.1 of this Appendix. (iii) Reserved (iv)Shall have been started and completed within the 3 years preceding the application for a type rating endorsement. (b) Practical training and assessment shall comply with the following requirements: (i) Shall be conducted by a maintenance training organisation appropriately approved in accordance with CAR- 147 or, when conducted by other organisations, as directly ap- proved by the DGCA. (ii) Shall comply, except as permitted by the differences training described in point (c), with: the relevant elements defined in the mandatory part of the operational suitability data established or, the standard described in point 3.2 of this Appendix, and the type training assessment standard described in point 4.2 of this Appendix. (iii) Shall include a representative cross section of maintenance activities relevant to the aircraft type. (iv) Shall include demonstrations using equipment, components, simulators, other training devices or aircraft. (v)Shall have been started and completed within the 3 years preceding the application for a type rating endorsement. (d) Differences training Page 70 of 180 Issue II datedCAR-66 (i)Differences training is the training required in order to cover the differences be- tween two different aircraft type ratings of the same manufacturer as determined by the DGCA. (ii) Differences training has to be defined on a case-to-case basis taking into account the requirements contained in this Appendix III in respect of both theoretical and practical elements of type (iii) A type rating shall only be endorsed on a licence after differences training when the applicant also complies with one of the following conditions: — having already endorsed on the licence the aircraft type rating from which the dif- ferences are being identified, or — having completed the type training requirements for the aircraft from which the dif- ferences are being identified. 2. Aircraft Type training levels The three levels listed below define the objectives that a particular level of training is intended to achieve. Level 1 A brief overview of the airframe, systems and powerplants as outlined in the Systems Description Section of the Aircraft Maintenance Manual / Instructions for Continued Airworthiness. Course objectives: Upon completion of the course, the student will be able to: (a) provide a simple description of the whole subject, using common words and exam- ples, using typical terms and identify safety precautions related to the airframe, its sys- tems and powerplant; (b) identify aircraft manuals, maintenance practices important to the airframe, its sys- tems and powerplant; (c) define the general layout of the aircraft's major systems; (d) define the general layout and characteristics of the powerplant; (e) identify special tooling and test equipment used with the aircraft Level 2 Basic system overview of controls, indicators, principal components including their lo- cation and purpose, servicing and minor troubleshooting. General knowledge of the the- oretical and practical aspects of the subject Course objectives: In addition to the information contained in the Level 1, training, at Page 71 of 180 Issue II datedCAR-66 the completion of this Level 2 , training the student will be able to: (a) understand the theoretical fundamentals; apply knowledge in a practical manner us- ing detailed procedures; (b) recall the safety precautions to be observed when working on or near the aircraft, powerplant and systems; (c) describe systems and aircraft handling particularly access, power availability and sources; (d) identify the locations of the principal components; (e) explain the normal functioning of each major system, including terminology and no- menclature; (f) perform the procedures for servicing associated with the aircraft for the following systems: Fuel, Power Plants, Hydraulics, Landing Gear, Water/Waste, and Oxygen; (g) demonstrate proficiency in use of crew reports and on-board reporting systems (mi- nor troubleshooting) and determine aircraft airworthiness per the MEL/CDL; (h) demonstrate the use, interpretation and application of appropriate documentation including instructions for continued airworthiness, maintenance manual, illustrated parts catalogue, etc. Level 3 Detailed description, operation, component location, removal/installation and bite and troubleshooting procedures to maintenance manual level. Course objectives: In addition to the information contained in Level 1 and Level 2 training, at the completion of Level III , the student will be able to: (a) demonstrate a theoretical knowledge of aircraft systems and structures and interrela- tionships with other systems, provide a detailed description of the subject using theo- retical fundamentals and specific examples and to interpret results from various sources and measurements and apply corrective action where appropriate; (b) Perform system, powerplant , component and functional checks as specified in the maintenance manual. (c) demonstrate the use, interpret and apply appropriate documentation including struc- tural repair manual, troubleshooting manual, etc.; (d) Correlate information for the purpose of making decisions in respect of fault diagnosis and rectification to maintenance manual level. (e) Describe procedures for replacement of components unique to aircraft type 3. Aircraft Type training standard Page 72 of 180 Issue II datedCAR-66 Although aircraft type training includes both theoretical and practical elements, courses can be approved for the theoretical element, the practical element or for a combination of both. 1.1. Theoretical element (a) Objective On completion of a theoretical training course the student shall be able to demonstrate, to the levels identified in the Appendix III syllabus, the detailed theoretical knowledge of the aircraft's applicable systems, structure, operations, maintenance, repair, and trouble- shooting according to approved maintenance data. The student shall be able to demon- strate the use of manuals and approved procedures, including the knowledge of relevant inspections and limitations. (b) Level of training: Training levels are those levels defined in point 2 above. After the first type course for category C certifying staff all subsequent courses need only be to level 1. During a level 3 theoretical training, level 1 and 2 training material may be used to teach the full scope of the chapter if required. However, during the training the majority of the course material and training time shall be at the higher level ( c ) Duration: The theoretical training minimum tuition hours are contained in the following table: Category Hours Aeroplanes with a maximum take-off mass above 30 000 kg: B1.1 150 B1.2 120 B2 100 C 30 Aeroplanes with a maximum take-off mass equal or less than 30 000 kg and above 5 700 kg: B1.1 120 B1.2 100 B2 100 C 25 Aeroplanes with a maximum take-off mass of 5 700 kg and below( B1.1 80 Page 73 of 180 Issue II datedCAR-66 B1.2 60 B2 60 C 15 Helicopters( 2) B1.1 120 B1.2 100 B2 100 C 25 (1) For non-pressurised piston engine aeroplanes below 2 000 kg MTOM the min- imum duration can be reduced by 50 %. (2) For helicopters in group 2 (as defined in point 66.A.42) the minimum duration can be reduced by 30 %. For the purpose of the table above, a tuition hour means 60 minutes of teaching and ex- clude any breaks, examination, revision, preparation and aircraft visit. These hours apply only to theoretical courses for complete aircraft/engine combinations according to the type rating as defined by the DGCA. (d) Justification of course duration: Training courses carried out in a maintenance training organisation approved in accord- ance with CAR-147 and courses directly approved by the DGCA shall justify their hour du- ration and the coverage of the full syllabus by a training needs analysis based on: — the design of the aircraft type, its maintenance needs and the types of operation, — detailed analysis of applicable chapters — see contents table in point 3.1(e) below, — detailed competency analysis showing that the objectives as stated in point 3.1(a) above are fully met. Where the training needs analysis shows that more hours are needed, course lengths shall be longer than the minimum specified in the table. Similarly, tuition hours of differences courses or other training course combinations (such as combined B1/B2 courses), and in cases of theoretical type training courses below the figures given in point 3.1(c) above, these shall be justified to the DGCA by the training needs analysis as described above. In addition, the course must describe and justify the following: — The minimum attendance required to the trainee, in order to meet the objectives of the course. — The maximum number of hours of training per day, taking into account pedagogical and human factors principles. If the minimum attendance required is not met, the certificate of recognition shall not be issued. Additional training may be provided by the training organisation in order to meet Page 74 of 180 Issue II datedCAR-66 the minimum attendance time. ( e ) Content: As a minimum, the elements in the Syllabus below that are specific to the aircraft type shall be covered. Additional elements introduced due to type variations, technological changes, etc. shall also be included. The training syllabus shall be focused on mechanical and electrical aspects for B1 personnel, and electrical and avionic aspects for B2. Aeroplanes Aeroplane Helicopter Helicopter Avi- Turbine Piston turbine Piston onics Level Chapters B1 C B1 C B1 C B1 C B2 Introduction module: 05 Time limits/maintenance 1 1 1 1 1 1 1 1 1 checks 06 Dimensions/Areas (MTOM, 1 1 1 1 1 1 1 1 1 etc.) 07 Lifting and Shoring 1 1 1 1 1 1 1 1 1 08 Levelling and weighing 1 1 1 1 1 1 1 1 1 09 Towing and taxiing 1 1 1 1 1 1 1 1 1 10 Parking/mooring, Storing and 1 1 1 1 1 1 1 1 1 Return to Service 11 Placards and Markings 1 1 1 1 1 1 1 1 1 12 Servicing 1 1 1 1 1 1 1 1 1 20 Standard practices — only type 1 1 1 1 1 1 1 1 1 particular Helicopters 18. Vibration and Noise Anal- – -- – – 3 1 3 1 – ysis( Blade tracking ) 60 Standard Practices Rotor - - - - 3 1 3 1 1 62 Rotors – – – – 3 1 3 1 1 62A Rotors — Monitoring and _ _ _ _ 3 1 3 1 3 indicating 63 Rotor Drives -- -- -- -- 3 1 3 1 1 63A Rotor Drives — Monitoring -- -- -- -- 3 1 3 1 3 and indicating 64 Tail Rotor – – – – 3 1 3 1 1 64A Tail rotor — Monitoring and -- -- -- -- 3 1 2 1 3 indicating 65 Tail Rotor Drive -- – – – 3 1 3 1 1 65A Tail Rotor Drive — Mon- -- -- -- -- 3 1 3 1 3 itoring and indicating Page 75 of 180 Issue II datedCAR-66 Aeroplanes Aeroplane Helicopter Helicopter Avi- Turbine Piston turbine Piston onics Level Chapters B1 C B1 C B1 C B1 C B2 66 Folding Blades/Pylon – – – – 3 1 3 1 – 67 Rotors Flight Control -- -- -- -- 3 1 3 1 -- 53 Airframe Structure (Heli- -- -- -- -- 3 1 3 1 -- copter) 25 Emergency Flotation -- -- -- -- 3 1 3 1 1 Equipment Airframe Structure 51 Standard practices and structures (damage classifica- 3 1 3 1 – – – – 1 tion, assessment and repair) 53 Fuselage 3 1 3 1 – – – – 1 54 Nacelles/Pylons 3 1 3 1 – – – – 1 55 Stabilizers 3 1 3 1 – – – – 1 56 Windows 3 1 3 1 – – – – 1 57 Wings 3 1 3 1 – – – – 1 27A Flight Control Surfaces ( 3 1 3 1 – – – – 1 All ) 52 Doors 3 1 3 1 – – – – 1 Zonal & Station Identification 1 1 1 1 1 1 1 1 1 Systems Airframe Systems 21 Air Conditioning 3 1 3 1 3 1 3 1 3 21A Air Supply 3 1 3 1 3 1 3 1 2 21B Pressurization 3 1 3 1 3 1 3 1 3 21C Safety & Warning Devic- 3 1 3 1 3 1 3 1 3 es 22 Autoflights 2 1 2 1 2 1 2 1 3 23 C0mmunication 2 1 2 1 2 1 2 1 3 24 Electrical Power 3 1 3 1 3 1 3 1 3 25 Equipment & Furnishings 3 1 3 1 3 1 3 1 1 25A Electronic Emergency Equip. & Cabin Entertain- 1 1 1 1 1 1 1 1 3 ment Equipment 26 Fire Protection 3 1 3 1 3 1 3 1 3 27 Flight Controls 3 1 3 1 3 1 3 1 2 27A Sys. Operation: Electri- 3 1 – – – – – – 3 cal/Fly-by-Wire Page 76 of 180 Issue II datedCAR-66 Aeroplanes Aeroplane Helicopter Helicopter Avi- Turbine Piston turbine Piston onics Level Chapters B1 C B1 C B1 C B1 C B2 28 Fuel Systems 3 1 3 1 3 1 3 1 2 28A Fuel Systems — Moni- 3 1 3 1 3 1 3 1 3 toring and indication 29 Hydraulic Power 3 1 3 1 3 1 3 1 2 29A Hydraulic Power — 3 1 3 1 3 1 3 1 3 Monitoring and indicating 30 Ice & Rain Protection 3 1 3 1 3 1 3 1 3 31 Indicating/Recording Sys- 3 1 3 1 3 1 3 1 3 tems 31A Instrument Systems 3 1 3 1 3 1 3 1 3 32 Landing Gear 3 1 3 1 3 1 3 1 2 32A Landing Gear — Moni- 3 1 3 1 3 1 3 1 3 toring and indicating 33 Lights 3 1 3 1 3 1 3 1 3 34 Navigation 2 1 2 1 2 1 2 1 3 35 Oxygen 3 1 3 1 – – – – 2 36 Pneumatic 3 1 3 1 3 1 3 1 2 36A Pneumatic — Monitor- 3 1 3 1 3 1 3 1 3 ing and indicating 37 Vacuum 3 1 3 1 3 1 3 1 2 38 Water/Waste 3 1 3 1 -- -- -- -- 2 41 Water Ballast 3 1 3 1 -- -- -- -- 1 42 Integrated modular avion- 2 1 2 1 2 1 2 1 3 ics 44 Cabin Systems 2 1 2 1 2 1 2 1 3 45 On-board Maintenance 3 1 3 1 3 1 – – 3 Systems 46 Information Systems 2 1 2 1 2 1 2 1 3 50 Cargo and Accessory 3 1 3 1 3 1 3 1 1 Compartments Turbine Engines: 70 Standard Practices — En- 3 1 – – 3 1 – – 1 gines, 70A constructional arrange- ment and operation (Installa- tion Inlet, Compressors, 3 1 -- -- 3 1 -- -- 1 Combustion Section, Turbine Section, Bearings and Seals, Lubrication Systems). 70B Engine Performance 3 1 – – 3 1 – – 1 71 Powerplant 3 1 – – 3 1 – – 1 Page 77 of 180 Issue II datedCAR-66 Aeroplanes Aeroplane Helicopter Helicopter Avi- Turbine Piston turbine Piston onics Level Chapters B1 C B1 C B1 C B1 C B2 72 Engine Turbine/Turbo Prop/Ducted Fan/Unducted 3 1 -- -- 3 1 -- -- 1 fan 73 Engine Fuel and Control 3 1 – – 3 1 – – 1 75 Air 3 1 – – 3 1 – – 1 76 Engine controls 3 1 – – 3 1 – – 1 78 Exhaust 3 1 – – 3 1 – – 1 79 Oil 3 1 – – 3 1 – – 1 80 Starting 3 1 – – 3 1 – – 1 82 water injection 3 1 – – 3 1 – – 1 83 Accessory Gear Boxes 3 1 – – 3 1 – – 1 84 Propulsion Augmentation 3 1 – – 3 1 – – 1 73A FADEC 2 1 – – 2 1 – – 3 74 Ignition 3 1 – – 3 1 – – 3 77 Engine Indicating Systems 3 1 – – 3 1 – – 3 49 Auxiliary Power Units 3 1 – – -- -- – – 2 (APUs) Piston Engines: 70 Standard Practices — En- -- -- 3 1 – – 3 1 1 gines 70A Constructional arrange- ment and operation (Installa- tion, Carburettors, Fuel injec- tion systems, Induction, Ex- – – 3 1 -- -- 3 1 1 haust and Cooling Systems, Supercharging/ Turbocharg- ing, Lubrication Systems). 71 Powerplant – – 3 1 – – 3 1 1 73 Engine Fuel and Control – – 3 1 – – 3 1 1 76 Engine Control – – 3 1 – – 3 1 1 79 Oil – – 3 1 – – 3 1 1 80 Starting – – 3 1 – – 3 1 1 81 Turbine 3 1 – – 3 1 – – 1 82 Water Injections – – 3 1 – – 3 1 1 83 Accessory Gear Boxes – – 3 1 – – 3 1 1 84 Propulsion Augmentation – – 3 1 – – 3 1 1 Page 78 of 180 Issue II datedCAR-66 Aeroplanes Aeroplane Helicopter Helicopter Avi- Turbine Piston turbine Piston onics Level Chapters B1 C B1 C B1 C B1 C B2 73A FADEC – – 3 1 – – 3 1 1 74 Ignition – – 3 1 – – 3 1 1 77 Engine Indication Systems – – 3 1 – – 3 1 1 Propellers: 60A Standard Practices — 3 1 3 1 – – – – 1 Propeller 61 Propellers/Propulsion 3 1 3 1 – – – – – 61APropeller Construction 61B Propeller Pitch Control 3 1 3 1 – – – – – 61C Propeller Synchronizing 3 1 3 1 – – – – – 61D Propeller Electronic con- 2 1 2 1 – – – – 3 trol 61E Propeller Ice Protection 3 1 3 1 – – – – – 61 F Propeller Maintenance 3 1 3 1 – – – – – (f) Multimedia Based Training (MBT) methods may be used to satisfy the theoretical train- ing element either in the classroom or in a virtual controlled environment subject to the acceptance of the DGCA approving the training course. 3. Practical element a) Objective: The objective of practical training is to gain the required competence in performing safe maintenance, inspections and routine work according to the maintenance manual and other relevant instructions and tasks as appropriate for the type of aircraft, for example troubleshooting, repairs, adjustments, replacements, rigging and functional checks. It in- cludes the awareness of the use of all technical literature and documentation for the air- craft, the use of specialist/special tooling and test equipment for performing removal and replacement of components and modules unique to type, including any on-wing mainte- nance activity. b) Content: At least 50 % of the crossed items in the table below, which are relevant to the particular aircraft type, shall be completed as part of the practical training. Tasks crossed represent subjects that are important for practical training purposes to en- sure that the operation, function, installation and safety significance of key maintenance Page 79 of 180 Issue II datedCAR-66 tasks is adequately addressed; particularly where these cannot be fully explained by theo- retical training alone. Although the list details the minimum practical training subjects, other items may be added where applicable to the particular aircraft type. Tasks to be completed shall be representative of the aircraft and systems both in complex- ity and in the technical input required to complete that task. While relatively simple tasks may be included, other more complex tasks shall also be incorporated and undertaken as appropriate to the aircraft type. B1 B2 B1/B2 Chapters SGH SGH M T LOC FOT R/I MEL TS FOT R/I EL S Introduction module: X/X -- X -- -- -- -- X -- -- - 05 Time limits/maintenance checks X/X -- -- -- -- -- -- -- -- -- - 06 Dimensions/Areas (MTOM, etc.) X/X -- -- -- -- -- -- -- -- -- - 07 Lifting and Shoring X/X -- X -- -- -- -- X -- -- - 08 Levelling and weighing X/X -- X -- -- -- -- X -- -- - 09 Towing and Taxing 10 parking/Mooring storing and return X/X -- X -- -- -- -- X -- -- - to service X/X -- -- -- -- -- -- -- -- -- - 11 Playcard and marking X/X -- X -- -- -- -- X -- -- - 12 servicing 20 standard practices –only type par- X/X -- X -- -- -- -- X -- -- - ticular Helicopters: 18Vibration and Noise Analysis (Blade X/-- -- -- -- -- X -- -- -- -- - tracking) 60Standard Practices Rotor — only type X/X -- X -- -- -- -- X -- -- - specific X/-- -- X X -- X -- -- -- -- - 62Rotors X/X X X X X X -- -- X -- - 62ARotors — Monitoring and indicating X/-- X -- -- -- -- -- -- -- -- - 63Rotor Drives 63ARotor Drives — Monitoring and indi- X/X X -- X X X -- -- X -- X cating X/-- -- X -- -- X -- -- -- -- - 64Tail Rotor X -- X X X -- X -- -- X 64ATail rotor -Monitoring and indicating X/X X -- -- -- X -- -- -- -- - 65Tail Rotor Drive X/-- Page 80 of 180 Issue II datedCAR-66 B1 B2 B1/B2 Chapters SGH SGH M T LOC FOT R/I MEL TS FOT R/I EL S 65ATail Rotor Drive — Monitoring and X -- X X X -- -- X X X/X indicating X X -- -- X -- -- -- -- - 66Folding Blades/Pylon X/-- X X -- X X -- -- -- -- - 67Rotors Flight Control X/-- 53Airframe Structure (Helicopter) Note: covered under Airframe structures X X X X X X X 25Emergency Flotation Equipment X/X Airframe structures: 51Standard Practices and Structures (damage classification, assessment and repair X/-- -- -- -- -- X -- -- -- -- - 53Fuselage X/-- -- -- -- -- -- -- -- -- -- - 54Nacelles/Pylons X/-- -- -- -- -- -- -- -- -- -- - 55Stabilisers X/-- -- -- -- -- X -- -- -- -- - 56Windows X/-- -- -- -- -- -- -- -- -- -- - 57Wings X/-- -- -- -- -- X -- -- -- -- - 27AFlight Control Surfaces X X -- -- -- -- X -- -- - 52Doors X/X Airframe systems: X X -- X X X X -- -- 21Air Conditioning X/X X X -- -- -- -- X -- -- -- 21AAir Supply X/X - X -- -- X X X -- -- X X 21BPressurisation X/X -- X -- -- -- -- X -- -- - 21CSafety and warning Devices X/X X/X -- -- -- X -- X X X X X 22Autoflight X/X -- X -- X -- X X X X X 23Communications X/X X X X X X X X X X X 24Electrical Power X/X X X X -- -- X X X -- - 25Equipment and Furnishings 25AElectronic Equipment including X/X X X X -- -- X X X -- - emergency equipment Page 81 of 180 Issue II datedCAR-66 B1 B2 B1/B2 Chapters SGH SGH M T LOC FOT R/I MEL TS FOT R/I EL S X/X X X X X X X X X X X 26Fire Protection X/X X X X X X X -- -- -- - 27Flight Controls 27ASys. Operation: Electrical/Fly-by- X/X X X X X -- X -- X -- X Wire X/X X X X X X X X -- X - 28Fuel Systems 28AFuel Systems — Monitoring and X/X X -- -- -- -- X -- X X indicating X/X X X X X X X X -- X - 29Hydraulic Power 29AHydraulic Power — Monitoring and X/X X -- X X X X -- X X X indicating X/X X X -- X X X X -- X X 30Ice and Rain Protection X/X X X X X X X X X X X 31Indicating/Recording Systems X X/X X X X X X X X X X X 31AInstrument Systems X/X X X X X X X X X X - 32Landing Gear 32ALanding Gear — Monitoring and X/X X -- X X X X -- X X X indicating X/X X X -- X -- X X X X - 33Lights -- X -- X -- X X X X X 34Navigation X/X X X X -- -- X X -- -- - 35Oxygen X/-- X -- X X X X -- X X X 36Pneumatic X/-- 36APneumatic — Monitoring and indi- X/X X X X X X X X X X X cating X -- X X X -- -- -- -- - 37Vacuum X/-- X X -- -- -- X X -- -- - 38Water/Waste X/-- 41Water Ballast X/-- -- -- -- -- -- -- -- -- -- - X/X -- -- -- -- -- X X X X X 42Integrated modular avionics X/X -- -- -- -- -- X X X X X 44Cabin Systems 45On-Board Maintenance System (or X/X X X X X X X X X X X covered in 31) X/X -- -- -- -- -- X -- X X X 46Information Systems Page 82 of 180 Issue II datedCAR-66 B1 B2 B1/B2 Chapters SGH SGH M T LOC FOT R/I MEL TS FOT R/I EL S -- X -- -- -- -- -- -- 50Cargo and Accessory Compartments X/X Turbine/Piston Engine Module: 70Standard Practices — Engines — only -- X -- -- -- -- X -- -- - --- type particular 70AConstructional arrangement and X/X -- -- -- -- -- -- -- -- - - operation (Installation Inlet, Compres- sors, Combustion Section, Turbine Sec- tion, Bearings and Seals, Lubrication Systems) Turbine engines: -- -- -- -- -- X -- -- -- -- - 70BEngine Performance X/-- X X -- -- -- -- X -- -- - 71Power Plant 72Engine Turbine/Turbo Prop/Ducted X/-- -- -- -- -- -- -- -- -- -- - Fan/ Unducted fan X/X X -- -- -- -- -- -- -- -- - 73Engine Fuel and Control X/X X -- X X X X -- X X X 73AFADEC Systems X/X X -- -- -- -- X -- -- -- - 74Ignition X/-- -- -- X -- X -- -- -- -- - 75Air X/-- X -- -- -- X -- -- -- -- - 76Engine Controls X/X X -- -- X X X -- -- X X 77Engine Indicating X/-- X -- -- X -- -- -- -- -- - 78Exhaust X/-- -- X X -- -- -- -- -- -- - 79Oil X/-- X -- -- X X -- -- -- -- - 80Starting X/-- X -- -- -- -- -- -- -- -- - 82Water Injection X/-- -- X -- -- -- -- -- -- -- - 83Accessory Gearboxes X/-- X -- -- -- -- -- -- -- -- - 84Propulsion Augmentation Auxiliary Power Units (APUs): X/-- X X -- -- X -- -- -- -- - 49Auxiliary Power Units (APUs) Piston Engines: 70Standard Practices — Engines — only -- X -- -- -- -- X -- -- - -- type particular 70AConstructional arrangement and X/X -- -- -- -- -- -- -- -- - - operation (Installation Inlet, Compres- Page 83 of 180 Issue II datedCAR-66 B1 B2 B1/B2 Chapters SGH SGH M T LOC FOT R/I MEL TS FOT R/I EL S sors, Combustion Section, Turbine Sec- tion, Bearings and Seals, Lubrication Systems) -- -- -- -- -- X -- -- -- -- - 70BEngine Performance X/-- X X -- -- -- -- X -- -- - 71Power Plant X/X -- -- -- -- -- -- -- -- -- - 73Engine Fuel and Control X/X X -- X X X X X X X X 73AFADEC Systems X/X X -- -- -- -- X -- -- -- - 74Ignition X/-- X -- -- -- X -- -- -- -- - 76Engine Controls X/X X -- -- X X X -- -- X X 77Engine Indicating X/-- X -- -- X X -- -- -- -- - 78Exhaust X/-- -- X X -- -- -- -- -- -- - 79Oil X/-- X -- -- X X -- -- -- -- - 80Starting X/-- X X X -- X -- -- -- -- - 81Turbines X/-- X -- -- -- -- -- -- -- -- - 82Water Injection X/-- -- X -- -- -- -- -- -- -- - 83Accessory Gearboxes X/-- X -- -- -- -- -- -- -- -- - 84Propulsion Augmentation Propellers: -- -- X -- -- -- X -- -- - 60AStandard Practices — Propeller -- X/X X X -- X X -- -- -- -- - 61Propellers/Propulsion X/-- -- X -- -- -- -- -- -- -- - 61APropeller Construction X/-- X -- X X X -- -- -- -- - 61BPropeller Pitch Control X/-- X -- -- -- X -- -- -- X - 61CPropeller Synchronising X/X X X X X X X X X X X 61DPropeller Electronic control X/-- X X X X X -- -- -- -- - 61EPropeller Ice Protection X/X X X X X X X X X X X 61FPropeller Maintenance Page 84 of 180 Issue II datedCAR-66 4. Type training examination and assessment standard 4.1. Theoretical element examination standard After the theoretical portion of the aircraft type training has been completed, a written examination shall be performed, which shall comply with the following: (a) Format of the examination is of the multi-choice type. Each multi-choice question shall have 3 alternative answers of which only one shall be the correct answer. The total time is based on the total number of questions and the time for answering is based upon a nomi- nal average of 90 seconds per question. (b) The incorrect alternatives shall seem equally plausible to anyone ignorant of the sub- ject. All the alternatives shall be clearly related to the question and of similar vocabulary, grammatical construction and length. (c) In numerical questions, the incorrect answers shall correspond to procedural errors such as the use of incorrect sense (+ versus -) or incorrect measurement units. They shall not be mere random numbers. (d) The level of examination for each chapter (1) shall be the one defined in point 2 ‘Air- craft type training levels’. However, the use of a limited number of questions at a lower level is acceptable. (e) The examination shall be of the closed book type. No reference material is permitted. An exception will be made for the case of examining a B1 or B2 candidate's ability to in- terpret technical documents. (f)The number of questions shall be at least 1 question per hour of instruction. The num- ber of questions for each chapter and level shall be proportionate to: — the effective training hours spent teaching at that chapter and level, — the learning objectives as given by the training needs analysis. DGCA will assess the number and the level of the questions when approving the course. (g)The minimum examination pass mark is 75 %. When the type training examination is split in several examinations, each examination shall be passed with at least a 75 % mark. In order to be possible to achieve exactly a 75 % pass mark, the number of questions in the examination shall be a multiple of 4. (h) Penalty marking (negative points for failed questions) is not to be used. Page 85 of 180 Issue II datedCAR-66 (i) End of module phase examinations cannot be used as part of the final examination un- less they contain the correct number and level of questions required. 