Drafted by G T SELVAN Draft CAR-66 dated 7th March 2011Government of India Directorate General of Civil Aviation New Delhi – 110 003 Ref file No. : 11-690/CAR-66/2011 Dated the 7th March 2011 Notice Inviting Comments of the Public on Proposed draft CAR 66 The Civil Aviation Requirements on Aircraft Maintenance Engineer (AME) licencing system hitherto followed is required to be changed subsequent to the publication of amended Rule 61* in “The Gazette of India”, Ministry of Civil Aviation, New Delhi, dated the 22nd December 2010. In order to implement the said Aircraft Rule, Civil Aviation Requirements-66 (CAR-66) and associated Acceptable means of compliance & Guidance material had been drafted to detail the proposed Aircraft Maintenance Engineers Licencing system. General public, personnel from Industry and Regulatory bodies may offer their comments and suggestions on the draft CAR 66 with a view to effectively implement the Rule 61 and efficiently administer the AME Licencing system. The comments and suggestions may be provided on the attached format either in Microsoft Word or Excel document form and mailed to
[email protected] and
[email protected] as attachment with the mail subject annotate “Draft CAR 66 Comments” Cutoff date for receipt of the comments is 30 days from the publication the draft CAR 66 on the DGCA website. Charan Dass Joint Director General of Civil Aviation for the Director General of Civil Aviation * “the Aircraft (6th Amendment) Rules Page 1 of 175 Drafted by G T SELVAN Draft CAR-66 dated 7th March 2011 Salient Features of the CAR-66 The CAR-66 has been drafted in line with the current Rule 61 and to harmonize the aircraft maintenance personnel licencing system with EASA Part 66 [General] details, requirements for qualifying an individual to obtain an Aircraft Maintenance Engineer’s Licence and extension of such licence [CAR-66] eliminates the system of obtaining Airframe and Engine Licences & Electrical, Instrument and Radio System Licences separately [66.A.01] provides for taking theoretical examinations while the individual is still in the process of acquiring the required practical experience [66.A.30] redefines the syllabus for basic knowledge examination in modular pattern [66.A.25] provides for qualifying under the existing system of obtaining the licence till December 2012 [66.A.70] provides for acquiring group type rating of aircraft and certification privileges 66.A.45 (g) has a provision to convert the existing AME licence to CAR 66 licence [66.A.70] with or without limitation lists the details of practical tasks to qualify an individual to obtain a type rating [Addendum II to AMC] details clauses under which a licence may be revoked or suspended or withheld [66.A.95] provides for endorsement of an AME licence after successful completion of type training and the type training examination shall consist of both theoretical and practical examinations [66.A.45 (c)] Page 2 of 175 Drafted by G T SELVAN Draft CAR-66 dated 7th March 2011 Public Comment / Response Document on the proposed CAR-66: Organization’s / Individual’s detail & email for communication Draft Page & Paragraph Number Draft Paragraph Reference with text (Reproduce the Contents) (if possible specify the Aircraft Rules that supports your view / comment or the drafted requirement contradicts) Organization’s / Individual’s Comments or Concern (if possible specify the Aircraft Rules that supports your proposal) How the draft should be modified. Note: It is not mandatory to fill-up the last column Page 3 of 175 NEW DELHI Page 4 of 175 .66 LICENCESING OF AIRCRAFT MAINTENANCE ENGINEERS DIRECTORATE GENERAL OF CIVIL AVIATION TECHNICAL CENTRE. OPP SAFDURJUNG AIRPORT.by G T SELVAN Draft CAR-66 Dated 7th March 2011 CIVIL AVIATION REQUIREMENTS CAR . 01 GENERAL In order to harmonize Indian requirements for licensing of aircraft maintenance engineer’s with international requirements. New. authorization.0 dated _______ April 2011. The requirements are followed by Acceptable means of compliance (AMC) and Guidance Material (GM) The CAR-66 is applicable to all personnel / Organizations engaged in maintenance and /or certification of aircraft registered in India with immediate effect. It also has a provision for converting the Aircraft Maintenance Engineer’s Licence issued prior to the CAR-66 coming into force. This CAR is issued pursuant to Rule 61 and under the provisions of Rule 133A of the Aircraft Rules. amended and corrected text will be indicated by vertical bars on the left margin Page 5 of 175 .by G T SELVAN Draft CAR-66 Dated 7th March 2011 66. Explanatory notes not forming part of the requirements appear in smaller typeface. each page being identified by the date of issue or the change number under which it is amended or reissued. CAR-66 Rev. which is primarily based on EASA Part 66 regulation is being introduced. approval. certificate of competency and conditions of its validity and use. 1937. The Section A of CAR-66 establishes the requirements for the issue and extension of an aircraft maintenance engineer’s licence. The requirements of CAR-66 are presented in a single column on loose pages. Issue I (Revision 0) Page 6 of 175 .by G T SELVAN Draft CAR-66 Dated 7th March 2011 Record of Revisions Initial . 