4.2. Practical element assessment standard After the practical element of the aircraft type training has been completed, an assessment must be performed, which must comply with the following: (a) The assessment shall be performed by designated assessors appropriately qualified. (b) The assessment shall evaluate the knowledge and skills of the trainee. 5.Type examination standard Type examination shall be conducted by training organisations appropriately approved under CAR-147 or by the DGCA The examination shall be oral, written and or practical assessment based, or a combina- tion thereof and it shall comply with the following requirements: (a) Oral examination questions shall be open. (b) Written examination questions shall be essay type or multi-choice questions. (c) Practical assessment shall determine a person's competence to perform a task. (d) Examinations shall be on a sample of chapters (1) drawn from point 3 type train- ing/examination syllabus, at the indicated level. (e) The incorrect alternatives shall seem equally plausible to anyone ignorant of the sub- ject. All of the alternatives shall be clearly related to the question and of similar vocabu- lary, grammatical construction and length. (f) In numerical questions, the incorrect answers shall correspond to procedural errors such as corrections applied in the wrong sense or incorrect unit conversions: they shall not be mere random numbers. (g)The examination shall ensure that the following objectives are met: 1. Properly discuss with confidence the aircraft and its systems. 2. Ensure safe performance of maintenance, inspections and routine work according to the maintenance manual and other relevant instructions and tasks as appropriate for the type of aircraft, for example troubleshooting, repairs, adjustments, replacements, rigging and functional checks such as engine run, etc., if required. Page 86 of 180 Issue II datedCAR-66 3. Correctly use all technical literature and documentation for the aircraft. 4.Correctly use specialist/special tooling and test equipment, perform removal and re- placement of components and modules unique to type, including any on-wing mainte- nance activity (h) The following conditions apply to the examination: The maximum number of consecutive attempts is three. Further sets of three attempts are allowed with a 1 year waiting period between sets. A waiting period of 30 days is required after the first failed attempt within one set, and a waiting period of 60 days is required after the second failed attempt. The applicant shall confirm in writing to the DGCA the number and dates of attempts dur- ing the last year.. DGCA is responsible for checking the number of attempts within the ap- plicable timeframes. 2. The type examination shall be passed and the required practical experience shall be completed within the 3 years preceding the application for the rating endorsement on the aircraft maintenance licence. 3. Type examination shall be performed with at least one examiner present. The examin- er(s) shall not have been involved in the applicant's training. (i) A written and signed report shall be made by the examiner(s) to explain why the can- didate has passed or failed. 6. On the Job Training On the Job Training (OJT) shall be approved by the DGCA .. It shall be conducted at and under the control of a maintenance organisation appropriate- ly approved for the maintenance of the particular aircraft type and shall be assessed by designated assessors appropriately qualified. It shall have been started and completed within the 3 years preceding the application for a type rating endorsement. (a) Objective: The objective of OJT is to gain the required competence and experience in performing safe maintenance. Content: Page 87 of 180 Issue II datedCAR-66 OJT shall cover a cross section of tasks acceptable to the DGCA. The OJT tasks to be com- pleted shall be representative of the aircraft and systems both in complexity and in the technical input required to complete that task. While relatively simple tasks may be in- cluded, other more complex maintenance tasks shall also be incorporated and undertaken as appropriate to the aircraft type. Each task shall be signed off by the student and countersigned by a designated supervisor. The tasks listed shall refer to an actual job card/work sheet, etc. The final assessment of the completed OJT is mandatory and shall be performed by a des- ignated assessor appropriately qualified. The following data shall be addressed on the OJT worksheets/logbook: 1. Name of Trainee; 2. Date of Birth; 3. Approved Maintenance Organisation; 4. Location; 5. Name of supervisor(s) and assessor, (including licence number if applicable); 6. Date of task completion; 7. Description of task and job card/work order/tech log, etc.; 8. Aircraft type and aircraft registration; 9. Aircraft rating applied for. In order to facilitate the verification by the DGCA, demonstration of the OJT shall consist of i) detailed worksheets/logbook and (ii) a compliance report demonstrating how the OJT meets the requirement of this Part. Page 88 of 180 Issue II datedCAR-66 Appendix IV - Experience requirements for extending a CAR-66 Aircraft Maintenance Engineer’s Licence The table below shows the experience requirements for adding a new category or sub- category to an existing CAR-66 licence. The experience must be practical maintenance experience on an operating aircraft in the subcategory relevant to the application. The experience is to be signed by the post holder only and this procedure is to be re- flected in MOE The experience requirement will be reduced by 50 % if the applicant has completed an approved CAR-147 course relevant to the subcategory To: A1 A2 A3 A4 B1.1 B1.2 B1.3 B1.4 B2 From - - - - - - - - - A1 X 6 months 6 months 6 months 2 years 6 months 2 years 1 year 2 years A2 6 months X 6 months 6 months 2 years 6 months 2 years 1 year 2 years A3 6 months 6 months 6 months 2 years 1 year 2 years 6 months 2 years X A4 6 months 6 months 6 months 2 years 1 years 2 years 6 months 2 years X B1.1 NONE 6 months 6 months 6 months 6 months 6 months 6 months 1 year X B1.2 6 months NONE 6 months 6 months 2 years 2 years 6 months 2 years X B1.3 6 months 6 months NONE 6 months 6 months 6 months 6 months 1 year X B1.4 6 months 6 months 6 months NONE 2 years 6 months 2 years X 2 years B2 6 months 6 months 6 months 6 months 1 year 1 year 1 year 1 year X Page 89 of 180 Issue II datedCAR-66 Appendix V –Applications and Formats APPLICATION FOR INITIAL ISSUE OF CAR- 66 DGCA INDIA CA Form 19-01 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Fields marked with an asterisk * are mandatory and must be completed in all cases. Use Date Format – DD-MM-YYYY 1. PERSONAL DETAILS CEO Computer No. Affix recent pass- port size photo graph duly at- *Name in full tested on the front side *Date of birth * Nationality *Educational Quali- * Details of Fees Paid ……………………………………………............................. fication *Permanent address…………………………………………….................................…………………………………………………………… …………………………………………………………………………………………………………………………PIN Code................................ *Address for Communication (if different from above)………………………..................................................... ………………………………………………………………………………………………………….……………….PIN Code................................ Applicant Contact Phone Number ………………………….................. E-mail…….…………………………………………………. Name of the Current Employer……………………………………………………………………………………………………………………… Contact Phone Number of Employer ……………………….................. E-mail…….………………………………………………… 2. *APPLICATION I wish to apply for initial CAR-66 Aircraft Maintenance Engineer’s License as indicated and confirm that the information contained in this form was correct at the time of application (Specify the category A1,A2,A3,A4.. B1.1,B1.2,1.B1.3, B1.4, B2, C and required type ratings as per Appendix I to AMC of CAR – 66) Category/Sub-category of License applied for A B Mechanical Avionic 3. *DETAILS OF CREDIT SOUGHT I wish to claim the following credits (if applicable) Please enclose all relevant certificates: Experience credit by virtue of passing approved aircraft maintenance training/Engineering degree examina- tion/ defence experience..…………………………………………………………………………………………………………………… Examination credit due equivalent exam certificates...................................................................................... Page 90 of 180 Issue II datedCAR-66 4. *SUMMARY OF EXPERIENCE - ( Attach additional sheet indicating detail of practical experience obtained in cross representation section of maintenance task as per Appendix-II to AMC of CAR 66 ) Date Aircraft Engine(s) and Organisation Description of Work /or Equipment From To 5.* Details of basic knowledge certificate if any issued by CEO/DGCA Category Sub-category Modules Passed 5a.* Details of Type Rating courses certificates Aircraft Type / Series Engine Type course approval details 5b. *Details of skill test passed Name of DGCA office that conduct- Aircraft Type / Series Date of Exam ed the test *Relevant certificates/documents required to be submitted as enclosures in Section 7 6. PHYSICAL DISABILITY / DISORDER Known Physical disability or disorder 7.*DECLARATION I hereby confirm that: i) I apply for initial issue of CAR-66 Aircraft Maintenance Engineer’s Licence as indicated and con- firm that the information contained in this form was correct at the time of application. ii) I never had a CAR 66 AME Li- cence issued which was revoked or suspended by DGCA iii) I am not in possession of any other AME Licence issued by DGCA. iv) I did not apply earlier to the office of DGCA for issue of my AME Licence and the request was not turned down. PLACE SIGNATURE DATE NAME Page 91 of 180 Issue II datedCAR-66 Instruction and Checklist DGCA Re- CHECKLIST Enclosure Enclosure marks 8.DETAILS OF ENCLOSURES No. Page No. Sat/Unsat A. Certified true copy proof of Date of Birth certificate I B. Certified true copy of 10+2 with Physics, Chemistry, Mathematics or II equivalent C. Certified true copy of Passport or any photo identity card issued by the III Government D. Certified true copy of Course completion from approved aircraft mainte- nance training organization / Degree in Engineering certificate if applicable IV / Defence experience certificate and organisation approval certificate E. Certified true copies of basic knowledge examination result sheet / certifi- V cate if any issued by CEO Session No. Module No. Roll No. - - - passed 3. Electrical Fundamentals V (3) 4. Electronic Fundamental V (4) 5.Digital Techniques/ Electronic instrument Sys- V (5) tems 6. Materials & Hardwares V (6) 7. Maintenance Practices V (7) 8. Basic Aerodynamics V (8) 9. Human Factors V (9) 10. Aviation Legislation V (10) 11A. Turbine Engine Aeroplane Aerodynamics, V (11A) Structures and Systems 11B. Piston Engine Aeroplane Aerodynamics, V (11B) Structures and Systems 12. Helicopter Aerodynamics, Structures and V (12) Systems 13. Aircraft Aerodynamics, Structures and Sys- V (13) tems 14. Propulsion V (14) 15. Gas Turbine Engine V (14) 16. Piston Engine V (16) 17. Propeller V (17) F. Type course examination result sheet, course completion certificate and VI organisation approval certificate. G. Certified true copy of skill test result VII H. Certified true copies of Logbook / Work records on CA form 19-10 VIII I. Medical fitness certificate issued by MBBS doctor on CA form 19-06 IX J. Three copies of the recent photographs ( Stamp Size ) with the name of the applicant on the back side K. Fees as specified in Rule 62 Page 92 of 180 Issue II datedCAR-66 INSTRUCTION TO CA FORM 19-01 It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, issue, renewal or extension of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable, to administrative/legal action as per Aircraft Rule 1937. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. Please refer to current notification for details of fees required. All original documents if required to be submitted, will be returned through the self addressed cover affixed with necessary postal stamp (Speed post) provided by the applicant. Completed application with the checklist should be posted along with the required documentation to: The Di- rectorate General of Civil Aviation, Opposite Safdarjung Airport, New Delhi 110003 Notes: Having clear concise supporting data will enable DGCA to issue licences more effectively and with less risk of errors or rejections. DGCA will not contact you for clarification of details on applications and therefore it is most im- portant that you have the correct information before applying. In order that DGCA can process the licence application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentats enclosed. Please note failure to submit a correctly completed application form and the required documentation will lead to the rejection of the application and the fees submitted will be utilized towards processing the application Section 2: Indicate what type of licence you are applying for indicating Airframe or Engine as per Appendix- I to AMC of CAR-66 Section 3: Credit claimed for exemptions from passing module or experience. Section 4: This section is required for DGCA record purposes and should provide a brief summary of experience appli- cable to your application. You will still need to submit detailed maintenance experience records in addition to this in- formation, please refer to CAR-66.A.25 and CAR-66.A.30. The detail of experience should indicate practical experience obtained in cross representation section of Maintenance task as per Appendix- II to AMC of CAR-66. Section 5: Indicate the subject modules passed or basic knowledge certificate issued by CEO (DGCA) Section 5a: Indicate details of type rating courses completed for covering aeroplane/engine/helicopter. Section 5b: Indicate details of name of the DGCA office conducted the skill test. Section 6: State the details of existing known physical disability or disorder Section 7: By signing the declaration you are confirming that all of the information is correct and true. Section 8: Assign annexure number as indicated and continuous page numbers to the enclosures and indicate it under column 3 against each item Page 93 of 180 Issue II datedCAR-66 APPLICATION FOR EXTENSION OF CAR- 66 DGCA INDIA AIRCRAFT MAINTENANCE ENGINEER’S LICENCE CA Form 19-02 Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Fields marked with an asterisk * are mandatory and must be completed in all cases. Use Date Format – DD-MM-YYYY 1. PERSONAL DETAILS *Name in full Computer No. *AME LICENCE No. *Fees Paid Permanent address…………………………. …………………………………………………..…………………….................................…… …………………………………………………………………………………………………………………………PIN Code................................ Address for Communication (if different from above)………………………..................................................... ………………………………………………………………………………………………………….……………….PIN Code................................ Applicant Contact Phone Number ……………………….................. E-mail…….……………………………………………………… Name of the Current Employer……………………………………………………………………………………………………………………….. Contact Phone Number of Employer……………………….................. E-mail…….…………………………………………………. 2. *APPLICATION I wish to apply for extension of CAR-66 Aircraft Maintenance Engineer’s License as indicated and confirm that the information contained in this form was correct at the time of application ( Specify the category A1,A2,A3,A4.. B1.1,B1.2,1.B1.3, B1.4, B2, C and required type ratings as per Appendix- I to AMC of CAR – 66) Category/Sub-category of License applied for A B Mechanical Avionic 3. *DETAILS OF CREDIT SOUGHT I wish to claim the following credits (if applicable) Please enclose all relevant certificates: Experience credit by virtue of passing approved aircraft maintenance training/defence experi- ence..…………………………………………………………………………………………………………………………………………………. Examination credit due equivalent exam certificates............................................................................... 4. *SUMMARY OF EXPERIENCE - ( Attach additional sheet indicating detail of practical experience obtained in cross representation section of maintenance task as per Appendix-II to AMC of CAR 66 ) Date Aircraft Engine(s) and Organisation Description of Work /or Equipment From To Page 94 of 180 Issue II datedCAR-66 5.* Details of basic knowledge certificate if any issued by CEO/DGCA Category Sub-category Modules Passed 5a.* Details of Type Rating courses certificates Aircraft Type / Series Engine Type course approval details 5b. *Details of skill test passed Name of DGCA office that conduct- Aircraft Type / Series Date of Exam ed the test *Relevant certificates/documents required to be submitted as enclosures in Section 7 6. PHYSICAL DISABILITY / DISORDER Known Physical disability or disorder 7.*DECLARATION I hereby confirm that: i) I apply for extension of CAR-66 Aircraft Maintenance Engineer’s Licence as indicated and confirm that the information contained in this form was correct at the time of application. ii) I never had a CAR 66 AME Licence issued which was revoked or suspended by DGCA iii) I am not in possession of any other AME Licence issued by DGCA. iv) I did not apply earlier to the office of DGCA for extension of my AME Licence and the request was not turned down. PLACE SIGNATURE DATE NAME Page 95 of 180 Issue II datedCAR-66 INSTRUCTION AND CHECKLIST 8. CHECKLIST TO CA FORM 19-02 DGCA Re- Enclosure Enclosure marks No. Page No. DETAILS OF ENCLOSURES Sat/Unsat A. Original CAR-66 Aircraft Maintenance Engineer’s licence I B. Certified true copies of basic knowledge examination result sheet II / certificate issued by CEO C. Certified true copy of Passport or any photo identity card issued III by the Government Module No Session No. passed Roll No. IV(a) IV(b) IV(c) D. Type course examination result sheet, course completion certifi- V cate and organisation approval certificate E. Certified true copy of skill test and oral cum practical examination VI F. Certified true copies of Logbook / Work records on CA form 19-10 G. Fees INSRUCTION TO CA FORM 19-02 It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, issue, renewal or extension of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable to adminis- trative/legal actions as per Aircraft Rules 1937. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. Please refer to current notification for details of fees required. All original documents if required to be submitted, will be re- turned through the self addressed cover affixed with necessary postal stamp (Speed post) provided by the applicant. Completed application with the checklist should be posted along with the required documentation to the respective Regional / Sub-Regional Airworthiness Office Notes: Having clear concise supporting data will enable Regional / sub-regional offices of DGCA to extend the licences more ef- fectively and with less risk of errors or rejections. DGCA office will not contact you for clarification of details on applications and there- fore it is most important that you have the correct information before applying. In order that DGCA can process the licence application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation enclosed. Please note failure to submit a correctly completed application form and the required documentation will lead to the rejection of the application and the fees submitted will be utilized towards processing the application. Section 2: Indicate what type of licence you are applying for and indicate Airframe -Engine combination as per Appendix- I to AMC of CAR 66 Section 3: credit claimed for exemptions from passing module or experience. Section 4: This section is required for DGCA record purposes and should provide a brief summary of experience applicable to your ap- plication. You will still need to submit detailed maintenance experience records in addition to this information, please refer to CAR- 66.A.25 and CAR-66.A.30. The detail of experience should indicate practical experience obtained in cross representation section of Maintenance task as per Appendix- II to AMC of CAR 66. Section 5:Indicate the subject modules passed or basic knowledge certificate issued by CEO (DGCA) Section 5a: Indicate details of type rating courses completed covering aeroplane/engine/helicopter. Section 5b: Indicate details of Name of the DGCA office conducted the skill test. Section 6: State the details of existing known physical disability or disorder Section 7: By signing the declaration you are confirming that all the information is correct and true. Section 8: Assign annexure number as indicated and continuous page numbers to the enclosures and indicate it under column 3 against each item Page 96 of 180 Issue II datedCAR-66 APPLICATION FOR RENEWAL OF DGCA INDIA CAR- 66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE CA Form 19-03 Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Fields marked with an asterisk * are mandatory and must be completed in all cases. Use Date Format – DD-MM-YYYY 1. PERSONAL DETAILS AME Licence No. Expiry Date *Name in full Details of Fees *Permanent address (in case of any change) ……………………………………………………………………………………………………………………... ……………………………………………………………………………………………………………………………………………. PIN Code ……………………………… *Address for Communication …………………………………………………………………………………………………………….............................. …………………………………………………………………………………………………………………................ PIN Code …………………………… Applicant Contact Phone Number ………………………........................ E-mail………………..….……………………………………………..……. Name of the Current Employer ….…………………………………………………………………………………………….…………….……………….….. Contact Phone Number of Employer ……………………….................. E-mail…….……………………………..………………………..………………. 2. *APPLICATION I wish to apply for Renewal of CAR-66 Aircraft Maintenance License as indicated and confirm that the information con- tained in this form was correct at the time of application 3. *SUMMARY OF AERONAUTICAL EXPERIENCE PRECEEDING TWENTY FOUR MONTHS Date Organisation Aircraft Description of Work From To *Relevant certificates/documents required to be submitted as enclosures in Section 5 4. DETAILS OF REFRESHER COURSE ATTENDED 4.*DECLARATION I hereby confirm that: i) I apply for renewal of CAR-66 Aircraft Maintenance Engineer’s Licence as indicated and confirm that the information contained in this form was correct at the time of application. ii) I never had a CAR 66 AME Licence issued which was revoked or suspended by DGCA iii) I did not apply earlier to the any other office of DGCA for renewal of my AME Licence and the request was not turned down. PLACE SIGNATURE DATE NAME Page 97 of 180 Issue II datedCAR-66 INSTRUCTION AND CHECKLIST CHECKLIST TO CA FORM 19-03 DGCA Enclosure Enclosure Remarks No. Page No. DETAILS OF ENCLOSURES Sat/Unsat 1. Original CAR 66 Aircraft Maintenance Engineer’s licence I 2. Certified true copies of Logbook / Work records for the corresponding II period 3. Medical fitness certificate III 4. Copies of refresher training corresponding to the previous five years IV 4. Fee paid It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, is- sue, renewal or extension of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable to administrative/Legal action n as per Aircraft Rule 1937. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. Please refer to current notification for details of fees required. All original documents if required to be submitted, will be returned through the self addressed cover affixed with necessary postal stamp (Speed post) provided by the appli- cant. Completed application with the checklist should be posted along with the required documentation to the respec- tive Regional / Sub-Regional Airworthiness Office Notes: Having clear concise supporting data will enable DGCA office to renew the licenses more effectively and with less risk of errors or rejections. DGCA office will not contact you for clarification of details on applications and there- fore it is most important that you have the correct information before applying. In order that DGCA can process the licence application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation enclosed. Please note failure to submit a correctly completed application form and the required documentation will lead to the rejection of the application and the fees submitted will be utilized towards processing the application Section 1: Indicate personal details as required. Section 3: Indicate aircraft maintenance and certification work done during the period. Page 98 of 180 Issue II datedCAR-66 APPLICATION FOR CONVERSION/REMOVAL OF LIMITATIONS OF DGCA INDIA CAR- 66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE CA Form 19-04 Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Fields marked with an asterisk * are mandatory and must be completed in all cases. Use Date Format – DD-MM-YYYY *1. PERSONAL DETAILS AME Licence No. Expiry Date Name Nationality Date of birth Computer No. Permanent Address .........................................…………………………………………………………… …………………………………………………………………………………………………………………………PIN Code................................ Address for Communication (if different from above)………………………..................................................... ………………………………………………………………………………………………………….……………….PIN Code................................ Applicant Contact Phone Number ……………………..................E-mail…….………………………………………………………. Name of the Current Employer ……………………………………………………………………………………………………………….. Contact Phone Number of Employer………………………..................E-mail…….……………………………………………………. *2(a) AME LICENCE HELD 2(b) DETAILS OF CAR-66 AME LICENCE APPLIED FOR Category Type Rating Category A/c Type Rating Limitation Code Page 99 of 180 Issue II datedCAR-66 *2(a) AME LICENCE HELD 2(b) DETAILS OF CAR-66 AME LICENCE APPLIED FOR Category Type Rating Category A/c Type Rating Limitation Code *3. DETAILS OF LIMITATION CODE TO BE REVOKED License Held Limitation Code Examination Module Endorsed Completed Category Type Rating *4. SUMMARY OF AERONAUTICAL EXPERIENCE GAINED WITH RESPECT TO THE LIMITATION OF AME Licence Date Organisation Aircraft Description of Work From To 5.DECLARATION I hereby confirm that: i) I apply for Conversion/Removal of limitation as indicated and confirm that the infor- mation contained in this form was correct at the time of application. PLACE SIGNATURE DATE NAME Page 100 of 180 Issue II datedCAR-66 INSTRUCTION AND CHECKLIST DGCA Re- CHECKLIST TO CA FORM 19-04 Enclosure Enclosure marks DOCUMENTS ENCLOSED No. Page No. Sat/Unsat 1. Original Pre - CAR 66 AME licence. I 2. Three copies of stamp size photograph duly attested on its back II side. (for conversion) 3. Certified true copies of Knowledge Examination modules (where III applicable) result sheets/ certificates. 4. Certified true copies of documentary evidence of experience, skill IV test (where applicable). 5. Type course completion certificate, where applicable. V 6. Copy of skill test result relating to the limitation of the licence VI 7. Certified true copies of Logbook / Work records as applicable. VII Instruction to complete CA Form 19-04 It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, issue, renewal or extension of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable to administrative/legal actions as per Aircraft Rules 1937. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Li- cence. All original documents if required to be submitted, will be returned through the self addressed cover affixed with necessary postal stamp (Speed post) provided by the applicant. Completed application with the checklist should be posted along with the required documentation to: The Directorate General of Civil Aviation, Opposite Safdarjung Airport, New Delhi 110003 Notes: Having clear concise supporting data will enable DGCA to issue licences more effectively and with less risk of errors or rejections. DGCA will not contact you for clarification of details on applications and therefore it is most im- portant that you have the correct information before applying. In order that DGCA can process the licence application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation enclosed. Please note failure to submit a correctly completed application form and the required documentation will lead to the rejection of the application and the fees submitted will be utilized towards processing the application Section 2: Indicate category & type rating of licence held/and the category and typerating applied for with or without limitation. Section 3: This section should be used if applying for the removal of limitation(s) from type rating(s), and should detail aircraft types by airframe/engine combination. Please enter the limitation (s) in the appropriate column. Enter only one airframe/engine per line. Section 4: Provide details of experience gained corresponding to the limitation code & aircraft type. Page 101 of 180 Issue II datedCAR-66 APPLICATION FOR ISSUE OF DUPLICATE DGCA INDIA CAR- 66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE CA Form 19-05 Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Fields marked with an asterisk * are mandatory and must be completed in all cases. Use Date Format – DD-MM-YYYY 1. PERSONAL DETAILS *Name in full AME Licence No. *Permanent address ................................…………………………………………………………… …………………………………………………………………………………………………………………………PIN Code................................ *Address for Communication (if different from above)………………………..................................................... ………………………………………………………………………………………………………….……………….PIN Code................................ Applicant Contact Phone Number …………………..................E-mail…….…………………………………………………….. Name of the Current Employer ………………………………………………………………………………………………………….. Contact Phone Number of Employer ………………………..................E-mail…….………………………………………………… 2. *APPLICATION I wish to apply for issue of Duplicate CAR-66 Aircraft Maintenance License as indicated and the information contained in this form was correct at the time of application. 3. *Reason for issue of duplicate AME Licence( Mark √ as ap- LOST MUTILATED plicable) If the licence was lost provide a brief account of circumstances under which the licence was lost: 4.*DECLARATION I hereby confirm that: i) I apply for issue of duplicate CAR-66 Aircraft Maintenance Engineer’s Licence as indi- cated and confirm that the information contained in this form is correct at the time of application. ii) My CAR 66 AME Licence not suspended / cancelled by DGCA and no disciplinary case is pending against me iii) I did not apply earlier to the office of DGCA for issue of my duplicate AME Licence and the request was not turned down. PLACE SIGNATURE DATE NAME Page 102 of 180 Issue II datedCAR-66 DGCA Enclosure Tick 5.DETAILS OF DOCUMENTS, PHOTOGRAPH AND FEE ENCLOSURES No. Mark Remarks 1.Original Mutilated AME Licence or Affidavit duly notarized by Authorized I notary in case of loss of AME Licence 2. Copy of FIR lodged with the police station in case of loss of AME Licence II 3. Copy of AME Licence if available in case of loss III 4. Two copy of recent photograph IV 5. Details of fee paid as per Rule 62 V Please refer to current notification for details of fees required. All original documents submitted will be re- turned through the self addressed cover affixed with necessary postal stamp (for speed post). Completed application should be posted along with the required documentation to: Licensing & Training Standards, Directorate General of Civil Aviation, Opposite Safdarjung Airport, New Delhi 110003, Notes: Having clear concise supporting data will enable DGCA to issue licences more effectively and with less risk of errors or rejections. Licensing & Training Standards will not contact you for clarification of details on applications and therefore it is most important that you have the correct information before applying. Instruction on how to complete CAR-66 Licence issue of duplicate Application Form (CA Form 19-05). In order that DGCA can process your licence application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation submitted. Please note failure to submit a correctly completed application form and the required documenta- tion will lead to the rejection of your application and the fees submitted will be utilized towards processing the application. Section 2: Indicate what type of licence you are applying for. Section 3: Tick whether the AME Licence is lost or mutilated Section 4: By signing the declaration you are confirming that all of the information is correct and true. Page 103 of 180 Issue II datedCAR-66 MEDICAL CERTIFICATE DGCA INDIA (To be provided by a Registered Medical Practitioner holding at least MBBS) CA Form 19-06 Mr. / Ms _________________________ whose signature is appended below, has been medically examined for any known disability or disorder which may become an hindrance to perform the normal functions of an Aircraft Maintenance Engineer. He/She has …………………………………………………………………………………………………………………………………………..………… physical disabilities or disorder / no physical disabilities or disorder. He/She has been assessed medically fit / unfit to function as an Aircraft Maintenance Engineer. ( Strikeout whichever is not applicable) Signature of the Doctor………………………………. Registration No. Designation Signature of the Applicant with date Date MEDICAL CERTIFICATE FOR COLOUR VISION I, Dr. _______________________ hereby certify that I have examined Mr. /Ms ___________________ whose signature is appended below, and certify that his colour vision is Normal/Defective safe/Defective unsafe. The colour vision has been tested with, (1) Pseudo – Isochromatic plates (2) Approved Lantern test (3) Any other test applicable ( Strikeout whichever is not applicable) Signature of the Doctor………………………………. Registration No. Designation Signature of the Applicant with date Date Page 104 of 180 Issue II datedCAR-66 APPLICATION FOR ALLOTMENT OF COMPUTER NUMBER DGCA INDIA FOR APPEARING IN AME LICENCE EXAMINATIONS CA Form 19-07 Please complete the form in BLOCK CAPITALS using black or dark blue Paste recent passport ink after reading the attached guidance notes. Fields marked with an size photograph asterisk * are mandatory and must be completed in all cases. Use Paste recent passport size Date Format – DD-MM-YYYY (WITHOUT ATTESTA- photograph * FOR OFFICE USE - Computer Number Allotted TION) (attested partly cover- (Allotment of Computer Number does not indicate the ac- ing photograph & Page ceptance of the applicant’s candidature in Basic Knowledge of this application) Examination) E- ………………………………….... . 1.*PERSONAL DETAILS SIGNATURE FIRST NAME MIDDLE NAME SURNAME Fathers Name *Name in full *Date of * Nationality SEX (Male/ Birth Female) *Permanent address ……………………………………………………………………………………………………………………..……………. ……………………………………………………………………………………………………………..………PIN Code................................... *Address for Communication (if different from above address) ……………………………………………………………..…… ………………………………………………………………………………………………………………………PIN Code................................... *Applicant Contact Phone Number…….......……………............... E-mail…….……..……………….……………………………… Employer/ Training School Contact Phone Number …………........................ E-mail…….…………….……..……………… *Subject studied and Name of the Educa- passed in 10+2 or Year of Passing Details of the School tion Board equivalent Physics, Chemistry & Mathematics 2. * AIRCRAFT MAINTENANCE EXPERIENCE / DURATION OF STUDY IN AN APPROVED TRAINING ESTAB- LISHMENT Type of air- Duration Maintenance Organization/ craft/ engine/ Approved Institute Period in From To system months Page 105 of 180 Issue II datedCAR-66 3. *DECLARATION I hereby declare that the information provided in this form is correct in every respect to the best of my knowledge and belief and that nothing has been concealed or withheld by me. I understand that if any of my particulars/ entries are found false or incorrect before or after the examination, my candidature shall be rejected and further action can be taken against me by DGCA as deemed fit. Further, I declare that I have read and understood the INSTRUCTIONS. PLACE SIGNATURE DATE NAME It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, is- sue, renewal or variation of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable, on summary conviction, to a fine of one Lakh Rupees and/or imprisonment for a term not exceed- ing three months. Further, it renders the person permanently ineligible to have an Aircraft Maintenance Engineer’s Licence. *CERTIFICATE [To be certified by QM/ CI/ Chief Engg. Officer(in case of serving defence candidates)] It is certified that the particulars claimed by Mr. / Ms ___________________________ has been verified by me and found correct. DATE: SIGNATURE………………………………………………………………… (SEAL OF ORGANISATION) NAME …………………………………………………………………. PLACE: Designation………………………………………………………………… Enclosure Tick DGCA 4.*DETAILS OF DOCUMENTS, PHOTOGRAPH AND FEE ENCLOSURES No. Mark Remarks 1. Certified true copy proof of Date of Birth certificate I 2. Certified true copy of 10+2 with Physics, Chemistry, Mathematics or II equivalent 3. Certified true copy of Passport or any photo identity card issued by the III Government 4. Certified true copy of Course completion from AME institute/ Degree IV in Engineering certificate is applicable Completed application should be posted along with the required documentation to the Central Examina- tion Organisation, O/o the Directorate General of Civil Aviation, East block II, R K Puram, New Delhi 110066. Failure to submit a correctly completed application form and the required documentation will lead to the rejection of your application. Instruction to complete application for allotment of computer No. for appearing in CAR-66 basic knowledge exami- nation (CA Form 19-07). In order that CEO can process your licence application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documents submitted. Page 106 of 180 Issue II datedCAR-66 APPLICATION FOR APPEARING IN WRITTEN PAPER(S) OF DGCA INDIA CAR 66 BASIC KNOWLEDGE EXAMINATION CA Form 19-08 A Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Fields marked with an asterisk * are mandatory and must be completed in all cases. Use Date Format – DD-MM-YYYY 1.* FEE DEAILS: Amount (in Rs.) Demand Draft/ Banker’s Cheque No. Name of Bank Date of Issue 2.*PERSONAL DETAILS COMPUTER NO: EXAMINATION SESSION & CENTRE MONTH YEAR CENTRE E- NAME: FIRST NAME MIDDLE NAME SURNAME *CATEGORY/ SUB-CATEGORY OF EXAMINATION (Tick appropriate box(s) Category A B Aeroplane Turbine A1 B1.1 Aeroplane Piston A2 B1.2 Helicopter Turbine A3 B1.3 Helicopter Piston A4 B1.4 Avionic B2 3. *EXAMINATION PAPERS (Please tick box(es) against the module(s) you wish to take at this examination) Module (cid:252) Module (cid:252) 3. Electrical Fundamentals 11A. Turbine Engine Aeroplane Aerodynamics, Structures and Systems 4. Electronic Fundamental 11B. Piston Engine Aeroplane Aerodynamics, Structures and Systems 5.Digital Techniques/ Electronic instrument 12. Helicopter Aerodynamics, Structures and Systems Systems 13. Aircraft Aerodynamics, Structures and Systems .(Please tick (√)the appropriate box) Ex- Ex- Ex- Ex- Ex- Ex- cludin cludin cludin cludin cludin cludin 6. Materials & Hardwares g g 13.8 g 13.4 g g g 13.4&, 13.5,1 13.5,1 13.4,1 13.8 3.9 3.6,13. 3.5&1 8&13. 3.9 9 7. Maintenance Practices 14. Propulsion 8. Basic Aerodynamics 15. Gas Turbine Engine Page 107 of 180 Issue II datedCAR-66 9. Human Factors 16. Piston Engine 10. Aviation Legislation 17. Propeller 4. * DETAILS OF AERONAUTICAL ENGINEERING EXPERIENCE: Type of aircraft/ Organization/ Duration Approved Insti- Area or Work engine/ system From To Period in months tute 5.* DECLARATION (delete as appropriate) I hereby declare that the information provided in this form is correct in every respect to the best of my knowledge and be- lief and that nothing has been concealed or withheld by me. I understand that if any of my particulars/ entries are found false or incorrect before or after the examination, my candidature shall be rejected and further action can be taken against me by DGCA as deemed fit. Further, I declare that I have read and understood the INSTRUCTIONS. PLACE SIGNATURE DATE NAME It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, issue, re- newal or variation of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable, on summary conviction, to a fine of one Lakh Rupees and/or imprisonment for a term not exceeding three months. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. *CERTIFICATE [To be certified by QM/ CI/ Chief Engg. Officer(in case of serving defence candidates)] It is certified that the particulars claimed by Mr. / Ms ___________________________ has been verified by me and found correct. SIGNATURE NAME Designation DATE: (SEAL OF ORGANISATION) Instruction to complete application form for CAR-66 AME Licence Knowledge (written) examination (CA Form 19-08 A). In order that DGCA (CEO) can process your application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation submitted. Please note fail- ure to submit a correctly completed application form and the required documentation will lead to the rejection of your application and the fees submitted will be utilized towards processing the application. Page 108 of 180 Issue II datedCAR-66 APPLICATION FOR APPEARING IN DGCA INDIA CAR 66 TYPE EXAMINATION CA Form 19-08 B *To be Submitted to the respective DGCA RAO’s Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Fields marked with an asterisk * are mandatory and must be completed in all cases. Use Date Format – DD-MM-YYYY 1.* FEE DEAILS: Amount (in Rs.) Demand Draft/ Banker’s Cheque No. Name of Bank Date of Issue 2.*PERSONAL DETAILS COMPUTER NO: EXAMINATION SESSION & CENTRE MONTH YEAR CENTRE E- FIRST NAME MIDDLE NAME SURNAME *CATEGORY/ SUB-CATEGORY OF EXAMINATION (Please tick (√) the appropriate Category/Categories) Category A B Aeroplane Turbine A1 B1.1 Aeroplane Piston A2 B1.2 Helicopter Turbine A3 B1.3 Helicopter Piston A4 B1.4 Avionic B2 3. *DETAILS OF BASIC KNOWLEDGE EXAMINATION PAPERS PASSED PERTAINING TO THE CATEGORY (Please tick (√)against the module(s) , enclose attested true copies of result cards) Module Module 11A. Turbine Engine, Aeroplane Aerodynamics, Struc- 3. Electrical Fundamentals tures and Systems 11B. Piston Engine, Aeroplane Aerodynamics, Struc- 4. Electronic Fundamental tures and Systems 5.Digital Techniques/ Electronic 12. Helicopter Aerodynamics, Structures and Systems instrument Systems 13. Aircraft Aerodynamics, Structures and Systems (Please tick (√)the appropriate box(es)) Exclud- Exclud- Exclud- Exclud- Exclud- Exclud- ing ing ing ing ing ing 6. Materials & Hardwares 13.4 & 13.5 & 13.8 13.4 13.5, 13.4, 13.5 & 13.8 13.9 13.6, 13.8 & 13.9 13.9 7. Maintenance Practices 14. Propulsion 8. Basic Aerodynamics 15. Gas Turbine Engine 9. Human Factors 16. Piston Engine Page 109 of 180 Issue II datedCAR-66 10. Aviation Legislation 17. Propeller 4. *Type of Applicant (Please tick (√) the ap- AME TRG DEF AEG GEN propriate type) 5.*Type of Aircraft, Engine for Type Exam- ination (As per the Appendix I to AMC of CAR-66) 6. * DETAILS OF TOTAL AERONAUTICAL ENGINEERING EXPERIENCE: Type of air- Organization/ Duration craft/ engine/ Approved Insti- Area or Work From To Period in months system tute 7.