95 REQUIREMENTS AIRCRAFT MAINTENANCE ENGINEER’S LICENCE AEROPLANES AND HELICOPTERS 11 Scope Application Eligibility Privileges Basic knowledge requirements Experience Requirements Continued validity of the aircraft maintenance engineer’s licence Type / task training and ratings Evidence of qualification Conversion provisions Duplicate Licence Approvals Authorization Certificate of Competency Cancellation.A.A.A.A.30 66.71 66.A.by G T SELVAN Draft CAR-66 Dated 7th March 2011 CONTENTS Cover Page Paragraph 66. authorisation and certificate of competency 11 12 12 13 13 15 15 17 17 18 18 18 19 19 Page 7 of 175 .A.A.55 66.A.10 66.40 66. suspension or limitation of the aircraft maintenance engineer’s license.85 66.A.A.A.A.20 66.80 66.A.15 66.75 66.70 66.A.25 66.45 66.01 66.A. approval.01 Description General Record of Revisions Page No 05 06 SECTION A SUBPART A 66. 1937 (CAR-66) . A.CA Form 26 Conversion of AME licences Issued Prior to CAR-66 Coming into Force Requirements and Procedures for Grant of Approvals Requirements and Procedures for Grant of Authorisations Requirements and Procedures for Grant of Certificate of Competency 22 25 69 75 83 84 116 121 131 132 133 Appendix VII Appendix VIII Appendix IX Appendix X Page 8 of 175 .200 SUBPART D 66. A.300 SUBPART E 66.by G T SELVAN Draft CAR-66 Dated 7th March 2011 SUBPART B 66. A. A.400 AIRCRAFT OTHER THAN AEROPLANES AND HELICOPTERS General COMPONENTS General Authorization General Certificate of Competency General 21 21 21 21 Appendices Appendix I Basic Knowledge Requirements Modules and Syllabus Appendix II Appendix III Appendix IV Appendix V Appendix VI Examination and Standard Type training and Examination Standard Experience requirements for extending a CAR-66 Aircraft Maintenance Engineer’s Licence Applications and Formats Aircraft Maintenance Engineer’s Licence referred to in Rule 61 of the Aircraft Rules.100 SUBPART C 66. A.45(d) AMC 66.A.A.A.45(h) AMC 66.A.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Acceptable Means of Compliance (AMC) to Section A of CAR 66 AMC 66.71 Addendum I to AMC Addendum II to AMC Addendum III to AMC Addendum IV to AMC Fuel Tank Safety training Application Privileges Privileges Basic knowledge requirements Experience requirements Experience requirements Continued validity of AME Licence Type/task training and ratings Type/task training and ratings Type/task training and ratings Type/task training and ratings Conversion provisions Duplicate Licence Group rating Practical Exercises Reserved 134 134 135 138 138 138 138 140 140 142 142 143 143 144 160 166 167 Page 9 of 175 .45(g) AMC 66.30(d) AMC 66.A.A.A.A.25 AMC 66.A.30(a) AMC 6.70 AMC 66.45(a) AMC 66.A.20(a) AMC 66.40 AMC 66.10 AMC 66.A.20(b)2 AMC 66.A. 30(a) GM 66.20(a)2 Privileges GM 66.A.45(d) GM 66.A.70 Basic knowledge requirements Basic knowledge requirements Type/task training and ratings Type/task training and ratings Type/task training and ratings Conversion provisions Page 10 of 175 .10 Application 170 171 171 171 172 173 173 174 174 174 GM 66.45(f) GM 66.A.A.45(d) GM 66.A.A.A.20(a)1 Privileges GM 66.25(a) GM 66.A.A.A.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Guidance Material to SECTION A of – CAR 66 GM 66.20(b)3 Privileges GM 66. Reserved.A4 and B1.Category C (b) Categories A and B1 are subdivided into subcategories relative to combinations of aeroplanes. Reserved Reserved Page 11 of 175 b) c) d) e) . helicopters.Category A . turbine and piston engines.10 (a) as appropriate. In addition to the documents required in points 66.4 Helicopter Piston 66. The subcategories are: .Category B1 .A. extension of an aircraft maintenance engineer’s licence and conditions of its validity and use for aeroplanes and helicopters of the following categories: .Category B2 . A.2 Aeroplane Piston .A3 and B1.A2 and B1. the applicant for additional categories or sub-categories to an aircraft maintenance engineer’s licence shall submit his/her current original aircraft maintenance engineer’s licence to the DGCA together with CA Form 19-02.by G T SELVAN Draft CAR-66 Dated 7th March 2011 SECTION A Requirements 66.10.A1 and B1. A. Application a) An application for issue of an aircraft maintenance engineer’s licence and extension to such licence shall be made on CA Form 19-01/02 with necessary documents and fees to the DGCA.1 Aeroplane Turbine .3 Helicopter Turbine .01 Scope (a) This section establishes the requirements for the issue. Category B1 aircraft maintenance engineer’s licence shall permit the holder to issue certificates of release to service following maintenance. including aircraft structure. A.20(b). Page 12 of 175 2.20 Privileges a) 1. 4. 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 of aircraft type endorsed on the licence. Category C aircraft maintenance engineer’s licence shall permit the holder to issue certificates of release to service following base maintenance in respect of an aircraft type endorsed on the licence.Eligibility An applicant for an aircraft maintenance engineer’s licence shall be at least 18 years of age. 3. Subject to the compliance with paragraph 66.A. power plant. Category B1 shall automatically include the appropriate subcategory of Category A. The privileges apply to the aircraft in its entirety including all system.by G T SELVAN Draft CAR-66 Dated 7th March 2011 f) the applicant shall have demonstrated to the DGCA or any other person authorized by him on his behalf. 66. The certification privileges shall be restricted to the work carried out by the licence holder himself. the ability to exercise the privileges of the category and subcategory of the licence for which the application has been made. The certification privileges shall be exercised only if the holder of Category A licence on a specific aircraft type has satisfactorily completed and demonstrated the relevant category A aircraft type task training conducted by an approved maintenance or AME training organisation approved for the purpose. requiring simple tests to prove their serviceability in respect of an aircraft type endorsed on the licence. 66. A. b) 1. mechanical and electrical systems including replacement of avionic line replaceable units.15. The certification privileges shall be restricted to the work carried out by the licence holder himself. . the following privileges shall apply: Category A aircraft maintenance engineer’s licence permits the holder to issue certificates of release to service following minor scheduled line maintenance and simple defect rectification within the limits of tasks specifically endorsed on the authorization issued by an organisation approved under rule 133B for the type of aircraft endorsed on the licence. 5. B2 or C licence after satisfactory completion of an examination in the relevant category B1.A. the licence is endorsed with the appropriate aircraft type rating in case of category B1. An applicant for an aircraft maintenance engineer’s licence or extension of a category or subcategory to such an aircraft maintenance engineer’s licence shall demonstrate by examination. namely:for category A (any sub-category) and category B1 (sub categories B1.25 Basic Knowledge requirements: a) b) The applicant must have passed 10+2 examination in Physics. DGCA on form CA 19-08 c) d) 66.30 Experience requirements: a) An applicant for an aircraft maintenance engineer’s licence. Categories A. Such credits in respect of ‘type rated AME licences issued and basic knowledge examinations Paper I. Chemistry and Mathematics from a recognized board or university or its equivalent. remain compliant with such other conditions attached to the licence. II & III’ passed prior to the CAR-66 coming into force shall be established in accordance with Appendix VII of this CAR Candidates desirous of appearing in the basic knowledge examination shall apply to the CEO. 66. a level of knowledge in the appropriate subject modules in accordance with the requirements specified in Appendix I to this CAR.2 and B1. B2 or C aircraft type training approved by DGCA or conducted by an approved maintenance training organisation. Full or partial credit against the basic knowledge requirements and associated examination shall be given for any other technical qualification considered by DGCA to be equivalent to the knowledge standard of this Part. A.4) four years of practical aircraft maintenance experience and Page 13 of 175 1. B2 and C licence for aircraft other than large aircraft endorsed with the appropriate group rating or manufacturer group rating as specified in Addendum I to AMC. within the preceding twenty-four months the holder of an aircraft maintenance engineer’s licence has either acquired six months of maintenance experience in accordance with the privileges granted by the Aircraft Maintenance Engineer’s Licence or met the provision for the issue of appropriate privileges for the first time. B1.25 paragraph and the following minimum practical experience. 3. 4. . A.by G T SELVAN Draft CAR-66 Dated 7th March 2011 2. shall have obtained the basic knowledge requirements specified at 66. 1 and B1.3 five years of practical aircraft maintenance experience. in the relevant category supplemented by at least one year of recent experience in a civil aircraft maintenance environment shall be treated as equivalent to the requirements laid down in (1) and (2) above. Such Page 14 of 175 ii. The required experience must be dependent upon the difference between the licence category/subcategory held and applied for. b) c) d) .by G T SELVAN Draft CAR-66 Dated 7th March 2011 2. acquired outside a civil aircraft maintenance environment.3 or B2 privileges on large aircraft or as support staff in an organisation approved under rule 133B or a combination of both. for Category C with respect to large aircraft: three years of maintenance experience exercising the privileges of category B1. 3. For all applicants. B1 and B2 the experience must be practical which means being involved with a representative cross section of maintenance tasks on aircraft relevant to the privileges conferred by the endorsement. three years of experience of exercising privileges of category B1 or B2 or as support staff in an organisation approved under rule 133B or a combination of both. 4. at least one year of the required experience must be recent maintenance experience on aircraft of the category/subcategory for which the initial aircraft maintenance engineer’s licence is sought. Provided that the experience requirement specified at (1) and (2) above shall be reduced by one year in case of an applicant who has satisfactorily completed training in any training organization approved under rule 133B or who has acquired a Degree in an allied field of Engineering from a recognized University: Provided further that twelve years of practical aircraft maintenance experience. or five years of maintenance experience exercising the privileges of category B1. For subsequent category /subcategory additions to an existing aircraft maintenance engineer’s licence.1 or B1. i. the additional recent maintenance experience required may be less than one year. but must be at least three months.4 privileges on large aircraft or as support staff in base maintenance in an organisation approved under rule 133B or a combination of both.2 or B1. 