*DETAILS OF TYPE RATED EXPERIENCE Type of Aircraft, Organisation/ Duration Periods Brief Details of Expe- Engines, Sys- Approved Insti- Area of Work in From To rience tems tute Months 8.* Name of the Approved Institute/Sponsoring Or- ganization/Employer 9.* DECLARATION (delete as appropriate) I hereby declare that the information provided in this form is correct in every respect to the best of my knowledge and belief and that nothing has been concealed or withheld by me. I understand that if any of my particulars/ entries are found false or incorrect before or after the examination, my candidature shall be rejected and further action can be taken against me by DGCA as deemed fit. Further, I declare that I have read and understood the INSTRUCTIONS. PLACE SIGNATURE DATE NAME It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, issue, re- newal or variation of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable to administrative/ Legal action as per Aircraft rule 1937. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. *CERTIFICATE [To be certified by QM/ CI/ Chief Engg. Officer(in case of serving defence candidates)] It is certified that the particulars claimed by Mr. / Ms ___________________________ has been verified by me and found correct. SIGNATURE NAME Designation DATE: (SEAL OF ORGANISATION) Page 110 of 180 Issue II datedCAR-66 FOR OFFICIAL USE ONLY CATEGORIES ACCEPTED ROLL NO ALLOTED A B REASONS FOR REJECTION, IF ANY: A1 B1.1 A2 B1.2 A3 B1.3 A4 B1.4 B2 NAME OF THE DGCA OFFICER SIGNATURE OF THE DGCA OFFICER Instruction to complete application form for CAR-66 AME Licence Type examination (CA Form 19-08 B). In order that DGCA (RAO) can process your application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation submitted. Please note failure to submit a correctly completed application form and the required documentation will lead to the rejection of your applica- tion and the fees submitted will be utilized towards processing the application. *AEG-Aeronautical Engineering Graduate & Graduates of other allied field of Engineering. Page 111 of 180 Issue II datedCAR-66 APPLICATION FOR APPEARING IN SKILL TEST OF DGCA INDIA CAR-66 AME LICENCE CA Form 19-09 Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Fields marked with an asterisk * are mandatory and must be completed in all cases. Use Date Format – DD-MM-YYYY Roll Number Allot- COMPUTER No. E ted 1.*PERSONAL DETAILS Licence No. ( If held) FIRST NAME MIDDLE NAME SURNAME AME Licence RTR 2. DETAILS OF LICENCE HELD ( If held) CAT/ SUB-CAT AIRCRAFT TYPE CAT/ SUB-CAT AIRCRAFT TYPE 3.*DETAILS OF SKILL TEST APPLIED FOR: CAT/ SUB-CAT AIRCRAFT TYPE EXAMINATION CENTRE 1.1 *DETAILS OF PREVIOUS SKILL TEST (For the same Airframe and Engine combination): CAT/ SUB-CAT AIRCRAFT TYPE DATE of EXAMINATION CENTRE 4.*EXAMINATION MODULE(S) passed relevant to Cat/ Sub-Cat applied for ) Module Session Module Session Module Session Page 112 of 180 Issue II datedCAR-66 5.*DETAILS OF SPECIFIC PAPER / OF TYPE COURSE PASSED: SESSION / Name of Level of the MARKS CAT/ SUB-CAT AIRCRAFT TYPE the Approved Organ- RESULT Course secured isation 6. * DETAILS OF AIRCRAFT TYPE MAINTENANCE EXPERIENCE Duration Type of aircraft/ Organization Area or Work Period in engine/ system From To months 7. *FEE DEAILS: ROLL NUMNER ALLOTED Fees Demand Draft/ Banker’s Cheque No. Date of Issue Name of Bank 8. *DECLARATION (delete as appropriate) I hereby declare that the information provided in this form is correct in every respect to the best of my knowledge and belief and that nothing has been concealed or withheld by me. I understand that if any of my particulars/ entries are found false or incorrect before or after the examination, my candidature shall be re- jected and further action can be taken against me by DGCA as deemed fit. Further, I declare that I have read and understood the INSTRUCTIONS. PLACE SIGNATURE DATE NAME DGCA Enclosure Tick 9.*DETAILS OF ENCLOSURES Re- No Mark marks 1. Details of DGCA Examinations passed. I Session Module No. and Paper No. Roll No. passed 3. Electrical Fundamentals I(1) 4. Electronic Fundamental I(2) 5.Digital Techniques/ Electronic instrument Systems I(3) 6. Materials & Hardwares I(4) Page 113 of 180 Issue II datedCAR-66 7. Maintenance Practices I(5) 8. Basic Aerodynamics I(6) 9. Human Factors I(7) 10. Aviation Legislation I(8) 11A. Turbine Engine Aeroplane Aerodynamics, Struc- I(9) tures and Systems 11B. Piston Engine Aeroplane Aerodynamics, Struc- I(10) tures and Systems 12. Helicopter Aerodynamics, Structures and Systems I(11) 13. Aircraft Aerodynamics, Structures and Systems I(12) 14. Propulsion I(13) 15. Gas Turbine Engine I(14) 16. Piston Engine I(15) 17. Propeller I(16) 2. Type course completion certificate with examination II result sheet 3. Certified true copy of previous skill test result, if any III 4. Certified true copies of Logbook / Work records on IV CA Form 19-10 Please refer to current notification for details of fees required. All original documents if required to be submitted, will be returned through the self addressed cover affixed with necessary postal stamp (for speed post). Completed ap- plication should be posted along with the required documentation to the respective regional / sub-regional office. It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, issue, renewal or variation of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable to administrative/legal actions as per Aircraft Rules 1937. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Li- cence. Notes: Having clear concise supporting data will enable regional office to process the application more effective- ly and with less risk of errors or rejections. Regional office will not contact you for clarification of details on applications and therefore it is most important that you have the correct information before applying. Failure to submit a correctly completed application form and the required documentation will lead to the rejec- tion of your application and fee submitted would be utilized for processing the application. Page 114 of 180 Issue II datedCAR-66 FOR OFFICIAL USE NAME OF CANDIDATE ROLL NUMBER CAT/ SUB-CAT AIRCRAFT TYPE Candidate was examined on the following topics: Candidate was found weak in the following topics: Percentage marks awarded in the Skill Test and Results: Date of Skill Test Cat/ Sub-Cat Aircraft Type % Marks Pass/ Fail Issue/ Extension/ of AME licence in respect of Sh. ___________________________ is recommended only in Cat/ Sub-Cat_____ to cover _____________________ (Aircraft). (Signature) Member of Examina- (Signature) Member of Examina- (Signature) Member of Exami- tion Board tion Board nation Board Name: Name: Name: Date: Date: Date: Page 115 of 180 Issue II datedCAR-66 FORMAT OF AIRCRAFT MAINTENACE ENGINEER DGCA INDIA WORK RECORD / LOG BOOK CA Form 19-10 Affix recent pass- 1. PERSONAL DETAILS port size photo graph duly at- CEO Computer tested on the No. front side *Name in full * Nationali- *Date of birth ty *Educational GENDER M / F AME Licence No. Qualification *Permanent Address……………………………………………................……………………………………………………………………… ……………………………………………………………………………………………………..……………PIN Code.................................... Changed Permanent Address *Address for Communication (if different from above)………………………........................................................... ………………………………………………………………………………………………………………..….PIN Code................................... Changed Address for Communication: Applicant Contact Phone Number ………………………….............. E-mail…….………………………………..………………. Name of the Current Employer………………………………………………………………………………………………………………. Contact Phone Number of Employer ………………….................... E-mail…….………………………………………………… Log Book Owners Name…………………………………………………………….... Signature ……………………………………….. Page 116 of 180 Issue II datedCAR-66 2. Record of Training: Training Completed Training Establish- From To Result ment and Location Page 117 of 180 Issue II datedCAR-66 3. (i) Details of Employer / Organisation at which engaged in Aircraft Maintenance Employer / Organisation: FROM To Position Nature of Work Types of Aircraft or other products Confirmation of the Organisation NAME SIGNATURE POSITION & STAMP DATE 3 (ii). Details of Employer / Organisation at which engaged in Aircraft Maintenance Employer / Organisation: FROM To Position Nature of Work Types of Aircraft or other products Confirmation of the Organisation NAME SIGNATURE POSITION & STAMP DATE 3 (iii) . Details of Employer / Organisation at which engaged in Aircraft Maintenance Employer / Organisation: FROM To Position Nature of Work Types of Aircraft or other products Confirmation of the Organisation NAME SIGNATURE POSITION & STAMP DATE Page 118 of 180 Issue II datedCAR-66 4.BASIC SKILL Supervisor *Typical Maintenance Tasks Aircraft Reg. Date on which Organization Name and CATEGORY (1) No & Type (2) performed (3) (4) AME Licence No. I. Time limit/ Maintenance # # LV .Accessory Gear Box c. *Check Chip detector (cid:183) All the applicable aircraft maintenance tasks listed under Appendix II to AMC of CAR-66 should be re- produced under column (1). (cid:183) Details of tasks performed should be furnished under column 2, 3, 4 and 5 (cid:183) Maintenance tasks not performed should be indicated as “ NOT PERFORMED” 5.*DECLARATION I hereby confirm that the information contained in this form was correct at the time of application. PLACE SIGNATURE DATE NAME It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, issue, renewal or variation of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable to administrative/legal actions as per Aircraft Rules 1937. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Air- craft Maintenance Engineer’s Licence. Page 119 of 180 Issue II datedCAR-66 APPLICATION FOR ISSUE OF BASIC KNOWLEDGE DGCA INDIA EXAMINATION CERTIFICATE CA Form 19-11 Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Fields marked with an asterisk * are mandatory and must be completed in all cases. Use Date Format – DD-MM-YYYY 1. *PERSONAL DETAILS CEO Computer No. *Name in full *Permanent address ……………………..………………………………………………………………………………………………….. …………………………………………………………………………………………………………….. PIN Code................................ *Address for Communication (if different from above) ……………………..………… ……………………..……………………………………………………………………………………… PIN Code................................ Applicant Contact Phone Number ………………………..................E-mail…….……………………………………….. Name of the Current Employer………………………………………………………………………….. Contact Phone Number of Employer …………………….................. E-mail…….………………………………………… 2. *APPLICATION I hereby request DGCA to issue of basic knowledge examination certificate as indicated and confirm that the information contained in this form was correct at the time of application ( Specify the re- quired category / sub-category of basic knowledge certificate) Category/Sub-category of License applied for A B Mechanical Avionic 3. *Details of basic modules/papers relevant to modules passed Page 120 of 180 Issue II datedCAR-66 Exam Session Exam Session Category/sub- Category/sub- Module No. in which Module No. in which category category Passed Passed 4 *FEE DEAILS: Demand Draft/ Banker’s Cheque Fees No. Name of Bank Date of Issue 5.*DECLARATION I hereby confirm that: i) I apply for issue of basic knowledge certificate as indicated and confirm that the information contained in this form was correct at the time of application ii) I did not apply earlier to the office of DGCA for issue of basic knowledge certificate and the request was not turned down. PLACE SIGNATURE DATE NAME It is an offence to make, with intent to deceive, any false representations for the purpose of procur- ing the grant, issue, renewal or variation of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable to administrative/legal actions as per Aircraft Rules 1937. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. 5.*DETAILS OF DOCUMENTS, PHOTOGRAPH AND FEE ENCLO- Enclosure Tick DGCA SURES No. Mark Remarks Page 121 of 180 Issue II datedCAR-66 Details of DGCA Examinations passed : I Session Module No. and Paper No. Roll No. passed 3. Electrical Fundamentals I (a) 4. Electronic Fundamental I (b) 5.Digital Techniques/ Electronic instrument I (c) Systems 6. Materials & Hardwares I (d) 7. Maintenance Practices I (e) 8. Basic Aerodynamics I (f) 9. Human Factors I (g) 10. Aviation Legislation I (h) 11A.Turbine Engine Aeroplane Aerodynam- I (i) ics, Structures and System 11B. Piston Engine Aeroplane Aerodynamics, I (j) Structures and Systems 12. Helicopter Aerodynamics, Structures and I (k) Systems 13. Aircraft Aerodynamics, Structures and I (l) Systems 14. Propulsion I (m) 15. Gas Turbine Engine I (n) 16. Piston Engine I (o) 17. Propeller I (p) Please refer to current notification for details of fees required. All original documents submitted will be returned through the self addressed cover affixed with necessary postal stamp (for speed post). Completed application should be posted along with the required documentation to the Central Ex- amination Organisation, O/o the Directorate General of Civil Aviation, East block II, R K Puram, New Delhi 110066. Notes: Having clear concise supporting data will CEO to issue licences more effectively and with less risk of errors or rejections. CEO will not contact you for clarification of details on applications and therefore it is most important that you have the correct information before applying. Failure to submit a correctly completed application form and the required documentation will lead to the rejection of your application and the fee will be utilized for processing the application. Page 122 of 180 Issue II datedCAR-66 DGCA INDIA CA Form 19-12 DIRECTORATE GENERAL OF CIVIL AVIATION CENTRAL EXAMINATION ORGANIZATION East Block III, RK Puram, New Delhi 110066 Aircraft Maintenance Engineer’s Basic Knowledge Examination Certificate This is to certify that Mr./Ms ______________________________________________________ Computer Number. ___________________________ has passed the following subjects/module/ papers examinations conducted by this office in partial fulfillment of requirements for grant of Aircraft Maintenance Engineer’s License. Stream/Category/Papers/ Module names: _ __________________ Session ____________in which Passed. Seal Signatures (Head, Central Examination Organization) For the Director General of Civil Aviation Appendix VI - Aircraft Maintenance Engineer’s Licence referred to in Rule 61 of the Aircraft Rules, 1937-CA Form 26 Page 123 of 180CAR-66 CA 26 GOVERNMENT OF INDIA DIRECTORATE GENERAL OF CIVIL AVIA- TION CAR-66 AIRCRAFT MAINTENANCE ENGINEER’s LI- CENCE I INDIA IX. CONDITIONS a. Certified that holder is authorized to exercise the privi- II. Aircraft Maintenance Engineer’s Licence leges of the licence as given in Rule 61 of the Aircraft III. Licence number Rules, 1937. b. Endorsement of aircraft types at section XII(b) titled Name of holder in STAMP SIZE IV. AIRCRAFT TYPE RATING means the holder is qualified full PHOTO to issue a certificate of release to service for such air- IVa Date of birth craft from the date of endorsement with a valid author- ization issued by approved maintenance organization. V. Address of holder c. Holder of this licence shall not exercise the privileges of the licence and related ratings at any time when he/she is aware of any decrease in medical fitness which might VI. Nationality render him/her unable to safely and properly exercise VII. Signature of these privileges. Holder d. This licence is not valid unless it bears the signature of the holder. VIII. Issued in accordance with the provisions of the Aircraft e. This licence remains current until the expiry date spec- Act 1934, and Aircraft Rules 1937. ified at section XIV whilst in compliance with the Air- craft Rule 61 and CAR 66 unless previously suspended X Signature of or revoked. Issuing Authorit ………………………………………………..…… f. This licence when endorsed with an aircraft type rating (for the Director General of Civil Aviation) meets the intent of ICAO Annex 1. g. Entry, endorsement or alteration in the licence shall be made by person authorized for this purpose by the Di- Date of Issue: rector General. XI. Stamp of the Issuing Authority 1 III. LIC No. 2 XII (a). LICENCE (SUB) CATEGORIES XII (b). AIRCARFT TYPE RATING Page 124 of 180CAR-66 CATEGORIES A B1 B2 C DATE AIRCRAFT TYPE OR GROUP CATEGORY STAMP & DATE AEROPLANES TURBINE n/a n/a AEROPLANES PISTON n/a n/a HELICOPTERS TURBINE n/a n/a HELICOPTERS PISTON n/a n/a AVIONICS n/a n/a n/a AIRCRAFT n/a n/a n/a III. LIC No. 3 III. LIC No. 4 XIII. LIMITATIONS XIV. LICENCE VALIDITY AIRCRAFT SIGNATURE WITH DATE LIMITATION DATE OF EXPI- SIGNATURE WITH TYPE OR CATEGORY (REMOVAL OF LIMITA- SEAL CODE RY DATE GROUP TION) III. LIC No. 5 III. LIC No 6 Page 125 of 180 Issue II datedCAR-66 XIV a). LICENCE ENDORSEMENTS INHERITED FROM THE XIV (b). REMARKS AME LICENCE HELD PRIOR TO CAR-66 LICENCE SIGNATURE WITH RATING CATEGORY DATE III. LIC No. 7 III. LIC No. 8 Page 126 of 180 Issue II datedCAR-66 1. The aircraft maintenance engineer’s licence once issued is required to be kept by the person to whom it applies in good condition and who shall remain accountable for en- suring that no unauthorized entries are made. 2. Failure to comply with paragraph 1 may invalidate the document and could lead to the holder not being permitted to hold any CAR -145 certification authorization 3. Failure to comply with paragraph 1 may also result in prosecution under relevant Indian Penal Code. 4. Each page issued shall be in this format and contain the specified information for that page. 5. If there are no limitations applicable, the LIMITATIONS page will be issued stating ‘No limitations’. Page 127 of 180 Issue II datedCAR-66 Acceptable Means of Compliance (AMC) / Guidance Material (GM) to SECTION A of CAR-66 This chapter contains Acceptable Means of Compliance (AMC) and Guidance Material ( GM ) to CAR - 66 Section A– Technical Requirements. Acceptable Means of Compliance (AMC) illustrate a means, or several alternative means, but not necessarily the only pos- sible means by which a requirement can be met. SECTION A TECHNICAL REQUIREMENTS GM 66.A.3 Licence categories Individual aircraft maintenance licence holders need not be restricted to a single catego- ry. Provided that each qualification requirement is satisfied, any combination of catego- ries may be granted. AMC 66.A.10 Application 1. Maintenance experience should be written in a manner that the reader has a reason- able understanding of where, when and what maintenance constitutes the experience. A task by task account is not necessary but at the same time a blank statement “X year’s maintenance experience completed” is not acceptable. A log book of maintenance expe- rience is desirable and be kept. It is acceptable to cross refer in the CA Form 19-01 to other documents containing information on maintenance. 2. Applicants claiming the maximum reduction in 66.A.30 (a) total experience based upon having successfully completed approved basic training should include the certifi- cate of approval with its validity schedule of the training establishment. 3. Applicants claiming reduction in 66.A.30 (a) total experience based upon having suc- cessfully completed technical training in an organization or institute recognized by DGCA as a competent organization or institute should include the relevant certificate of successful completion of training. AMC 66.A.15 (a) Eligibility To prove the equivalence to 10 +2, the applicant is required to submit a certificate from a competent authority such as Association of Indian Universities (AIU). Page 128 of 180 Issue II datedCAR-66 GM 66.A.20(a) Privileges 1. The following definitions apply: Electrical system means the aircraft electrical power supply source, plus the distribu- tion system to the different components contained in the aircraft and relevant connect- ors. Lighting systems are also included in this definition. When working on cables and connectors which are part of these electrical systems, the following typical practices are included in the privileges: (cid:183) Continuity, insulation and bonding techniques and testing; (cid:183) Crimping and testing of crimped joints; (cid:183) Connector pin removal and insertion; (cid:183) Wiring protection techniques. Avionics system means an aircraft system that transfers, processes, displays or stores analogue or digital data using data lines, data buses, coaxial cables, wireless or other da- ta transmission medium, and includes the system’s components and connectors. Exam- ples of avionics systems include the following: (cid:183) Autoflight; (cid:183) Communication, Radar and Navigation; (cid:183) Instruments (see NOTE below); (cid:183) In-Flight Entertainment Systems; (cid:183) Integrated Modular Avionics (IMA); (cid:183) On-Board Maintenance Systems; (cid:183) Information Systems; (cid:183) Fly-by-Wire Systems (related to ATA27 “Flight Controls”); (cid:183) Fibre Optic Control Systems. NOTE: Instruments are formally included in the privileges of the B2 licence holders. However, maintenance on electromechanical and pitot-static components may also be released by a B1 license holder. Simple test means a test described in approved maintenance data and meeting all the following criteria: (cid:183) The serviceability of the system can be verified using aircraft controls, switches, Built-in Test Equipment (BITE), Central Maintenance Computer (CMC) or exter- nal test equipment not involving special training. (cid:183) The outcome of the test is a unique go–no go indication or parameter, which can be a single value or a value within an interval tolerance. No interpretation of the test result or interdependence of different values is allowed. Page 129 of 180 Issue II datedCAR-66 (cid:183) The test does not involve more than 10 actions as described in the approved maintenance data (not including those required to configure the aircraft prior to the test, i.e. jacking, flaps down, etc., or to return the aircraft to its initial configu- ration). Pushing a control, switch or button, and reading the corresponding out- come may be considered as a single step even if the maintenance data shows them separated. Troubleshooting means the procedures and actions necessary to identify the root cause of a defect or malfunction using approved maintenance data. It may include the use of BITE or external test equipment. Line maintenance means any maintenance that is carried out before flight to ensure that the aircraft is fit for the intended flight. It may include: (cid:183) trouble shooting; (cid:183) defect rectification; (cid:183) component replacement with the use of external test equipment, if required. Component replacement may include components such as engines and propel- lers; (cid:183) scheduled maintenance and/or checks including visual inspections that will de- tect obvious unsatisfactory conditions/discrepancies but do not require exten- sive in-depth inspection. It may also include internal structure, systems and powerplant items which are visible through quick opening access panels/doors; (cid:183) minor repairs and modifications which do not require extensive disassembly and can be accomplished by simple means; (cid:183) for temporary or occasional cases (Airworthiness Directives, hereinafter AD; ser- vice bulletins, hereinafter SB) the quality manager may accept base maintenance tasks to be performed by a line maintenance organisation provided all require- ments are fulfilled. The DGCA will prescribe the conditions under which these tasks may be performed. Base Maintenance means any task falling outside the criteria are given above for Line Maintenance. NOTE: Aircraft maintained in accordance with “progressive” type programmes need to be indi- vidually assessed in relation to this paragraph. In principle, the decision to allow some “progressive” checks to be carried out is determined by the assessment that all tasks within the particular check can be carried out safely to the required standards at the designated line maintenance station. 