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 Appendix IV to this CAR For category A. or for category C with respect to aircraft other than large aircraft. for category B2 and sub-categories B1. by G T SELVAN Draft CAR-66 Dated 7th March 2011 additional experience must be typical of the new licence category/subcategory sought. Any certification privileges based upon an aircraft maintenance engineer’s licence becomes invalid as soon as the aircraft maintenance engineer’s licence is invalid. The training shall include practical hands on training and theoretical training as appropriate for each task authorized. the holder of a category B1.45 Type/task training and ratings a) The holder of a category A aircraft maintenance engineer’s licence may only exercise certification privileges on a specific aircraft endorsed on the licence following the satisfactory completion of the relevant category A aircraft task training carried out by an appropriately approved maintenance organization. Except as otherwise specified in paragraph (g). unless the holder works in a DGCA approved maintenance organization 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. B2 or C aircraft maintenance engineer’s licence shall only exercise certification privileges on a specific aircraft type when the aircraft maintenance engineer’s licence is endorsed with the appropriate aircraft type rating. ratings shall be granted following satisfactory completion of the relevant category A. Page 15 of 175 b) c) . Except as otherwise specified in paragraph (h). unless the holder submits his/her aircraft maintenance engineer’s licence to the DGCA. and may be renewed for another five years at a time on receipt of the application for renewal. in order to verify the information contained in the licence is the same as that contained in the DGCA records. 66.A. 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.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 renewal. The aircraft maintenance engineer’s licence is only valid when issued and/or extended by DGCA and when the holder has signed the document b) (c) (d) 66. B1 or B2 or C aircraft type training approved by DGCA. Satisfactory completion of training shall be demonstrated by an examination and/or by workplace assessment carried out by an appropriately approved maintenance organisation. subject to a maximum period of five years in each case.A. A licence shall remain valid for the period specified therein. 3. or manufacturer group ratings. Manufacturer group ratings may be granted after complying with the type rating requirements of two aircraft types representative of the group from the same manufacturer. B1 and B2 approved type training shall include theoretical and practical elements and consist of the appropriate course in relation to para 66. unless DGCA has determined that the complexity of the aircraft in question requires a type rating.aeroplane single piston engine – wooden structure . Theoretical and practical training shall comply with Appendix III to this CAR. 2.helicopter piston engine .A. Notwithstanding paragraph (b).aeroplane multiple piston engines – metal structure . the holder of a category B1 or B2 aircraft maintenance engineer’s licence may also exercise certification privileges.20 (a) privileges. shall be demonstrated by an examination. as required by paragraphs (b) to (e). Full group ratings may be granted after complying with the type rating requirements of three aircraft types representative of the group from different manufacturers. The groups shall consist of the following: (i) for category B1 or C .helicopter turbine engine . no full group rating may be granted to B1 multiple turbine engine aeroplanes. The examinations in respect of category A. However.aeroplane multiple piston engines – wooden structure .aeroplane single piston engine – composite structure Page 16 of 175 e) f) g) 1. when the aircraft maintenance engineer’s licence is endorsed with the appropriate group ratings.aeroplane single piston engine – metal structure . B1 or B2 or C aircraft type ratings shall be conducted by DGCA or in coordination with the DGCA by the training organization conducting the approved type training course. Category C approved type training shall comply with Appendix III to this CAR Completion of approved aircraft type training.by G T SELVAN Draft CAR-66 Dated 7th March 2011 d) Category A. . for aircraft other than large aircraft. where only manufacturer group rating applies. The examination shall comply with Appendix III to this CAR. as evidence of qualification.70 Conversion provisions a) The holder of a valid Aircraft Maintenance Engineer’s Licence on the date of coming into force of this CAR may continue to exercise the privileges of his licence and shall Page 17 of 175 .helicopter h) Notwithstanding paragraph (c). Aircraft type practical experience shall include a representative cross section of maintenance activities relevant to the category.aeroplane . ratings on aircraft other than large aircraft may also be granted. Category A. subject to satisfactory completion of the relevant category A.A. 1. A. The examination shall comply with Appendix III to this CAR. The examination shall be conducted by DGCA or in coordination with the DGCA by an appropriately approved training organisation. i) j) 66.55 Evidence of qualification Personnel exercising certification privileges must produce their licence/Approval/Authorisation/Certificate of Competency within 24 hours.by G T SELVAN Draft CAR-66 Dated 7th March 2011 . The results of aircraft type examination and approved type training shall lapse after a period of 2 years from the date of declaration of result. 3. unless DGCA has determined that the aircraft is complex.aeroplane turbine – single engine .aeroplane multiple piston engines – composite structure . B1. 66.aeroplane turbine – multiple engine (ii) for category B2 or C: . B1 or B2 aircraft type examination and demonstration of practical experience on the aircraft type. if required by an authorized person of DGCA. (f) and (h) shall be permitted to appear again for the same examination after 30 days of additional practical experience. B2 and C approved type examinations must consist of a mechanical examination for category A and B1 and an avionics examination for category B2 and both mechanical and avionics examination for category C. 2. where paragraph (c) approved type training is required. An applicant who had failed in a written examination as required by paragraphs (a). system component. the holder of AMEL may apply to Director General of Civil Aviation for the issue of a duplicate licence. The holder of a qualification gained following such qualification process may be issued an aircraft maintenance engineer’s licence without further examination subject to the conditions specified by DGCA. experience and has passed such examinations as specified in subpart C of this CAR 66.80 Authorization DGCA may grant authorization to the holders of an Aircraft Maintenance Engineer's Licence to carry out maintenance of any new aircraft. repair. accessory or item of equipment including radio equipment not required to be covered under license. instrument. engine. b) A person undergoing a qualification process. Page 18 of 175 . after inspection. an Aircraft Maintenance Engineer’s Licence in the appropriate category subject to such conditions specified by the DGCA in Appendix VII.A. A. experience and training and has passed such examination as specified in subpart D of this CAR. with or without limitation and without further examination.75 Approvals DGCA may grant Approval to the holder of Aircraft Maintenance Engineer’s Licence / other appropriately qualified person employed in an approved maintenance organization to certify maintenance work in respect of an aircraft. Where necessary. ”D” and “X” to cover Aircraft. Engine. prior to the date of entry into force of 6th amendment to the Rule 61 of the Aircraft Rules. 1937. provided that the Director-General is satisfied that the applicant has sufficient knowledge. maintenance. may continue to be qualified till December 2012. modification or test performed in accordance with the procedures approved by the DGCA upon being satisfied that the applicant has sufficient knowledge. Aircraft Maintenance Engineer’s Licences issued prior to this CAR coming into force in category “A” to cover Gliders. Balloons and in category “B”. engine or system which has been brought into the organization and which is not within the scope of his licence and to issue a certificate of release thereof. 66. the aircraft maintenance engineer’s licence shall contain technical limitations in relation to the scope of the pre-existing qualification. overhaul. c) d) 66.71 Duplicate Aircraft Maintenance Engineer’s Licence Where an Aircraft Maintenance Engineers Licence has been lost or mutilated. 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 (b) without altering the privileges hitherto exercised by the holder.by G T SELVAN Draft CAR-66 Dated 7th March 2011 be issued. A. or the holder has signed a certificate in respect of any matter which he is not licensed to deal with in contravention to the Aircraft Rule 61 or CAR 66. revoke. approval and certificate of competency: 1. or the holder has failed to carry out required maintenance resulting from own inspection combined with failure to report such fact to the organization or person for whom the maintenance was intended to be carried out. cancel. Without prejudice to the provisions of Rule 19 the DGCA may after such inquiry as it may deem fit and after giving a reasonable opportunity of being heard. cancellation.by G T SELVAN Draft CAR-66 Dated 7th March 2011 66.A. or (a) (b) (c) (d) (e) (f) (g) (h) Page 19 of 175 . suspension or limitation of the aircraft maintenance engineer’s licence. where it is satisfied that. or found carrying out unfair means when examined.A. 66. or the holder has falsified the maintenance record. upon being satisfied that the applicant has competency and skill and has passed examinations as specified in subpart E of this CAR.85 Certificate of Competency: DGCA may grant a Certificate of Competency to an applicant employed in a firm approved by Director-General to perform specialized processes which may affect the airworthiness of an aircraft. the holder has obtained the aircraft