2. Reserved 3. The category C licence permits certification of scheduled base maintenance by the is- sue of a single certificate of release to service for the complete aircraft after the comple- tion of all such maintenance. The basis for this certification is that the maintenance has Page 130 of 180 Issue II datedCAR-66 been carried out by competent mechanics and category B1, B2 support staff, as appro- priate have signed for the maintenance tasks under their respective specialisation. The principal function of the category C certifying staff is to ensure that all required mainte- nance has been called up and signed off by the category B1, B2 support staff, as appro- priate, before issue of the certificate of release to service. Only category C personnel who also hold category B1, B2 qualifications may perform both roles in base mainte- nance. AMC 66.A.20 (b) (2) Privileges The 6 months maintenance experience in 2 years should be understood as consisting of two elements, duration and nature of the experience. The minimum to meet the re- quirements for these elements may vary depending on the size and complexity of the aircraft and type of operation and maintenance. 1. Duration: Within an approved maintenance organization: (cid:45) 6 months continuous employment within the same organisation; or (cid:45) 6 months split up into different blocks, employed within the same or in different or- ganisations. The 6 months period can be replaced by 100 days of maintenance experience in accord- ance with the privileges, whether these have been performed within an approved organ- isation or as independent certifying staff according to M.A.801 (b) 2 or as a combination thereof. When certifying staff maintains and releases aircraft in accordance with M.A.801 (b) 2, in certain circumstances this number of days may even be reduced by 50% when agreed in advance by the DGCA. These circumstances consider the cases where the holder of a CAR-66 licence happens to be the owner of an aircraft and carries out maintenance on his own aircraft, or where a licence holder maintains an aircraft operated for low utiliza- tion, that does not allow the licence holder to accumulate the required experience. This reduction should not be combined with the 20% reduction permitted when carrying out technical support, or maintenance planning, continuing airworthiness management or engineering activities. To avoid a too long period without experience, the working days should be spread over the intended 6 months period. 2. Nature of the experience: Depending on the category of the aircraft maintenance engineer’s licence, the following activities are considered relevant for maintenance experience: - Servicing; - Inspection; - Operational and functional testing; Page 131 of 180 Issue II datedCAR-66 - Trouble-shooting; - Repairing; - Modifying; - Changing component; - Supervising these activities; - Releasing aircraft to service. For category A certifying staff, the experience should include exercising the privileges, by means of performing tasks related to the authorization on at least one aircraft type for each licence subcategory. This means tasks as mentioned in AMC 145.A.30 (g), in- cluding servicing, component changes and simple defect rectifications. For category B1 and B2, for every aircraft included in the authorization the experience should be on that particular aircraft or on a similar aircraft within the same licence sub- category. Two aircraft can be considered as similar when they have similar technology, construction and comparable systems, which means equally equipped with the follow- ing (as applicable to the licence category): (a) Propulsion systems (piston or turboprop or turbofan or turboshaft or jet-engine or push propellers); and (b) Flight control systems (only mechanical controls or hydro-mechanically powered controls or electro-mechanically powered controls); and (c) Avionic systems (analog systems or digital systems); and (d) Structure (manufactured of metal or composite or wood). For licences endorsed with (sub)group ratings: (cid:45) In the case of B1 licence endorsed with group ratings (either manufacturer group or full group) as defined in 66.A.45(g) the holder may show experience on at least one aircraft type per group and per aircraft structure (metal, composite, wood). (cid:45) In the case of a B2 licence endorsed with group ratings (either manufacturer group or full group) as defined in 66.A.45 (g) the holder may show experience on at least one aircraft type per group. For category C, the experience should cover at least one of the aircraft types endorsed on the authorization. For a combination of categories, the experience should include some activities of the na- ture shown in paragraph 2 in each category. Page 132 of 180 Issue II datedCAR-66 A maximum of 20% of the experience duration required may be replaced by the follow- ing relevant activities on an aircraft type of similar technology, construction and with comparable systems: (cid:45) Aircraft maintenance related training as an instructor/assessor or as a student; (cid:45) Maintenance technical support/engineering; (cid:45) Maintenance management/planning. The experience should be documented in an individual log book or in any other record- ing system (which may be an automated one) containing the following data: (a) Date and time; (b) Aircraft type; (c) Aircraft identification i.e. registration; (d) ATA chapter; (e) Operation performed i.e. 100 FH check, MLG wheel change, engine oil check and complement, SB embodiment, trouble shooting, structural repair, STC embodi- ment…; (f) Type of maintenance i.e. base, line; (g) Type of activity i.e. perform, supervise, release; (h) Category used A, B1, B2 or C. (i) Duration in days or partial-days. GM 66.A.20(b)2 Privileges The sentence “met the provision for the issue of the appropriate privileges” included in 66.A.20(b)2 means that during the previous 2 years the person has met all the require- ments for the endorsement of the corresponding aircraft rating (for example, in the case of aircraft in Group 1, theoretical plus practical element plus, if applicable, on-the-job training). This supersedes the need for 6 months of experience for the first 2 years. However, the requirement of 6 months of experience in the preceding 2 years will need to be met after the second year. AMC 66.A.20(b)3 Privileges The wording “has the adequate competence to certify maintenance on the correspond- ing aircraft” means that the licence holder and, if applicable, the organisation where he/she is contracted/employed, should ensure that he/she has acquired the appropriate knowledge, skills, attitude and experience to release the aircraft being maintained. This is essential because some systems and technology present in the particular aircraft be- Page 133 of 180 Issue II datedCAR-66 ing maintained may not have been covered by the training/examination/experience re- quired to obtain the licence and ratings. This is typically the case, among others, in the following situations: (cid:183) Type ratings which have been endorsed on a licence in accordance with Appen- dix I to AMC to CAR-66 “List of Type Ratings” after attending type training/on- the-job training which did not cover all the models/variants included in such rat- ing. For example, a licence endorsed with the rating Airbus A318/A319/A320/A321 (CFM56) after attending type training/on-the-job train- ing covering only the Airbus 320 (CFM56). (cid:183) Type ratings which have been endorsed on a licence in accordance with Appen- dix I to AMC to CAR-66 “List of Type Ratings” after a new variant has been added to the rating in Appendix I, without performing difference training. For example, a licence endorsed with the rating Boeing 737-600/700/800/900 for a person who already had the rating Boeing 737-600/700/800, without performing any difference training for the 737-900. (cid:183) Work being carried out on a model/variant for which the technical design and maintenance techniques have significantly evolved from the original model used in the type training/on-the-job training. (cid:183) Specific technology and options selected by each customer which may not have beencovered by the type training/on-the-job training. (cid:183) Changes in the basic knowledge requirements of Appendix I to CAR -66 not re- quiring reexamination of existing licence holders (grandfathered privileges). (cid:183) The endorsement of group/subgroup ratings based on experience on a repre- sentative number of tasks/aircraft or based on type training/examination on a representative number of aircraft. (cid:183) Persons meeting the requirements of 6 months of experience every 2 years only oncertain similar aircraft types as allowed by AMC 66.A.20(b)2. (cid:183) Persons holding a CAR-66 licence with limitations, obtained through conversion of pre-existing qualifications (66.A.70), where such limitations are going to be lifted after performing the corresponding basic knowledge examinations. In this case, the type ratings endorsed in the licence may have been obtained without covering all the aircraft systems (because of the previous limitations) and there will be need to assess and, if applicable, to train this person on the missing sys- tems. Additional information is provided in AMC 145.A.35(a). Page 134 of 180 Issue II datedCAR-66 GM 66. A. 20 (b) 4 Privileges 1. Holders of a CAR-66 aircraft maintenance licence may not exercise certification privi- leges unless they have a general knowledge of the language used within the mainte- nance environment including knowledge of common aeronautical terms in the lan- guage. The level of knowledge should be such that the licence holder is able to: -read and understand the instructions and technical manuals in use within the organisation; (cid:45) make written technical entries and any maintenance documentation entries, which can be understood by those with whom they are normally required to communicate; (cid:45) read and understand the maintenance organisation procedures; (cid:45) communicate at such a level as to prevent any misunderstanding when exercising certification privileges. 2. In all cases, the level of understanding should be compatible with the level of cer- tification privileges exercised. GM 66.A.25(a) Basic knowledge requirements The levels of knowledge for each licence (sub)category are directly related to the com- plexity of the certifications related to the corresponding licence (sub)category, which means that category A should demonstrate a limited but adequate level of knowledge, whereas category B1, B2 should demonstrate a complete level of knowledge in the ap- propriate subject module AMC 66.A.30 (a) Experience requirements 1. For a category C applicant holding an academic degree the representative selection of tasks should include the observation of hangar maintenance, maintenance plan- ning, quality assurance, record-keeping, approved spare parts control and engi- neering development. 2. While an applicant to a CAR-66 Category C licence may be qualified by having 3 years experience as category B1 or B2 certifying staff only in line maintenance, it is however recommended that any applicant for a category C holding a B1 or B2 li- cence demonstrate at least 12 months experience as a B1 or B2 base maintenance support staff. 3. A skilled worker is a person who has successfully completed a training acceptable to the DGCA and involving the manufacture, repair, overhaul or inspection of me- chanical, electrical or electronic equipment. The training would include the use of tools and measuring devices. Page 135 of 180 Issue II datedCAR-66 4. Maintenance experience on operating aircraft: - Means the experience of being involved in maintenance tasks on aircraft which are being operated by airlines, air taxi organisations, owners, etc.; - Should cover a wide range of tasks in length, complexity and variety; - Aims at gaining sufficient experience in the real environment of maintenance as opposed to only the training school environment; - May be gained within different types of maintenance organisations (CAR-145, M.A. Subpart F etc.) or under the supervision of independent certifying staff; - May be combined with CAR-147 approved training so that periods of training can be intermixed with periods of experience, similar to an apprenticeship AMC 66.A.30 (d) Experience requirements To be considered as recent experience; at least 50% of the required 12 month experi- ence should be gained within the 12 month period prior to the date of application for the CAR-66 aircraft maintenance license. The remainder of the experience should have been gained within the 7 year period prior to application. It must be noted that the rest of the basic experience required by 66.A.30 must be obtained within the 10 years prior to the application as required by 66.A.30(f). AMC 66.A.30 (e) Experience requirements 1. For category A the additional experience of civil aircraft maintenance should be a minimum of 6 months. For category B1 or B2, B3 the additional experience of civil aircraft maintenance should be a minimum of 12 months. 2. Aircraft maintenance experience gained outside a civil aircraft maintenance envi- ronment can include aircraft maintenance experience gained in armed forces, coast guards, police etc. or in aircraft manufacturing. GM 66.A.40 Continued validity of the aircraft maintenance licence Validity of the CAR-66 aircraft maintenance licence is not affected by recency of mainte- nance experience whereas the validity of the 66.A.20 privileges is affected by mainte- nance experience as specified in 66.A.20 (a). GM 66.A.45(b) Endorsement with aircraft ratings An aircraft type rating includes all the aircraft models/variants listed in column 2 of Ap- pendix I to AMC to CAR-66. When a person already holds a type rating on the licence and such type rating is amended in the Appendix I to AMC to CAR-66 in order to include additional mod- els/variants, there is no need for additional type training for the purpose of amending the type rating in the licence. The rating should be amended to include the new variants, upon request by the applicant, without additional requirements. However, it is the re- sponsibility of the licence holder and, if applicable, the maintenance organisation where he/she is employed to comply with 66.A.20(b)3, 145.A.35(a) and M.A.607(a), as appli- cable, before he/she exercises certification privileges. Page 136 of 180 Issue II datedCAR-66 Similarly, type training courses covering certain, but not all the models/variants includ- ed in a type rating, are valid for the purpose of endorsing the full type rating AMC 66.A.45(e) Endorsement with aircraft ratings 1. For the granting of manufacturer subgroup ratings for Group 2 aircraft, for B1 and C licence holders, the sentence “at least two aircraft types from the same manufac- turer which combined are representative of the applicable manufacturer sub- group” means that the selected aircraft types should cover all the technologies rel- evant to the manufacturer subgroup in the following areas: - Flight control systems (mechanical controls/hydromechanically powered con- trols/electromechanically powered controls); and - Avionic systems (analogue systems/digital systems); and - purpose it may be possible to use aircraft types from the same manufacturer clas- sified in Group 1 as long as Structure (manufactured of metal/composite/wood). In cases where there are very different aircraft types within the same manufacturer subgroup, it may be necessary to cover more than two aircraft types to ensure ade- quate representation. For this the selected aircraft belong to the same licence sub- category for which the rating will be endorsed. 2. For the granting of full subgroup ratings for Group 2 aircraft, for B1 and C licence holders, the sentence “at least three aircraft types from different manufacturers which combined are representative of the applicable subgroup” means that the se- lected aircraft types should cover all the technologies relevant to the manufacturer subgroup in the following areas: - Flight control systems (mechanical controls/hydromechanically powered controls/ electromechanically powered controls); and - Avionic systems (analogue systems/digital systems); and - Structure (manufactured of metal/composite/wood). In cases where there are very different aircraft types within the same subgroup, it may be necessary to cover more than three aircraft types to ensure adequate repre- sentation. For this purpose it may be possible to use aircraft types from different manufacturers classified in Group 1 as long as the selected aircraft belong to the same licence subcategory for which the rating will be endorsed. 3. For manufacturer subgroup ratings, the term “manufacturer” means the TC holder defined in the certification data sheet, which is reflected in the list of type ratings in Appendix I to AMC to CAR-66. In the case of an aircraft rating where the type rating refers to a TC holder made of a combination of two manufacturers which produce a similar aircraft (i.e. AGUSTA/BELLELICOPTER TEXTRON or any case of aircraft similarly built by another manufacturer), this combination should be considered as one manufacturer. Page 137 of 180 Issue II datedCAR-66 As a consequence: (cid:183) When a licence holder gets a manufacturer type or a manufacturer subgroup rating made of a combination of manufacturers, it covers the combination of such manufacturers. (cid:183) When a licence holder who intends to endorse a full subgroup rating selects three aircraft from different manufacturers, this means from different combi- nations of manufacturers a applicable. AMC 66.A.45(d), (e)3, (f)1 and (g)1 Endorsement with aircraft ratings 1 The “practical experience” should cover a representative cross section including at least 50 % of tasks contained in Appendix II to AMC relevant to the licence cat- egory and to the applicable aircraft type ratings or aircraft (sub)group ratings be- ing endorsed. This experience should cover tasks from each paragraph of the Ap- pendix II list. Other tasks than those in the Appendix II may be considered as a replacement when they are relevant. In the case of (sub)group ratings, this expe- rience may be shown by covering one or several aircraft types of the applicable (sub)group and may include experience on aircraft classified in group 1, 2 and/or 3 as long as the experience is relevant. The practical experience should be ob- tained under the supervision of authorised certifying staff. 2 In the case of endorsement of individual type ratings for Group 2 and Group 3 aircraft, for the second aircraft type of each manufacturer (sub)group the practi- cal experience should be reduced to 30 % of the tasks contained in Appendix II to AMC relevant to the licence category and to the applicable aircraft type. For sub- sequent aircraft types of each manufacturer (sub)group this should be reduced to 20 %. 3. Practical experience should be demonstrated by the submission of records or a logbook showing the Appendix II tasks performed by the applicant. Typical data to be recorded are similar to those described in AMC 66.A.20(b)2. GM 66.A.45 Endorsement with aircraft ratings The following table shows a summary of the aircraft rating requirements contained in 66.A.45, 66.A.50 and Appendix III to CAR-66. The table contains the following: (cid:183) The different aircraft groups; (cid:183) For each licence (sub)category, which ratings are possible (at the choice of the applicant): o Individual type ratings; o Full and/or Manufacturer (sub)group ratings; Page 138 of 180 Issue II datedCAR-66 (cid:183) For each rating option, which are the qualification options; (cid:183) For the B1.2 licence (Group 3 aircraft) which are the possible limitations to be included in the licence if not sufficient experience can be demonstrated in those areas. Note: OJT means “On-the-Job Training” (Appendix III to CAR-66, Section 6) and is only required for the first aircraft rating in the licence (sub)category. Aircraft rating requirements Aircraft Groups B1 B2 licence C licence Group 1 (For B1) Individual TYPE Individual TYPE  Complex motor powered Individual TYPE RATING RATING RATING Type training: Type training: Type training: aircraft. - Theory + examination - Theory + examina-  Multiple engine helicopters. - Practical + assessment tion - Theory + examina-  Aeroplanes certified above PLUS - Practical + assess- tion FL290. OJT (for first aircraft in licence sub- ment category PLUS  Aircraft equipped with OJT (for first aircraft in fly-by-wire. licence category  Other aircraft when defined by the Agency DGCA Group 2: (For B1.1, B1.3, B1.4) Individual TYPE Individual TYPE Subgroups: Individual TYPE RATING RATING RATING 2a: single turboprop (type training + OJT) or (type training + OJT) type training or type aeroplanes (*) (type examination + practical experi- or (type examination + examination 2b: single turbine engine ence) practical experience) Full SUBGROUP helicopters (*) Full SUBGROUP RATING Full SUBGROUP RATING 2c: single piston-engine (type training + OJT) or (type exami- RATING type training or type helicopters (*) nation + practical experience) on at based on demonstra- examination on at least least 3 aircraft representative of that tion of practical experi- 3 aircraft representa- (*) Except those classified in subgroup ence tive of that subgroup Group Manufacturer SUBGROUP RATING Manufacturer Manufacturer (type training + OJT) or SUBGROUP RATING SUBGROUP RATING (type examination + practical experi- based on demonstra- type training or type ence) on at least 2 aircraft tion of practical experi- examination on at least representative of that manufacturer ence 2 aircraft representa- subgroup tive of that manufac- turer subgroup Group 3 (For B1.2) Individual TYPE Individual TYPE Piston-engine aeroplanes Individual TYPE RATING RATING RATING (except those classified in (type training + OJT) or (type training + OJT) type training or type (type examination + practical experi- or examination Group ence) (type examination + Full GROUP 3 RAT- Full GROUP 3 RATING practical experience) ING based on demonstration of practical Full GROUP 3 RAT- based on demonstra- experience ING tion of practical experi- Limitations: based on demonstra- ence  Pressurised aeroplanes tion of practical experi- ence  Metal aeroplanes  Composite aeroplanes  Wooden aeroplanes  Metal tubing & fabric aeroplanes Page 139 of 180 Issue II datedCAR-66 AMC 66.A.50(b) Limitations 1. The appropriate experience required to remove the limitations referred to in 66.A.45(f) and (g) should consist of the performance of a variety of tasks appropri- ate to the limitations under the supervision of authorised certifying staff. This should include the tasks required by a scheduled annual inspection. Alternatively, this experience may also be gained, if agreed by the DGCA, by theoretical and prac- tical training provided by the manufacturer, as long as an assessment is further carried out and recorded by this manufacturer. 