maintenance engineer’s licence or an authorization or an approval or a certificate of competency and/or the certification privileges by fraudulent means. or the holder has carried out maintenance or has issued a certificate of release to service while under the influence of alcohol or any other intoxicating or any psychoactive substance. suspend or endorse any licence or authorization or approval or certificate of competency granted under Sub-rule 15 of Rule 61 or issue a warning or an admonition or debar a person from acquiring a licence temporarily or permanently. or the holder has performed work or granted a certificate in respect of work which has not been performed in a careful and competent manner and was responsible for compromising the airworthiness of the aircraft.95 Withholding. or the holder has issued a certificate of release to service knowing that the maintenance specified on the certificate of release to service has not been carried out or without verifying that such maintenance has been carried out. Page 20 of 175 .by G T SELVAN Draft CAR-66 Dated 7th March 2011 (i) 2. it is undesirable for any other reason that the holder should continue to exercise his privileges granted under the Rule 61. for reasons to be recorded in writing it considers it expedient to do so in public interest. DGCA may withhold issue or extension or renewal of a licence or authorization or approval or certificate of competency if. engine or system which has been brought into the organization and which is not within the scope of his licence. paraplanes. balloons or airships may be certified by an aircraft maintenance engineer holding a licence in Category A or Category B1.400 General Certificate of Competency to persons employed in an approved organization to carry out and certify specialized process which may affect the airworthiness of an aircraft shall be issued in accordance and procedures specified in Appendix X Page 21 of 175 .A. A. gliders.100.by G T SELVAN Draft CAR-66 Dated 7th March 2011 SUBPART B AIRCRAFT OTHER THAN AEROPLANES AND HELICOPTERS 66.A. Certification of micro light aircraft. shall be issued in accordance with the requirements and procedures specified in Appendix IX SUBPART E Certificate of Competency 66. engine or components shall be issued in accordance with requirements and procedures specified in Appendix VIII or requirements and procedures approved in the Maintenance Organization’s Exposition. SUBPART D Authorization 66. SUBPART C COMPONENTS 66. General Micro-light Aircraft. Gliders.300 General Authorization to persons employed in an organization approved by DGCA to carry out maintenance of any new aircraft. The holder of AME licence should have undergone relevant training and gained minimum three months maintenance experience prior to exercising the privileges of the authorization. A. balloons or airships may be carried out by category A or B1 licence holder and authorized by DGCA to carry out and certify such maintenance work.200 General Approval to persons employed in an organization approved by DGCA to certify maintenance work carried out on aircraft. KNOWLEDGE LEVELS . The applicant should be able to apply his knowledge in a practical manner using detailed procedures. The applicant should be able to use mathematical formulae in conjunction with physical laws describing the subject. B1 and B2 are indicated by the allocation of knowledge levels indicators (1. The applicant should be able to use typical terms. The applicant should be able to read and understand sketches. using common words and examples. Objectives: The applicant should be familiar with the basic elements of the subject. B2 AND C AIRCRAFT MAINTENANCE ENGINEER’s LICENCE Basic knowledge for categories A. typical examples.CATEGORY A. Objectives: The applicant should be able to understand theoretical fundamentals of the subject. as appropriate. Page 22 of 175 . An ability to apply that knowledge. 2 or 3) against each applicable subject. B1.Basic Knowledge Requirements 1. drawings and schematics describing the subject. The knowledge level indicators are defined as follows: LEVEL 1 Familiarization with the principal elements of the subject. The applicant should be able to give a general description of the subject using.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Appendix I . LEVEL 2 A general knowledge of the theoretical and practical aspects of the subject. The applicant should be able to give a simple description of the whole subject. by G T SELVAN Draft CAR-66 Dated 7th March 2011 LEVEL 3 A detailed knowledge of the theoretical and practical aspects of the subject. Objectives: The applicant should know the theory of the subject and interrelationship with other subjects. The applicant should be able to give a detailed description of the subject using theoretical fundamentals and specific examples. The applicant should be able to read. understand and prepare sketches. Page 23 of 175 . A capacity to combine and apply the separate elements of knowledge in a logical and comprehensive manner. simple drawings and schematics describing the subject. The applicant should be able to interpret results from various sources and measurements and apply corrective action where appropriate. The applicant should be able to apply his knowledge in a practical manner using manufacturer's instructions. The applicant should understand and be able to use mathematical formulae related to the subject. by G T SELVAN Draft CAR-66 Dated 7th March 2011 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 Modules A or B1 aeroplane with Turbine engine (s) A1.1 B1.1 Piston engine (s) A2 B1.2 A or B1 helicopter with Turbine engine (s) A3 B1.3 Piston engine (s) A4 B1.4 B2 Avionics 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X Not Applicable Not Applicable X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X Page 24 of 175 by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULES & SYLLABUS MODULE 1. Reserved MODULE 2. Reserved LEVEL A x x B1 x x B2 x x MODULE 3. ELECTRICAL FUNDAMENTALS LEVEL A 1 B1 1 B2 1 3.1 Electron Theory Structure and distribution of electrical charges within: atoms, molecules, ions, compounds; Molecular structure of conductors, semiconductors and insulators. 3.2 Static Electricity and Conduction 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 The following terms, their units and factors affecting them: potential difference, electromotive force, voltage, current, resistance, conductance, charge, conventional current flow, electron flow. 3.4 Generation of Electricity Production of electricity by the following methods: light, heat, friction, pressure, chemical action, magnetism and motion. 3.5 DC Sources of Electricity 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 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 1 2 2 1 2 2 1 1 1 1 2 2 X 2 2 Page 25 of 175 by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 3. ELECTRICAL FUNDAMENTALS (a) Resistance and affecting factors; Specific resistance; Resistor colour code, values and tolerances, preferred values, wattage ratings; Resistors in series and parallel; Calculation of total resistance using series, parallel and series parallel combinations; Operation and use of potentiometers and rheostats; Operation of Wheatstone Bridge. (b) 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 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 Operation and function of a capacitor; Factors affecting capacitance area of plates, distance between plates, number of plates, dielectric and dielectric constant, working voltage, voltage rating; 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) 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; LEVEL A X B1 2 B2 2 X 1 1 X 2 2 X 2 2 X 2 2 Page 26 of 175 magnetic flux density. torque. Effects of the following on the magnitude of an induced voltage: magnetic field strength. peak to peak current values and calculations of these values. physical size of coil.13 AC Theory Sinusoidal waveform: phase. and factors affecting output and direction of current flow in DC generators. ELECTRICAL FUNDAMENTALS Electromagnets construction and principles of operation. hysteresis loop. current and power Triangular/Square waves. Page 27 of 175 LEVEL A B1 B2 X 2 2 X 2 2 X 2 2 1 2 2 . cycle. Principle uses of inductors. permeability of coil. Saturation point. eddy currents. The effect the rate of change of primary current and mutual inductance has on induced voltage. average. Induction principles. Hand clasp rules to determine: magnetic field around current carrying conductor. (b) Magnetomotive force. saturation point. retentivity. and factors affecting output power. 3. Action of inducing a voltage in a conductor moving in a magnetic field. frequency.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 3.11 Inductance/Inductor Faraday's Law. shunt wound and compound motors. field strength. root mean square. Construction and purpose of components in DC generator. Factors affecting mutual inductance: number of turns in coil. Single/3 phase principles. Precautions for care and storage of magnets. peak. number of conductor turns. in relation to voltage. period. Lenz's Law and polarity determining rules. Operation of.12 DC Motor/Generator Theory Basic motor and generator theory. Series wound. Back emf. Operation of. Instantaneous. rate of change of flux. position of coils with respect to each other. Mutual induction. Starter Generator construction. 3. permeability. coercive force reluctance. 3. speed and direction of rotation of DC motors. self induction. Permanent Magnet Generators. True power. band pass. Calculation of line and phase voltages and currents. power factor and current calculations.14 Resistive (R).by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 3. 3. Primary and Secondary current. efficiency. C and R circuits. shaded or split pole. parallel. Single phase. Methods of speed control and direction of rotation. turns ratio. band stop. voltage. two phase and three phase alternators. LEVEL A X B1 2 B2 2 X 2 2 X 1 1 X 2 2 X 2 2 Page 28 of 175 . ELECTRICAL FUNDAMENTALS 3. apparent power and reactive power calculations. Calculation of power in a three phase system. power. Three phase star and delta connections advantages and uses.17 AC Generators Rotation of loop in a magnetic field and waveform produced. series and series parallel. inductor.15 Transformers Transformer construction principles and operation. Transformer action under load and no-load conditions. efficiency. 3. Auto transformers. Capacitive (C) and Inductive (L) Circuits Phase relationship of voltage and current in L. Power transfer. Impedance.18 AC Motors Construction. Power dissipation in L.16 Filters Operation. Transformer losses and methods for overcoming them. polarity markings. phase angle. 