2. It may be acceptable to have this experience on just one aircraft type, provided that this type is representative of the (sub)group in relation to the limitation being removed. 3. The application for the limitation removal should be supported by a record of ex- perience signed by the authorised certifying staff or by an assessment signed by the manufacturer after completion of the applicable theoretical and practical train- ing. GM 66.A.70 Conversion provisions 1. As described in point 66.A.70, the conversion provisions apply to the holder of a AME Licence prior to the date of entry into force of CAR-66. . 2. The conversion applies to “certifying staff qualifications” such as, for example: (cid:183) Holding a AME licence (or completed the process to obtain such a licence; This does not mean that in order to be entitled to a conversion process, the appli- cant has to be exercising certification privileges. A person may hold a “certifying staff qualification” while not having certification privileges (or while exercising very limited certification privileges below his/her qualification) for different rea- sons such as, for example, the following: (cid:183) The person is working as “support staff” in the base maintenance environment; (cid:183) The person has been authorised only for a very limited range of tasks (lower than what he/she would be entitled if his/her qualification is considered) since the person is working in a line station where the scope of tasks is very limited; (cid:183) The person holds a licence with a wider scope than the scope of the organisa- tion where he/she is employed; (cid:183) The person is working outside the aviation industry or is temporarily on leave due to different reasons (medical, personal, etc.). Page 140 of 180 Issue II datedCAR-66 These persons are entitled to have the conversion performed in accordance with the full scope of their qualification and the full privileges that they would be enti- tled to hold on the basis of such qualification. 3. As described in point 66.A.70, certifying staff qualifications eligible for conversion are those valid “prior to the date of entry into force of CAR-66”, which means those qualifications valid before the following dates: 4. Although only those certifying staff qualifications gained as indicated above are eli- gible for conversion, this does not mean that the application for conversion has to be submitted prior to those dates. The applicant is entitled to have the conversion per- formed irrespective of when he/she applies for conversion. 5. A certifying staff qualification can be subject to more than one conversion process and can also be converted to more than one licence (with any applicable limita- tions). This could be the case, for example, for a person who already had the certi- fying staff qualification converted to a B1.2 licence with limitations linked to some missing elements of the CAR-66 Appendix I and II standard (following 66.A.70(c)). This person would be entitled to apply and have his/her certifying staff qualifica- tion converted to a B1.2 on the basis of 66.A.70(d), which would mean that there is no need to compare with the CAR-66 Appendix I and II standard, introducing only those limitations required to maintain the existing privileges. GM 66.A.70(c) Conversion provisions For example, a limitation could be where a person holds a pre-existing certifying staff qualification which covered, to the standard of CAR-66 Appendix I and II, all the mod ules/subjects corresponding to the B1 licence except for electrical power systems. This person would receive a CAR-66 aircraft maintenance licence in the B1 category with a limitation (exclusion) on electrical power systems. For removal of limitations, refer to 66.A.50(c). GM 66.A.70(d) Conversion provisions In the case of aircraft not involved in commercial air transport other than large aircraft, an example of limitations could be where a person holds a pre CAR-66 qualification which covered privileges to release work performed on aircraft structures, powerplant, mechanical and electrical systems but excluded privileges on aircraft equipped with turbine engine, aircraft above 2 000 kg MTOM, pressurised aircraft and aircraft equipped with retractable landing gear. This person would receive a CAR-66 aircraft maintenance licence in the B1.2 or B3 (sub)category with the following limitations (ex- clusions): Page 141 of 180 Issue II datedCAR-66  Aircraft involved in commercial air transport (this limitation always exists);  Aircraft above 2 000 kg MTOM;  Pressurised aircraft;  Aircraft equipped with retractable landing gear. Another example of limitations could be where a pilot-owner holds a pre CAR-66 qualification which covered privileges to release work performed on aircraft struc- tures, powerplant, mechanical and electrical systems but limited to his/her own aircraft and to a particular aircraft type (for example, a Cessna 172). This pilot- owner would receive a CAR-66 aircraft maintenance licence in the B1.2 (sub)category with the following limitations (exclusions):  Aircraft involved in commercial air transport (this limitation always exists);  Aircraft other than a Cessna 172;  Aircraft not owned by the licence holder. The essential aspect is that the limitations are established in order to maintain the privi- leges of the pre CAR-66 qualification, without comparing the previous qualification with the standard of CAR-66 Appendix I and II. For removal of limitations, refer to 66.A.50(c). AMC to Section 1 of Appendix III to CAR-66 “Aircraft Type Training and Examina- tion Standard. On-the-Job Training” Aircraft type training 1. Aircraft type training may be subdivided in airframe and/or powerplant and/or avionics/electrical systems type training courses (cid:183) Airframe type training course means a type training course including all rele- vant aircraft structure and electrical and mechanical systems excluding the powerplant. (cid:183) Powerplant type training course means a type training course on the bare en- gine, including the build-up to a quick engine change unit. (cid:183) The interface of the engine/airframe systems should be addressed by either air- frame or powerplant type training course. In some cases, such as for general aviation, it may be more appropriate to cover the interface during the airframe course due to the large variety of aircraft that can have the same engine type in- stalled. Page 142 of 180 Issue II datedCAR-66 (cid:183) Avionics/electrical systems type training course means type training on avion- ics and electrical systems covered by but not necessarily limited to ATA (Air Transport Association) Chapters 22, 23, 24, 25, 27, 31, 33, 34, 42, 44, 45, 46, 73 and 77 or equivalent. 2. Practical training may be performed either following or integrated with the theoret- ical elements. However, it should not be performed before theoretical training. 3. The content of the theoretical and practical training should: (cid:183) address the different parts of the aircraft which are representative of the struc- ture, the systems/components installed and the cabin; and (cid:183) include training on the use of technical manuals, maintenance procedures and the interface with the operation of the aircraft. Therefore, it should be based on the following elements: (cid:183) Type design including relevant type design variants, new technology and tech- niques; (cid:183) Feedback from in-service difficulties, occurrence reporting, etc.; (cid:183) Significant applicable airworthiness directives and service bulletins; (cid:183) Known human factor issues associated with the particular aircraft type; (cid:183) Use of common and specific documentation, (when applicable, such as MMEL, AMM,MPD, TSM, SRM, WD, AFM, tool handbook), philosophy of the trouble- shooting, etc.; (cid:183) Knowledge of the maintenance on-board reporting systems and ETOPS mainte- nance conditions, when applicable; (cid:183) Use of special tooling and test equipment and specific maintenance practises in- cluding critical safety items and safety precautions; (cid:183) Significant and critical tasks/aspects from the MMEL, CDL, Fuel Tank Safety (FTS), airworthiness limitation items (ALI) including Critical Design Configura- tion Control Limitations (CDCCL), CMR and all ICA documentation such as MRB, MPD, SRM, AMM, etc., when applicable. (cid:183) Maintenance actions and procedures to be followed as a consequence of specific certification requirements, such as, but not limited to, RVSM (Reduced Vertical Separation Minimum) and NVIS (Night Vision Imaging Systems); (cid:183) Knowledge of relevant inspections and limitations as applicable to the effects of environmental factors or operational procedures such as cold and hot climates, wind, moisture, sand, de-icing/anti-icing, etc. The type training does not necessarily need to include all possible customer options corresponding to the type rating described in the Appendix I to AMC to CAR-66. 4. Limited avionic system training should be included in the category B1 type training as the B1 privileges include work on avionics systems requiring simple tests to prove their serviceability. Page 143 of 180 Issue II datedCAR-66 5. Electrical systems should be included in both categories of B1 and B2 type training. 6. The theoretical and practical training should be complementary and may be: (cid:183) Integrated or split; (cid:183) Supported by the use of training aids, such as, trainers, virtual aircraft, aircraft components, synthetic training devices (STD), computer-based training devices (CBT), etc. AMC to Paragraph 3.1(d) of Appendix III to CAR-66 “Aircraft Type Training and Examination Standard. On-the-Job Training” Training Needs Analysis for the theoretical element of the aircraft type training 1. The minimum duration for the theoretical element of the type rating training course, as described in Appendix III to CAR-66, has been determined based on: (cid:183) generic categories of aircraft and minimum standard equipment fit; (cid:183) the estimated average duration of standard courses imparted in Europe. 2. The purpose of the Training Needs Analysis (TNA) is to adapt and justify the du- ration of thecourse for a specific aircraft type. This means that the TNA is the main driver for determining the duration of the course, regardless of whether it is above or below the minimum duration described in Appendix III to CAR-66. In the particular case of type training courses approved on the basis of the re- quirements valid before Regulation this CAR is applicable and having a duration for the theoretical element equal to or above the minimum duration contained in paragraph 3.1(c) of Appendix III to CAR-66, it is acceptable that the TNA only co- vers the differences introduced by this CAR in paragraph 3.1(e) “Content” and the criteria introduced in paragraph 3.1(d) “Justification of course duration” related to the minimum attendance and the maximum number of training hours per day. This TNA may result in a change in the duration of the theoretical element. 3. The content and the duration deriving from the TNA may be supported by an anal- ysis from the Type Certificate holder. 4. In order to approve a reduction of such minimum duration, the evaluation done by the DGCA should be performed on a case-by-case basis appropriate to the air- craft type. For example, while it would be exceptional for a theoretical course for a large transport category aircraft such as an A330 or B757 to be below the mini- mum duration shown, it would not necessarily be exceptional in the case of a Gen- eral Aviation (GA) business aircraft such as a Learjet 45 or similar. Typically, the TNA for a GA aircraft course would demonstrate that a course of a shorter dura- tion satisfies the requirements. Page 144 of 180 Issue II datedCAR-66 5. When developing the TNA, the following should be considered: a) The TNA should include an analysis identifying all the areas and elements where there is a need for training as well as the associated learning objectives, consider- ing the design philosophy of the aircraft type, the operational environment, the type of operations and the operational experience. This analysis should be written in a manner which provides a reasonable understanding of which areas and ele- ments constitute the course to meet the learning objectives. b) As a minimum, the Training Need Analysis (TNA) should take into account all the applicable elements contained in paragraph 3.1 of CAR-66 Appendix III and as sociated AMCs. c) The TNA should set up the course content considering the Appendix III objectives for each level of training and the prescribed topics in the theoretical element table contained in paragraph 3.1 of CAR-66 Appendix III. d) For each Chapter described in the theoretical element table contained in para- graph 3.1 of CAR-66 Appendix III, the corresponding training time should be rec- orded e) Typical documents to be used to identify the areas and elements where there is a need for training typically include, among others, the Aircraft Maintenance Manu- al, MRB report, CMRs, airworthiness limitations, Troubleshooting Manual, Struc- tural Repair Manual, Illustrated Parts Catalogue, Airworthiness Directives and Ser- vice Bulletins. f) During the analysis of these documents: (cid:183) Consideration should be given to the following typical activities: o Activation/reactivation; o Removal/installation; o Testing; o Servicing; o Inspection, check and repairs; o Troubleshooting/diagnosis. (cid:183) For the purpose of identifying the specific elements constituting the training course, it is acceptable to use a filtering method based on criteria such as: o Frequency of the task; o Human factor issues associated to the task; o Difficulty of the task; o Criticality and safety impact of the task; o In-service experience; o Novel or unusual design features (not covered by CAR-66 Appendix I); o Similarities with other aircraft types; o Special tests and tools/equipment. Page 145 of 180 Issue II datedCAR-66 (cid:183) It is acceptable to follow an approach based on: o Tasks or groups of tasks; or o Systems or subsystems or components. g) The TNA should: (cid:183) Identify the learning objectives for each task, group of tasks, system, subsystem or component; (cid:183) Associate the identified tasks to be trained to the regulatory requirements (table in paragraph 3.1 of Appendix III to CAR-66); (cid:183) Organise the training into modules in a logical sequence (adequate combination of chapters as defined in Appendix III of CAR-66); (cid:183) Determine the sequence of learning (within a lesson and for the whole syllabus); (cid:183) Identify the scope of information and level of detail with regard to the minimum standard to which the topics of the TNA should be taught according to the set-up objectives. (cid:183) Address the following: o Description of each system/component including the structure (where applicable); o System/component operation taking into account: a. Complexity of the system (e.g. the need of further breakdown into sub sys- tems, etc.); b. Design specifics which may require more detailed presentation or may contribute to maintenance errors; c. Normal and emergency functioning; d. Troubleshooting; e. Interpretation of indications and malfunctions; f. Use of maintenance publications; g. Identification of special tools and equipment required for servicing and maintaining the aircraft; h. Maintenance Practices; i. Routine inspections, functional or operational tests, rigging/adjustment, etc. (cid:183) Describe the following: o The instructional methods and equipment, teaching methods and blending of the teaching methods to ensure the effectiveness of the training; o The maintenance training documentation/material to be delivered to the stu- dent; o Facilitated discussions, questioning session, additional practice- oriented training, etc.; o The homework, if developed; o The training provider’s resources available to the learner. h) It is acceptable to differentiate between issues which have to be led by an instruc- tor and issues which may be delivered through interactive simulation training de- vices and/or covered by web-based elements. Overall time of the course will be al- located accordingly. Page 146 of 180 Issue II datedCAR-66 i) The maximum number of training hours per day for the theoretical element of type training should not be more than 6 hours. A training hour means 60 minutes of tu- ition excluding any breaks, examination, revision, preparation and aircraft visit. In exceptional cases, the DGCA may allow deviation from this standard when it is properly justified that the proposed number of hours follows pedagogical and hu- man factors principles. These principles are especially important in those cases where: (cid:183) Theoretical and practical training are performed at the same time; (cid:183) Training and normal maintenance duty/apprenticeship are performed at the same time. j) The minimum participation time for the trainee to meet the objectives of the course should not be less than 90 % of the tuition hours of the theoretical training course. Additional training may be provided by the training organisation in order to meet the minimum participation time. If the minimum participation defined for the course is not met, a certificate of recognition should not be issued. k) The TNA is a living process and should be reviewed/updated based on operation feedback, maintenance occurrences, Airworthiness Directives, major service bulle- tins impacting maintenance activities or requiring new competencies for mechan- ics, alert service bulletins, feedback from trainees or customer satisfaction, evolu- tion of the maintenance documentation such as MRBs, MPDs, MMs, etc. The fre- quency at which the TNA should be reviewed/updated is left to the discretion of the organisation conducting the course. NOTE: The examination is not part of the TNA. However, it should be prepared in accordance with the learning objectives described in the TNA. MC to Paragraphs 1(b), 3.2 and 4.2 of Appendix III to CAR-66 “Aircraft Type Training and Examination Standard. On-the-Job Training” Practical element of the aircraft type training 1. The practical training may include instruction in a classroom or in simulators but part of the practical training should be conducted in a real maintenance or manufacturer environment. 2. The tasks should be selected because of their frequency, complexity, variety, safety, criticality, novelty, etc. The selected tasks should cover all the chapters described in the table contained in paragraph 3.2 of Appendix III to CAR-66. 3. The duration of the practical training should ensure that the content of training re- quired by paragraph 3.2 of Appendix III to CAR-66 is completed. Nevertheless, for aeroplanes with a MTOM equal or above 30 000 kg, the duration for the practical el- ement of a type rating training course should not be less than two weeks unless a shorter duration meeting the objectives of the training and taking into account peda- gogical aspects (maximum duration per day) is justified to the DGCA. Page 147 of 180 Issue II datedCAR-66 4. The organisation providing the practical element of the type training should provide trainees with a schedule or plan indicating the list of tasks to be performed under in- struction or supervision. A record of the tasks completed should be entered into a logbook which should be designed such that each task or group of tasks may be coun- tersigned by the designated assessor. The logbook format and its use should be clear- ly defined. 5. In paragraph 4.2 of Appendix III to CAR-66, the term “designated assessors appropri- ately qualified” means that the assessors should demonstrate training and experience on the assessment process being undertaken and be authorised to do so by the organ- isation. Further guidance about the assessment and the designated assessors is provided in Appendix III to AMC to CAR-66. 6. The practical element (for powerplant and avionic systems) of the Type Rating Train- ing may be subcontracted by the approved CAR-147 organisation under its quality system according to the provisions of 147.A.145(d)3 and the corresponding Guidance Material. AMC to Paragraph 1(c) of Appendix III to CAR-66 “Aircraft Type Training and Ex- amination Standard. On-the-Job Training” Differences training Approved difference training is not required for different variants within the same air- craft type rating (as specified in Appendix I to AMC to CAR-66) for the purpose of type rating endorsement on the aircraft maintenance licence. However, this does not necessarily mean that no training is required before a certifying staff authorisation can be issued by the maintenance organisation (refer to AMC 66.A.20(b)3). AMC to Section 5 of Appendix III to CAR-66 “Aircraft Type Training and Examina- tion Standard. On-the-Job Training” Type Examination Standard This Section 5 “Type Examination Standard” does not apply to the examination per- formed as part of type training. This Section only applies to those cases where type ex- amination is performed as a substitute for type training. AMC to Section 6 of Appendix III to CAR-66 “Aircraft Type Training and Examina- tion Standard. On-the-Job Training” On-the-Job Training (OJT) 1. “A maintenance organisation appropriately approved for the maintenance of the par- ticular aircraft type” means a CAR-145 or M.A. Subpart F approved maintenance or- ganisation holding an A rating for such aircraft. Page 148 of 180 Issue II datedCAR-66 2. The OJT should include one-to-one supervision and should involve actual work task performance on aircraft/components, covering line and/or base maintenance tasks. 3. The use of simulators for OJT should not be allowed. 4. The OJT should cover at least 50 % of the tasks contained in Appendix II to AMC to CAR-66. Some tasks should be selected from each paragraph of the Appendix II list. Tasks should be selected among those applicable to the type of aircraft and licence (sub)category applied for. Other tasks than those in the Appendix II may be consid- ered as a replacement when they are relevant. Typically, in addition to the variety and the complexity, the OJT tasks should be selected because of their frequency, safe- ty, novelty, etc. 5. Up to 50 % of the required OJT may be undertaken before the aircraft theoretical type training starts. 6. The organisation providing the on-the-job training should provide trainees with a schedule or plan indicating the list of tasks to be performed under supervision. A rec- ord of the tasks completed should be entered into a logbook which should be de- signed such that each task or group of tasks is countersigned by the corresponding supervisor. The logbook format and its use should be clearly defined. 7. Regarding the day-to-day supervision of the OJT programme in the approved mainte- nance organisation and the role of the supervisor(s), the following should be consid- ered: (cid:183) It is sufficient that the completion of individual OJT tasks is confirmed by the di- rect supervisor(s), without being necessary the direct evaluation of the assessor. (cid:183) During the day-to-day OJT performance, the supervision aims at overseeing the complete process, including task completion, use of manuals and procedures, observance of safety measures, warnings and recommendations and adequate behaviour in the maintenance environment. (cid:183) The supervisor(s) should personally observe the work being performed to en- sure the safe completeness and should be readily available for consultation, if needed during the OJT performance. (cid:183) The supervisor(s) should countersign the tasks and release the maintenance tasks as the trainee is still not qualified to do so. (cid:183) The supervisor(s) should therefore: (cid:183) have certifying staff or support staff privileges relevant to the OJT tasks; (cid:183) be competent for the selected tasks; (cid:183) be safety-orientated; (cid:183) be capable to coach (setting objectives, giving training, performing supervision, evaluating, handling trainee’s reactions and cultural issues, managing objective- ly and positively debriefing sessions, determining the need for extra training or reorientate the training, reporting, etc.); (cid:183) be designated by the approved maintenance organisation to carry out the supervision. Page 149 of 180 Issue II datedCAR-66 8. Regarding the assessor, the following should be considered: (cid:183) The function of the assessor, as described in Section 6 of Appendix III to CAR-66, is to conduct the final assessment of the completed OJT. This assessment should include confirmation of the completion of the required diversity and quantity of OJT and should be based on the supervisor(s) reports and feedback. (cid:183) In Section 6 of Appendix III to CAR-66, the term “designated assessor appropri- ately qualified” means that the assessor should demonstrate training and expe- rience on the assessment process being undertaken and should be authorised to do so by the organisation. Further guidance about the assessment and the designated assessors is provided in Ap- pendix III to AMC to CAR-66. 9 The procedures for OJT should be included into the Exposition Manual of the ap proved maintenance organisation (Chapter 3.15, as indicated in AMC 145.A.70(a)). These procedures in the Exposition Manual are approved by the DGCA , and provid- ing training is not one of the privileges of a maintenance organisation, they can only be used when the licencing authority is the DGCA. In other cases, it is up to the li- cencing authority to decide whether it accepts such procedures for the purpose of approving the OJT (refer to AMC 66.B.115). AMC to Appendix III to CAR-66 “Aircraft Type Training and Examination Standard. On-the-Job Training” Aircraft type training and On-the-Job Training The theoretical and practical training providers, as well as the OJT provider, may con- tract the services of a language translator in the case where training is imparted to students not conversant in the language of the training material. Nevertheless, it re- mains essential that the students understand all the relevant maintenance documenta- tion.During the performance of examinations and assessments, the assistance of the translator should be limited to the translation of the questions, but should not provide clarifications or help in relation to those questions. Page 150 of 180 Issue II datedCAR-66 APPENDICES to AMC for CAR-66 Appendix I AIRCRAFT TYPE RATINGS FOR CAR-66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE The following aircraft type ratings should be used to ensure a common standard throughout India. The inclusion of an aircraft type in the licence does not indicate that the aircraft type has been granted a type certificate under the Aircraft Rule No. 49A and CAR-21, this list is only intended for the maintenance purposes. In order to keep this list current and type ratings consistent, such information should be first passed on to the DGCA daw@dgca.nic.in by affected personnel or organizations to issue a type rating that is not included in this list. Notes: When a modification is introduced to an aircraft type rating or to an engine designation in the rating which affect licences already issued, the ratings on the AME licences may be modified at the next renewal or when the licence is received for endorsement /re- issued, unless there is an urgent reason to modify the icence. Notes on aircraft modified by Supplemental Type Certificate STC: . (cid:183) When an aircraft has been modified by an STC for installation of another engine, the CAR-66 type rating of this aircraft may change i.e. from Group 2 to Group 1. This is not reflected in this document. In case the applicant to a licence faces such a case, the holder of AME License may inform the DGCA and a new type rat- ing will be defined by the DGCA In the following tables: (cid:183) The column ‘TC Holder’ includes the TC holder as defined in the Type Certificate Data Sheets TCDS (EASA, FAA or other) or the Specific Airworthiness Specifica- tions (SAS). (cid:183) Some TC holders’ designations have been corrected to add the information :’Aircraft with an SAS’, this means that the aircraft listed under this TC holder designation is considered an ‘orphan aircraft’. Page 151 of 180 Issue II datedCAR-66 (cid:183) In Group 3, a third column has been added which is called ‘Type of structure’ and which intends to assist the DGCA in identifying the experience required for this type with a view on removing existing limitations on the licence. (cid:183) Wooden structure covered with fabric is considered to fall under wooden struc- ture. For Aeroplanes with a combination of structures; e.g. metal tubing fuselage and wooden wings, both experience ‘metal tube covered with fabric’ and ‘wood- en structure’ are required. (cid:183) In Group 3, a fourth column has been added which is called ‘MTOM’ and which intends to assist in identifying the aeroplanes types where the Maximum Take- Off Mass (MTOM) is: (cid:183) — above 2T and is subject to a B1.2 licence, or (cid:183) — 2T and below and is subject to a B1.2 or B3 licence. Column 1 includes the TC holder as defined in the TCDS (EASA, FAA or other). For aeroplanes of group 1 and 2 and helicopters, the Column 2 includes the aircraft models as defined in the relevant TCDS (EASA, FAA or other). The following column includes the “commercial designation” when available. Column 3 includes the relevant individual type rating. Only the designations of ratings in column 3 should be used for endorsing individual type ratings on CAR-66 licences. Note: aircraft STC data are not included in this table. Page 152 of 180 Issue II datedCAR-66 Group -1 Aeroplanes Group -1 Aeroplanes Commercial Desig- 1. TC holder 2 Aeroplanes Model 3 Type Rating Endorsement nation A310-304 Airbus A310 (GE CF6) A310-324 Airbus A310 (PW 4000) A318-110 series A319-110 series A320-111 Airbus A318/A319/A320/A321 (CFM56) A320-210 series A321-110 series Airbus A321-210 series A319-130 series A320-230 series Airbus A319/A320/A321 (IAE V2500) A321-130 series A321-230 series A330-200 series Airbus A330 (GE CF6) A330-300 series A330-220 series Airbus A330 (PW 4000) A330-320 series L410 M AIRCRAFT IN- Let L-410 (Walter M601) DUSTRIES L-410 UVP-E9 Turbolet ATR 42-200 ATR 42-200/300 series (PWC PW120) ATR 42-320 ATR-GIE Avions ATR 72-200 series (PWC de Transport ATR 72-212 PW120) Régionals 42-500 ATR 42-500 42-600 ATR 42-400/500/72-212A (PWC 72-500 PW120) ATR 72-212 A 72-600 Page 153 of 180 Issue II datedCAR-66 Group -1 Aeroplanes Commercial Desig- 1. TC holder 2 Aeroplanes Model 3 Type Rating Endorsement nation BAe 146/ AVRO 146-RJ (Honeywell AVRO 146-RJ70 ALF500 Series) HS.748 Series 1 BAE SYSTEMS HS.748 Series 2 HS748 (RRD Dart) HS 748 Series 2A HS 748 Series 2B B737-200 Boeing 737-/200 (PW JT8D) B737-400 Boeing 737-400 (CFM56) B737-700 B737-800 Boeing 737-700/800/900 (CFM56) B737-900 B737-900ER B747-400 Boeing 747-400 (PW 4000) B747-400F/SF(BCF) B757-200 Boeing B757-200PF Boeing 757-200/300 (PW 2000) B757-300 B757-200 Boeing 757-200 (RR RB211) B777-200 B777-200LR Boeing 777-200/300 (GE 90) B777-300ER B777-200 Boeing 777-200/300 (PW 4000) B777-300 Boeing 787-8 (GE GEnx) B 787-8 Dreamliner Page 154 of 180 Issue II datedCAR-66 Group -1 Aeroplanes Commercial Desig- 1. TC holder 2 Aeroplanes Model 3 Type Rating Endorsement nation Boeing 787-8 (RR RB 211 Trent B 787-8 Dreamliner 1000) Bombardier BD-100-1A10 (Honey- BD-100-1A10 Challenger 300 well AS907) Global Express Bombardier BD-700 Series (RRD BD-700-1A10 Global 6000 BR710) Global 5000 BD-700-1A11 Global 5000 GVFD CL-600-2B16 (CL 604 Challenger-604 Bombardier CL-600-2B16 (variant Variant) (MSN < 5701) CL 604) (GE CF34} CL-600-2B16 (CL 604 Challenger-605 BOMBARDIER Variant) (MSN > 5701) CL-600-2B19 Regional Jet Series Bombardier CL-600-2B19 (GE CF34) 100/200 Bombardier CRJ 200(GE CF34) CRJ 200 Regional Jet Series CL-600-2C10 700/701/702 Bombardier CL-600-2C10/-2D15/- 2D24/-2E25 (GE CF34) Regional Jet Series CL-600-2D15 705 DHC -8-401 DHC-8 Series 400 Bombardier DHC-8-400 (PWC DHC-8-402 PW150) Citation Jet CJ1 525 Cessna 525/525A (Williams FJ 44) Citation Jet CJ2 525A CESSNA AIR- 525B Citation Jet CJ3 Cessna C (Williams FJ 44 ) CRAFT Company 525C Citation Jet CJ4 Cessna C (Williams FJ 44 ) 550 Citation Bravo 560 Citation Encore Cessna 550/560 (PWC PW530/535) 560 Citation Encore + 550 Citation II S550 Citation S/II Cessna 550/560 (PWC JT15D) 560 Citation V 560 Citation Ultra 560XL Citation Excel Cessna 560XL/XLS (PWC PW545) 560 XLS Citation XLS Page 155 of 180 Issue II datedCAR-66 Group -1 Aeroplanes Commercial Desig- 1. TC holder 2 Aeroplanes Model 3 Type Rating Endorsement nation 650 Citation III – VI IV Cessna 650 (Honeywell TFE731) 650 Citation VII Falcon 900EX Falcon 900EX (Honeywell TFE731) Falcon 900EX F900EX EASy Falcon 900EX EASy (Honeywell Falcon 900EX F900DX TFE731) Falcon 900EX F900LX Falcon 2000 Falcon 2000 (CFE 738) Dassault Aviation Falcon 2000EX Falcon 2000EX (PWC PW308) Falcon 2000EX F2000EX EASy Falcon 2000EX EASy (PWC PW308) Falcon 2000EX F2000DX Falcon 2000EX F2000LX Falcon 7X Falcon 7X (PWC PW307A) RUAG Aerospace GmbH 228-200 series Dornier 228 (Honeywell TPE331) (DORNIER) EMB-500 Phenon-100 Embraer EMB-500 ( PWC PW617) Legacy 600 Embraer EMB-135 (RR Corp EMB-135BJ Legacy 650 AE3007A) EMBRAER Embraer ERJ-170 Series (GE CF34) ERJ 170-100 LR ERJ-170 Embraer ERJ-190 Series(GE CF34) ERJ 190-100 /200 ERJ-170 FOKKER SER- F27 Mark 100 Friendship VICES F27 Mark 200 Friendship Fokker F27 / Fairchild F-27/FH-227 F27 Mark 300 Friendship (RRD Dart) F27 Mark 400 Friendship F27 Mark 500 Friendship GULFSTREAM Gulfstream 200 / Gal- Gulfstream (IAI) 200/Galaxy (PWC Galaxy 200 AEROSPACE LP axy PW306) Page 156 of 180 Issue II datedCAR-66 Group -1 Aeroplanes Commercial Desig- 1. TC holder 2 Aeroplanes Model 3 Type Rating Endorsement nation (GALP) c/o Israel Gulfstream G150 Gulfstream (IAI) G150 (Honeywell Aircraft Gulfstream G150 TFE731 Industries BAe 125 Series 700 (Honeywell HS.125 series 700 "Hawker Siddeley" TFE731) Hawker 750 Hawker 750 Hawker 800XP Hawker 800XP BAe 125 Series 750/800XP/850XP/900XP (Honey- Hawker 850XP Hawker 850XP well TFE731) Hawker 900XP Hawker 900XP 300 Super King Air 300LW Super King Air HAWKER Beech 300 Series (PWC PT6) BEECHCRAFT B300 Super King Air 350 Corporation B300C Super King Air 350 C 400 Beechjet Beech 400 / Mitsubishi MU-300 Beechjet (Hawker (PWC JT15) 400A 400XP) 1900 Airliner 1900C Airliner Beech 1900 (PWC PT6) 1900D Airliner 4000 Hawker 4000 Hawker 4000 (PWC PW308) Learjet 45 LJ45 Learjet Model 45 (Honeywell TFE731) Learjet 40 LJ45 Lear Jet Learjet 60 LJ60 Learjet 60 (PWC PW305) LJ60XR 65-90 C90 BEECHCRAFT C90 A Beech 90 Series (PWC PT6) Corporation C90GT BEECHCRAFT C90GTi King Air Corporation B200/ B200C B200 CT Beech 200 Series (PWC PT6) B200GT B200T Page 157 of 180 Issue II datedCAR-66 Group -1 Aeroplanes Commercial Desig- 1. TC holder 2 Aeroplanes Model 3 Type Rating Endorsement nation 390 Premier 1, 1A Beech 390 (Williams FJ44) 99/99A/100 King Air Beech 99/100 Series (PWC PT6) P180 Avanti PIAGGIO Aero P180 Avanti II Piaggio P180 Avanti/Avanti II (PWC Industries PT6) PILATUS AIR- PC-12 Pilatus PC-12 (PWC PT6) CRAFT DHC-6-1 Twin Otter DHC-6-100/110 VIKING AIR (Bombardier) DHC-6-200/210 (De Havilland) De Havilland DHC-6 (PWC PT6) DHC-6-300/310/320 DHC-6-400 Page 158 of 180 Issue II datedCAR-66 Group 1 Helicopter 1 TC Holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation AGUSTA Westland A109E Agusta A109 Series (PWC PW206/207) A109S AW109SP AW /109 N A109 Agusta A109 Series (RR Corp 250) A109A 109 C AW139 Agusta AW139 (PWC PT6) BELL HELICOPTER 212 Bell 212 / Agusta AB212 (PWC TEXTRON PT6) 412 Bell 412 / Agusta AB412 (PWC PT6) 412EP 412CF BELL HELICOPTER 427 Bell 427 (PWC PW207D) CANADA 222 Bell 222 (Honeywell LTS 101) 222B 222U 230 230 Execu- Bell 230 (RR Corp 250) tive 230 Utility 230 EMS 429 Bell 429 (PWC PW207D) 430 Bell 430 (RR Corp 250) EUROCOPTER AS 355 E Eurocopter AS 355 (RR Corp AIR BUS HELICOPTERS 250) AS 355 F AS 355 F1 AS 355 F2 Page 159 of 180 Issue II datedCAR-66 Group 1 Helicopter 1 TC Holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation AS 355 N Eurocopter AS 355 (Turbomeca AIR BUS HELICOPTERS Arrius 1) AS 355 NP Contd--- SA 365 N Dauphin Eurocopter SA 365 N (Turbomeca Arriel 1) SA 365 N1 Dauphin Eurocopter SA 365 N1, AS 365 N2 (Turbomeca Arriel 1) AS 365 N2 AS 365 N3 Dauphin Eurocopter AS 365 N3 (Turbomeca Arriel 2C) EC 155 B Eurocopter EC 155 (Turbomeca Arriel 2) EC 155 B1 EC 135 P1 Series Eurocopter EC 135 (PWC PW206) EC 135 P2 Series EUROCOPTER Deutschland GMBH EC 35 P3 Series MBB-BK 117 C2 EC145 Eurocopter MBB-BK 117 C2 (Turbomeca Arriel 1) HINDUSTAN AERO- DHRUV DHRUV NAUTICS Ltd. MD HELICOPTERS, INC. MD900 MD Helicopters MD900 (PWC PW206/207) MI 172 M1 172 - Klimo TV/TB-3-117 MOSCOW HELICOPTERS VM/BM PLANT S-76C S-76C+ Sikorsky S-76C(Turbomeca Arriel 2) S-76C S-76C++ SIKORSKY AIRCRAFT S-76C Sikorsky S-76C(Turbomeca Arriel 1) ` Page 160 of 180 Issue II datedCAR-66 SUBGROUP 2a: SINGLE TURBO-PROPELLER ENGINE AEROPLANES (Other than those in Group 1) TC holder Type rating endorsement CESSNA AIRCRAFT Company Cessna 208 Series (PWC PT6) Pilatus PC-6 Series (PWC PT6) PILATUS AIRCRAFT Pilatus PC-6 Series (Turbomeca Astazou) Pilatus PC-6 Series (Honeywell TPE 331) Page 161 of 180 Issue II datedCAR-66 SUBGROUP 2b: SINGLE TURBINE ENGINE HELICOPTERS (Other than those in Group 1) 1 TC Holder 2 Helicopter Model Commercial 3 Type Rating Endorsement Designation AGUSTA A119 Koala Agusta A119/ (PWC PT6) AW 119 MK II BELL HELICOPTER CANADA 407 Bell 407 (RR Corp 250) AB 206A AGUSTA AB 206B Agusta AB206 / Bell 206 (RR Corp 250) BELL HELICOPTER 206 series from A to L TEXTRON CANADA LIM- ITED THE ENSTROM HELICOP- 480 Enstrom 480 (RR Corp 250) TER CORPORATION 480B EUROCOPTER AS 350 Ecureuil Eurocopter AS 350 (Turbomeca Arriel 1) AS 350 B1 AIRBUS HELICOP- AS 350 B2 TERS AS 350 BA AS 350 BB AS 350 B3 Eurocopter AS 350 (Turbomeca Arriel 2) AS 350 D Eurocopter AS 350 (Honeywell LTS 101) EC 120 B Colibri Eurocopter EC 120 (Turbomeca Arrius 2F) EC 130 B4 Eurocopter EC 130 (Turbomeca Arriel 2B) SA 315 B Lama Eurocopter SA 315B (Turbomeca Artouste) SA 316 B Eurocopter SA 316 B Alouette III (Turbomeca Artouste) 500N MD Helicopters 500N N/ MD HELICOPTERS INC. (MDHI) MD 600N AMD500N (RR Corp 250) ROBINSON HELICOPTER R 66 Robinson R66 (RR Corps 250 ) 269 D SCHEIZER AIRCRAFT CORP Scgeizer 269 D ( RR Corp 250 ) Page 162 of 180 Issue II datedCAR-66 SUBGROUP 2C: SINGLE PISTON ENGINE HELICOPTERS (Other than those in Group 1) 1 TC Holder 2 Helicopter Model Commercial 3 Type rating endorsement Designation THE ENSTROM HELICOP- F-28 series Enstrom F-28 (Lycoming) TER CORPORATION SEI (BREDA-NARDI) NH 300C Model 300C Schweizer / Breda Nardi (Hughes) 269/300 (Lycoming) 269A 269B SCHWEIZER AIRCRAFT CORPORATION 269C R 22 ROBINSON HELICOPTER Robinson R22 / R44 Series (Ly- COMPANY R 44 coming) Page 163 of 180 Issue II datedCAR-66 GROUP – 3 PISTON ENGINE AEROPLANE ( Other than in Group – 1 ) TC holder Type rating endorsement Type of struc- Maximum Take off Mass ture 2 T and Above 2 T Below AEROSTAR AIRCRAFT Piper PA-60/61 Series (Ly- Metal X Corporation coming) CESSNA AIRCRAFT Com- Cessna 310/320 Series (Con- Metal X pany/ REIMS AVIATION tinental) Cessna 336 (Continental) Metal X Cessna 421 (Continental) Composite X Cessna T303 (Continental) Metal X Beech 55 Series (Continental) Metal X Beech 58 Series (Continental) Metal X Beech 58P (Continental) Metal + Pres- X surised Beech 65-80 Series (Ly- Metal X coming) Beech 76 (Lycoming) Metal X Beech 95 Series (Lycoming) Metal X Piper PA-30 Series (Ly- coming) Composite X Piper PA-31 Series (Ly- X coming) Composite Piper PA-31P (Lycoming) Metal + Pres- X Piper Aircraft surised Piper PA-34 Series (Ly- Metal X coming) Piper PA-34 Series (Continen- Metal X tal) VULCANAIR Vulcanair P.68 Series (Ly- Metal X coming) Cessna/Reims-Cessna Metal X 150/F150 Series (Continen- tal) Cessna/Reims-Cessna Metal X 152/F152 Series (Lycoming) Cessna/Reims-Cessna Metal X 172/F172 Series (Lycoming) Cessna/Reims-Cessna Metal X 172/F172 Series (Continen- tal) Cessna 172 Series (Thielert) Metal X Cessna 175 Series (Lycoming) Metal X Page 164 of 180 Issue II datedCAR-66 GROUP – 3 PITON ENGINE AEROPLANE ( Other than in Group – 1 ) TC holder Type rating endorsement Type of struc- Maximum Take off Mass ture 2 T and Above 2 T Below Cessna 175 Series (Conti- Metal X nental) Cessna 177 Series (Ly- Metal X coming) Cessna 180 Series (Conti- Metal X nental) Cessna/Reims-Cessna Metal X 182/F182 Series (Lycoming) Cessna/Reims-Cessna Metal X 182/F182 Series (Continen- tal) Cessna/Reims-Cessna Metal X 182/F182 Series (SMA) Cessna 185 Series (Conti- Metal X nental) Cessna 206 Series (Conti- Metal X nental) Cessna 206 Series (Ly- Metal X coming) HAWKER BEECHCRAFT Beech 35 Series (Continen- Metal X Corporation tal) Beech 36 Series (Continen- Metal X tal) LAVIA Argentina S.A Piper PA-25 Series (Ly- Metal X (Laviasa) coming) PILATUS AIRCRAFT Pilatus PC-6 Series (Ly- Metal X coming) PIPER AIRCRAFT Piper PA-24 Series (Ly- Metal X coming) Piper PA-28 Series (Ly- Metal X coming) Piper PA-28 Series (Conti- Metal X nental) Piper PA-28 Series (Thielert) Metal X Piper PA-32 Series (Ly- Metal X coming) Piper PA-36 Series (Ly- Metal X coming) Piper PA-36 Series (Conti- Metal X nental) SKY Int Aviat Husky A (Lycoming) Metal X Zlin Z-143 L (Lycoming) Metal X Zlin Aircraft (Moravan Zlin Z-242 L (Lycoming) Metal X Aviation) Page 165 of 180 Issue II datedCAR-66 GROUP – 3 PITON ENGINE AEROPLANE ( Other than in Group – 1 ) TC holder Type rating endorsement Type of Maximum Take off Mass structure 2 T and Above 2 T Below DIAMOND AIRCRAFT Indus- Diamond DA42 Series (Thielert) tries Composite X Diamond DA42 Series (Austro Engine) Composite X CIRRUS Design Corpora- Cirrus SR20 (Continental) tion Composite X Cirrus SR22 Series (Continen- tal) DIAMOND AIRCRAFT In- Diamond DA40 (Lycoming) dustries Composite X Diamond DA40 D (Thielert) Composite X Diamond DA40 (Austro En- gine) Composite X NATIONAL AEROSPACE Hansa 3 ( Rotax) LABORATORIES Composite X Page 166 of 180 Issue II datedCAR-66 Appendix II to AMC to CAR-66 Aircraft type practical experience and On-the-Job Training list of tasks I Time limits/Maintenance checks VII Placards and Markings a. 100 hour check (general aviation a. Check aircraft for correct plac- aircraft). ards. b. B or C Check check (transport b. Check aircraft for correct mark- ings. category aircraft). VIII Servicing Assist carrying out a scheduled maintenance check i.a.w. AMM. a. Refuel aircraft. Review aircraft maintenance b. Defuel aircraft. log for correct completion Carry out tank to tank fuel c. Review records for compliance transfer. with airworthiness directives. c. Check / adjust tire pressures. d. Review records for compliance d. Check / replenish oil level. with component life limits. e. Check/ replenish hydraulic fluid e. Procedure for Inspection follow- level. ing heavy landing. f. Check/ replenish accumulator pressure. f. Procedure for Inspection follow- g. Charge pneumatic system. ing lightning strike. h. Grease aircraft. II Dimensions/Areas i. Connect ground power. a. Locate component(s) by station number. j. Service toilet/water system b. Perform symmetry check. k. Perform pre-flight/daily check III Lifting and Shoring IX Vibration and Noise Analysis Assist in : a. Analyze helicopter vibration a. Jack aircraft nose or tail wheel. problem. b. Analyze noise spectrum. b. Jack complete aircraft. Analyse engine vibration. c. Sling or trestle major component. X Air Conditioning IV Leveling /Weighing a. Replace combustion heater. a. Level aircraft. Replace flow control valve. b. Weigh aircraft. b. Replace outflow valve. Replace safety valve. c. Prepare weight and balance c. Replace vapour cycle unit. amendment. d. Check aircraft against equipment d. Replace air cycle unit. list. e. Replace cabin blower. V Towing and Taxiing f. Replace heat exchanger. Prepare for aircraft towing g. Replace pressurization controller. a. Tow aircraft. h. Clean outflow valves. b. Be part of aircraft towing team. Deactivate/reactivate cargo VI Parking and mooring isolation valve. a. Tie down aircraft. Deactivate/reactivate avionics ventilation components b. Park, secure and cover aircraft. i. Check operation of air c. Position aircraft in dock. conditioning/heating system d. Secure rotor blades. Page 167 of 180 Issue II datedCAR-66 j. Check operation of pressurization cable. system k. Troubleshoot faulty system k. Troubleshoot faulty system XIV Equipment/Furnishings XI Auto flight a. Replace pets a. Install servos. b. Replace crew seats. b. Rig bridle cables c. Replace passenger seats. c. Replace controller. d. Check inertia reels. d. Replace amplifier. e. Check seats/belts for security. e. Check operation of auto-pilot. f. Check emergency equipment. f. Check operation of auto-throttle. g. Check ELT for compliance with g. Check operation of yaw damper. regulations. h. Check and adjust servo clutch. h. Repair toilet waste container. i. Perform autopilot gain adjust- i. Repair upholstery. ments. j. Change cabin configuration. j. Perform mach trim functional XV Fire protection check. a. Check fire bottle contents. k. Troubleshoot faulty system. b. Check operation of warning sys- l. Check auto land system tem. m. Check flight management systems c. Check cabin fire extinguisher con- n. Check stability augmentation sys- tents. tem d. Check lavatory smoke detector XII Communications system. a. Replace VHF com unit. e. Install new fire bottle. b. Replace HF com unit. f. Replace fire bottle squib. c. Replace existing antenna. g. Troubleshoot faulty system. d. Replace static discharge wicks. h. Inspect engine fire wire detection e. Check operation of radios. systems XVI Flight Controls f. Perform antenna VSWR check. a. Replace horizontal stabilizer. g. Perform Selcal operational check. b. Replace elevator. h. Perform operational check of c. Replace aileron. i. passenger address system. d. Replace rudder. j. Functionally check audio inte- grating system. e. Replace trim tabs. f. Install control cable and fittings. k. Repair co-axial cable. g. Replace flaps. l. Troubleshoot faulty system. h. Replace powered flying control XIII Electrical Power unit a. Charge lead/acid battery. i. Replace flat actuator b. Charge ni-cad battery. j. Adjust trim tab. c. Check battery capacity. k. Adjust control cable tension. d. Deep-cycle ni-cad battery. l. Check control range and sense of e. Replace generator/alternator. movement. f. Replace switches. m. Check for correct assembly and locking. g. Replace circuit breakers. n. Troubleshoot faulty system. h. Adjust voltage regulator. XVII Fuel i. Amend electrical load analysis a. Replace booster pump. report. j. Repair/replace electrical feeder b. Replace fuel selector. Page 168 of 180 Issue II datedCAR-66 c. Replace fuel tank cells. m. Adjust micro switches. d. Check filters. n. Charge struts. e. Flow check system. o. Troubleshoot faulty system. f. Check calibration of fuel quantity p. Test out brake system gauges. XXII Lights g. Check operation feed/selectors a. Repair/replace rotating beacon. h. Troubleshoot faulty system. b. Repair/replace landing lights. XVIII Hydraulics c. Repair/replace navigation lights. a. Replace engine driven pump. d. Repair/replace interior lights. b. Replace standby pump. e. Repair/replace emergency light- c. Replace accumulator. ing system. d. Check operation of shut off valve. f. Perform emergency lighting sys- e. Check filters. tem checks. f. Check indicating systems. g. Troubleshoot faulty system g. Perform functional checks. XXIII Navigation h. Troubleshoot faulty system. a. Calibrate magnetic direction indi- XIX Ice and rain protection cator. a. Replace pump. b. Replace airspeed indicator. b. Replace timer. c. Replace altimeter. c. Install wiper motor. d. Replace air data computer. d. Check operation of systems. e. Replace VOR unit. e. Troubleshoot faulty system. f. Replace ADI. XX Indicating/recording systems g. Replace HSI. a. Replace flight data recorder. h. Check pitot static system for b. Replace cockpit voice recorder. leaks. i. Check operation of directional c. Replace clock. gyro. d. Replace master caution unit. j. Functional check weather radar. e. Replace FDR. k. Functional check Doppler. f. Perform FDR data retrieval. l. Functional check TCAS. g. Troubleshoot faulty system. m. Functional check DME h. Implement ESDS procedures n. Functional check ATC Tran- i. Inspect for HIRF requirements sponder XXI Landing Gear o. Functional check flight director system. a. Build up wheel. p. Functional check inertial nav sys- b. Replace main wheel. tem. c. Replace nose wheel. q. Complete quadrantal error cor- d. Replace shimmy damper. rection of ADF system. e. Rig nose wheel steering. r. Update flight management sys- tem database. f. Replace shock strut seals. s. Check calibration of pitot static g. Replace brake unit. instruments. h. Replace brake control valve. t. Check calibration of pressure alti- i. Bleed brakes. tude reporting system. j. Test anti skid unit. u. Troubleshoot faulty system k. Test gear retraction. v. Check marker systems l. Change bungees. w. Compass replacement di- rect/indirect Page 169 of 180 Issue II datedCAR-66 x. Check Satcom b. Treat corrosion. y. Check GPS c. Apply protective treatment. z. Test AVM XXXI Doors XXIV Oxygen a. Rig/adjust locking mechanism. a. Inspect on board oxygen equip- b. Adjust air stair system. ment. c. Check operation of emergency b. Purge and recharge oxygen sys- exits. tem. d. Test door warning system. c. Replace regulator. e. Troubleshoot faulty system. d. Replace oxygen generator. XXXII Windows e. Test crew oxygen system. a. Replace windshield. f. Perform auto oxygen system de- b. Replace window. ployment check. c. Repair transparency. g. Troubleshoot faulty system. XXXIII Wings XXV Pneumatic systems d. Skin repair. a. Replace filter. e. Recover fabric wing. b. Replace compressor. f. Replace tip. c. Recharge desiccators. g. Replace rib. d. Adjust regulator. h. Check incidence/rig. e. Check for leaks. XXXIV Propeller f. Troubleshoot faulty system. a. Assemble prop after transporta- XXVI Vacuum systems tion. a. Replace vacuum pump. b. Replace propeller. b. Check/replace filters. c. Replace governor. c. Adjust regulator. d. Adjust governor. d. Troubleshoot faulty system. e. Perform static functional checks. XXVII Water/Waste f. Check operation during ground a. Replace water pump. run. g. Check track. b. Replace tap. h. Check setting of micro switches. c. Replace toilet pump. i. Dress out blade damage. d. Troubleshoot faulty system. j. Dynamically balance prop. XXVIII Central Maintenance System k. Troubleshoot faulty system. a. Retrieve data from CMU. XXXV Main Rotors b. Replace CMU. a. Install rotor assembly. c. Perform Bite check. b. Replace blades. d. Troubleshoot faulty system. c. Replace damper assembly. XXIX Airborne Auxiliary power d. Check track. a. Install APU. e. Check static balance. b. Inspect hot section. f. Check dynamic balance. c. Troubleshoot faulty system. g. Troubleshoot. XXX Structures XXXVI Rotor Drive a. Sheet metal repair. a. Replace mast. b. Fibre glass repair. b. Replace drive coupling. c. Wooden repair. c. Replace clutch/freewheel unit XXXI Fabric repair. d. Replace drive belt. a. Recover fabric control surface. Page 170 of 180 Issue II datedCAR-66 e. Install main gearbox. c. Engine ground run. f. Overhaul main gearbox. d. Establish reference power. g. Check gearbox chip detectors. e. Trend monitoring/gas path anal- XXXVII Tail Rotors ysis. f. Troubleshoot. a. Install rotor assembly. XLIII Fuel and control, piston b. Replace blades. a. Replace engine driven pump. c. Troubleshoot. b. Adjust AMC. XXXVIII Tail Rotor Drive c. Adjust ABC. a. Replace bevel gearbox. d. Install carburetor/injector. b. Replace universal joints. e. Adjust carburetor/injector. c. Overhaul bevel gearbox. f. Clean injector nozzles. d. Install drive assembly. g. Replace primer line. e. Check chip detectors. h. Check carburetor float setting. XXXIX Rotorcraft flight controls i. Troubleshoot faulty system. a. Install swash plate. XLIV Fuel and control, turbine b. Install mixing box. a. Replace FCU. c. Adjust pitch links. b. Replace engine driven pump. d. Rig collective system. c. Clean/test fuel nozzles. e. Rig cyclic system. d. Clean/replace filters. f. Rig anti-torque system. e. Adjust FCU. g. Check controls for assembly and f. Troubleshoot faulty system. locking. XLV Ignition systems, piston h. Check controls for operation and sense. a. Change magneto. i. Troubleshoot faulty system. b. Change ignition vibrator. XL Power Plant c. Change plugs. a. Build up ECU. d. Test plugs. b. Replace engine. e. Check H.T. leads. c. Repair cooling baffles. f. Install new leads. g. Check timing. d. Repair cowling. h. Check system bonding. e. Adjust cowl flaps. i. Troubleshoot faulty system. f. Repair faulty wiring. XLVI Ignition systems, turbine g. Troubleshoot. a. Check glow plugs/ ignitors. XLI Piston Engines b. Check H.T. leads. a. Remove/install reduction gear. c. Check ignition unit. b. Check crankshaft run-out. d. Replace ignition unit. c. Check tappet clearance. e. Troubleshoot faulty system. d. Check compression. XLVII Engine Controls e. Extract broken stud. a. Rig thrust lever. f. Install helicoil. b. Rig RPM control. g. Perform ground run. c. Rig mixture HP cock lever. h. Establish/check reference RPM. d. Rig power lever. i. Troubleshoot. e. Check control sync (multi-eng). XLII Turbine Engines f. Check controls for correct as- a. Replace module. sembly and locking. b. Hot section inspection. g. Check controls for range and Page 171 of 180 Issue II datedCAR-66 sense of operation. e. Troubleshoot faulty system h. Adjust pedestal micro-switches. LV Accessory gear boxes i. Troubleshoot faulty system. a. Replace gearbox. XLVIII Engine Indicating b. Replace drive shaft. a. Replace engine instruments(s). c. Check Chip detector b. Replace oil temperature bulb. c. Replace thermocouples. d. Check calibration. e. Troubleshoot faulty system. XLIX Exhaust, piston a. Replace exhaust gasket. b. Inspect welded repair. c. Pressure check cabin heater muff. d. Troubleshoot faulty system. L Exhaust, turbine a. Change jet pipe. b. Change shroud assembly. c. Install trimmers. LI Oil a. Change oil. b. Check filter(s). c. Adjust pressure relief valve. d. Replace oil tank. e. Replace oil pump. f. Replace oil cooler. g. Replace firewall shut off valve. h. Perform oil dilution. i. Troubleshoot faulty system. LII Starting a. Replace starter. b. Replace start relay. c. Replace start control valve. d. Check cranking speed. e. Troubleshoot faulty system. LIII Turbines, piston engines a. Replace PRT. b. Replace turbo-blower. c. Replace heat shields. d. Replace waste gate. e. Adjust density controller. LIV Engine water injection a. Replace water/methanol pump. b. Flow check water/methanol sys- tem. c. Adjust water/methanol control unit. d. Check fluid for quality. Page 172 of 180 Issue II datedAPPENDIX III to AMC of CAR-66 Evaluation of the competence: assessment and assessors This Appendix applies to the competence assessment performed by the designated as- sessors (and their qualifications). 1) What does “competence” mean and areas of focus for assessment The assessment should aim at measuring the competence by evaluating three major fac- tors associated to the learning objectives: (cid:183) Knowledge; (cid:183) Skills; (cid:183) Attitude. Generally, knowledge is evaluated by examination. The purpose of this document is not to describe the examination process: this material mainly addresses the evaluation of “skills” and “attitude” after training containing practical elements. Nevertheless, the trainee needs to demonstrate sufficient knowledge to perform the required tasks. “Attitude” is indivisible from the “skill” as this greatly contributes to the safe perfor- mance of the tasks. The evaluation of the competence should be based on the learning objectives of the training, in particular: (cid:183) the (observable) desired performance. This covers what the trainee is expected to be able to do and how the trainee is expected to behave at the end of the train- ing; (cid:183) the (measurable) performance standard that must be attained to confirm the trainee’s level of competence in the form of tolerances, constraints, limits, per- formance rates or qualitative statements; and (cid:183) the conditions under which the trainee will demonstrate competence. Condi- tions consist of the training methods, the environmental, situational and regula- tory factors. The assessment should focus on the competencies relevant to the aircraft type and its maintenance including, but not limited to: (cid:183) Environmental awareness (act safely, apply safety precautions and prevent dan- gerous situations); (cid:183) Systems integration (demonstrate understanding of aircraft systems interaction, identify, describe, explain, plan, execute); 173(cid:183) Knowledge and understanding of areas requiring special emphasis or novelty (areas peculiar to the aircraft type, domains not covered by CAR 66 Appendix I, practical training elements that cannot be imparted through simulation devices, etc.); (cid:183) Using reports and indications (the ability to read and interpret); (cid:183) Aircraft documentation finding and handling (identify the appropriate aircraft documentation, navigate, execute and obey the prescribed maintenance proce dures); (cid:183) Perform maintenance actions (demonstrate safe handling of aircraft, engines, components and tools); (cid:183) Aircraft final/close-up and report (apply close up, initiate appropriate actions /follow-up/ records of testing, establish and sign maintenance reords /logbooks). 2) How to assess As far as feasible, the objectives of the assessment should be associated with the learn- ing objectives and the passing level; it means that observable criteria should be set to measure the performance and should remain as objective as possible. The general characteristics of effective assessment are: objective, flexible, acceptable, comprehensive, constructive, organised and thoughtful. At the conclusion, the trainee should have no doubt about what he/she did well, what he/she did poorly and how he/she can improve. The following is a non-exhaustive list of questions that may be posed to assist the as- sessment: (cid:183) What are the success factors for the job? (cid:183) What are typical characteristics of a correct behaviour for the task? (cid:183) What criteria should be observed? (cid:183) What level of expertise is expected? (cid:183) Is there any standard available? (cid:183) What is the pass mark? For example: o “Go-no go” situation; o How to allocate points? Minimum amount to succeed; o “Must know or execute” versus “Good to know or execute” versus “Don’t expect the candidate to be an expert”. (cid:183) Minimum or maximum time to achieve? Use time effectively and efficiently. (cid:183) What if the trainee fails? How many times is the trainee allowed to fail? (cid:183) When and how should the trainee be prepared for the assessment? (cid:183) What proportion of judgment by the instructor out of collaboration with the trainee is needed during the evaluation stage? The assessment may be: 174(cid:183) diagnostic (prior to a course), formative (reorientate the course on areas where there is a need to reinforce) or summative (partial or final evaluation); (cid:183) performed task-by-task, as a group of tasks or as a final assessment. One method might be an initial assessment to be performed by the trainee himself /herself, then discussing areas where the perceptions of the trainee’s performance by the assessors differ in order to: (cid:183) develop the self develop the self-assessment habits; (cid:183) make the assessment more acceptable and understandable to both parties. A “box-ticking” exercise would be pointless. Experience has shown that assessment sheets have largely evolved over time into assessment of groups of “skills” because in practice such things eventually detracted from the training and assessment that it was intended to serve: evaluate at a point of time, encourage and orientate the training needs, improve safety and ultimately qualify people for their duties. In addition, many other aspects should be appropriately considered during the assess- ment process such as stress and environmental conditions, difficulty of the test, history of evaluation (such as tangible progresses or sudden and unexpected poor performance made by the trainee), amount of time necessary to build competence, etc. All these reasons place more emphasis on the assessor and highlight the function of the organisation’s approval. 3) Who should assess In order to qualify, the assessor should: (cid:183) Be proficient and have sufficient experience or knowledge in: o human performance and safety culture; o the aircraft type (necessary to have the certifying staff privileges in case of CRS issuances); o training/coaching/testing skills; o instructional tools to use; (cid:183) Understand the objective and the content of the practical elements of the train- ing that is being assessed; (cid:183) Have interpersonal skills to manage the assessment process (professionalism, sincerity objectivity and neutrality, analysis skills, sense of judgement, flexibility, capability of evaluating the supervisor’s or instructor’s reports, handling of trainee’s reactions to failing assessment with the cultural environment, being constructive, etc.); (cid:183) Be ultimately designated by the organisation to carry out the assessment. 175The roles may be combined for: (cid:183) the assessor and the instructor for the practical elements of the Type Rating Training; or (cid:183) the assessor and the supervisor for the On-the-Job Training Provided that the objectives associated with each role are clearly understood and that thecompetence and qualification criteria according to the company’s procedures are met for bothfunctions. Whenever possible (depending on the size of the organisation), it is recommended to split the roles (two different persons) in order to avoid any conflicts of interests. When the functions are not combined, the role of each function should be clearly under- stood 176Appendix IV to AMC of CAR- 66. A. 45(d) Fuel Tank Safety training This appendix includes general instructions for providing training on Fuel Tank Safety issues. 1. Level of training required by this Annex is only level 2. Level 2 Detailed training Objectives: The attendant should, after the completion of the training: 1. know the history and the theoretical and practical elements of the subject, have an overview of Special Federal Aviation Regulations (SFARs) from 14 CFR SFAR 88 of the FAA and of JAA TGL 47, be able to give a detailed description of the concept of CDCCL, Airworthiness Limitations Items (ALI) and using theoretical fundamentals and specific examples, 2. have the capacity to combine and apply the separate elements of knowledge in a log- ical and comprehensive manner. 3. have detailed information on how the above items affect the aircraft in the scope of the activity of the organisation or in the fleet. 4. understand and carry out activities with the use of manufacturer and regulatory au- thority data providing instructions on design and maintenance, such as Service Bul- letins, Airworthiness Directives, Aircraft Maintenance Manual, Component Mainte- nance Manual etc. 5. use easily the manufacturer’s documentation from various sources and apply cor- rective action where appropriate. 6. identify the components or parts or the aircraft subject to FTS from the manufactur- er’s documentation, plan the action or apply a Service Bulletin and an Airworthiness Directive. Continuing training The interval between continuing training shall be established by the organisation em- ploying such personnel, but should not exceed two years. The continuing training shall include knowledge on evolution of material, tools, documentation and manufacturer’s or DGCA directives. 2. The personnel directly involved in Fuel Tank Safety (FTS) systems shall be qualified according to the following table: 177Level of Continuing Organisation Personnel knowledge training CAR-66 licence holders in a The airworthiness continuing airworthiness review staff as re- 2 Yes management organisation quired by M.A.707. CAR-66 licence holders in Maintenance organi- aircraft and component sation support and 2 Yes maintenance organisations certifying staff 3. General requirements The training for the personnel designated in table above has to be carried out before any airworthiness review certificate is issued or any maintenance task is certified on an aircraft or a component. The training should be made in appropriate facilities containing examples of compo- nents, systems and parts affected by FTS issues and having access to aircraft or compo- nent where typical examples of FTS issues can be shown. The use of pictures, films and practical examples of the maintenance on fuel tank system is recommended. The train- ing shall include a representative number of repair and inspections as required by the maintenance programme showing the necessity of using the manufacturer’s data. 4. Characteristics of the training The following characteristics shall be taken into consideration when the level 2 training programme are being established: (a) understanding of the background and concepts of fuel tank safety as developed dur- ing the last 10 years, and (b) how in maintenance organisations mechanics can recognize, interpret and handle the improvements that have been made or are being made during fuel tank system maintenance, (c) awareness of any hazards working on the Fuel System, and especially with a Flam- mability Reduction System using nitrogen. a), b) and c) should be introduced in the training programme addressing the following issues: i) The theoretical background behind the fuel tank safety: the explosions of mixtures of fuel and air, the behavior of those mixtures in an aviation environment, the ef- fects of temperature and pressure, energy needed for ignition etc, the ‘fire triangle’, - Explain 2 concepts to prevent explosions: (1) ignition source prevention and (2) flammability reduction, ii) The major accidents and accident investigations and their conclusions, 178iii) SFARs from 14 CFR SFAR 88 of the FAA and JAA Internal Policy INT POL 25/12: reason of these documents, and what was the ultimate goal, margins of fuel system safety improvements (from 10-6 to 10-9, in fact improvement by a factor 100- 1000, to identify unsafe conditions and to correct them, to systematically improve fuel tank maintenance), iv) Explain the concepts that are being used: the results of SFAR 88 of the FAA and JAA INT/POL 25/12: modifications, airworthiness limitations and CDCCL, v) Where relevant information can be found by the mechanics and how to use and in- terpret this information (maintenance manuals, component maintenance manuals) vi) Fuel Tank Safety and Maintenance: fuel tank entry and exit procedures, clean work- ing environment, what is meant by configuration control, wire separation, bonding of components etc, vii) Flammability reduction systems: reason for their presence, their effects, the haz- ards of an FRS using nitrogen for maintenance, safety precautions in mainte- nance/working with an FRS, viii) Recording maintenance actions, recording measures and results of inspections. 179DGCA application forms for licenses and examinations Form No Description Application For Initial Issue Of CAR- 66 Aircraft Maintenance Engineer’s CA Form 19-01 Licence CA Form 19-02 Application for extension of CAR- 66 aircraft maintenance engineer’s li- cence CA Form 19-03 Application for renewal of CAR- 66 aircraft maintenance engineer’s licence CA Form 19-04 Application for conversion/removal of limitations of CAR- 66 aircraft maintenance engineer’s licence CA Form 19-05 Application for issue of duplicate CAR- 66 aircraft maintenance engineer’s licence CA Form 19-06 Medical certificate CA Form 19-07 Application for allotment of computer number for appearing in AME li- cence examinations CA Form 19-08A Application for appearing in written paper(s) of CAR 66 basic knowledge examination CA Form 19-08B Application for appearing in CAR 66 type examination CA Form 19-09 Application for appearing in skill test of CAR-66 AME licence CA Form 19-10 Format of aircraft maintenance engineer work record / log book CA Form 19-11 Application for issue of basic knowledge examination certificate ********* 180

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