3. C and R circuits. principles of operation and characteristics of: AC synchronous and induction motors both single and polyphase. high pass. Methods of producing a rotating field: capacitor. Operation and construction of revolving armature and revolving field type AC generators. 3. application and uses of the following filters: low pass. oscillators. Diodes in series and parallel. multivibrators.1 Semiconductors 4. Diode characteristics and properties. leakage current.1. light emitting diode. 4. (b) Construction and operation of PNP and NPN transistors. majority and minority characters. Detailed operation and characteristics of the following devices: silicon controlled rectifier (thyristor). full and half wave rectifiers. Multistage circuit principles: cascades. (b) Materials. maximum forward current. development of a potential across a PN junction in unbiased. clampers.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 4. Diode parameters: peak inverse voltage. 4. electrical properties. forward biased and reverse biased conditions. rectifier diodes.1. Zener diode. varistor.3 Integrated Circuits (a) LEVEL A B1 B2 X 2 2 X X 2 X 1 2 X X 2 X 1 X Page 29 of 175 .1 Diodes (a) Diode symbols. Functional testing of diodes. varistor. P and N type materials: effects of impurities on conduction. electron configuration. Simple circuits including: bias. Operation and function of diodes in the following circuits: clippers. power dissipation. PN junction in a semiconductor. collector and emitter configurations. ELECTRONIC FUNDAMENTALS 4. frequency. Shottky diode. Application of transistors: classes of amplifier (A. bridge rectifiers. voltage doublers and triplers. flip-flop circuits. B. C). light emitting diode. Base. decoupling. varactor diode.1. Transistor characteristics and properties. Component description and orientation. Main characteristics and use of silicon controlled rectifiers (thyristors). Basic appreciation of other transistor types and their uses. temperature. feedback and stabilisation. rectifier diodes. Testing of transistors. photo conductive diode.2 Transistors (a) Transistor symbols. photo conductive diode. push-pull. analogue transducers.4 2 2 B2 3 5. 4.1 B1. Demonstration of conversions between the decimal and binary. reversal of synchro leads. E and I transformers.3 B1. feedback. octal and hexadecimal. voltage follower. control and torque. comparator. deadband. inductive resistive (IR). LEVEL A B1 B2 X X 2 X 1 2 X 1 X X X 2 MODULE 5.3 Servomechanisms (a) Understanding of the following terms: Open and closed loop systems. differential. control and torque. inductive (transformer).by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 4. (b) Understanding of the following terms: Open and closed loop. 5. differentiator. octal and hexadecimal systems and vice versa. X 1 X 2 Page 30 of 175 . DIGITAL TECHNIQUES ELECTRONIC INSTRUMENT SYSTEMS A 1 LEVEL B1. direct. follow up. hunting. Construction operation and use of the following synchro system components: resolvers. follow up. synchronous transmitters. feedback. null. (b) Description and operation of logic circuits and linear circuits. ELECTRONIC FUNDAMENTALS Description and operation of logic circuits and linear circuits/operational amplifiers. Servomechanism defects.1 Electronic Instrument Systems Typical systems arrangements and cockpit layout of electronic instrument systems. inductance and capacitance transmitters. 4. servomechanism. analogue. transformers. damping. Advantages and disadvantages of positive and negative feedback. Operation and amplifier stages connecting methods: resistive capacitive.2 Numbering Systems Numbering systems: binary. inductance transmitters. Introduction to operation and function of an operational amplifier used as: integrator.2 Printed Circuit Boards Description and use of printed circuit boards. Principles of operation and use of the following synchro system components/features: resolvers. differential. transducer. capacitance transmitters.2 B1. 7 Microprocessors Functions performed and overall operation of a microprocessor. clock. DIGITAL TECHNIQUES ELECTRONIC INSTRUMENT SYSTEMS 5. Basic operation of each of the following microprocessor elements: control and processing unit.3 Data Conversion Analogue Data.4 Data Buses Operation of data buses in aircraft systems. byte. Memory associated terms. schematic diagrams. PROM).6 Basic Computer Structure (a) Computer terminology (including bit. Page 31 of 175 X X X 2 LEVEL B1. hardware.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 5.3 B1. Computer technology (as applied in aircraft systems). and digital to analogue converters. 5.5 Logic Circuits (a) Identification of common logic gate symbols. inputs and outputs. Digital Data. (b) Computer related terminology. Operation and application of analogue to digital. Information contained in single and multiaddress instruction words. Operation.1 B1. IC. CPU.4 1 X A X B2 2 X 2 X 2 X 2 X 2 X X X 2 1 2 X X X X X 2 . layout and interface of the major components in a micro computer including their associated bus systems. software. Applications used for aircraft systems. and various memory devices such as RAM. (b)Interpretation of logic diagrams. 5. 5. ROM. tables and equivalent circuits. advantages and disadvantages of the various data storage systems.2 B1. register. arithmetic logic unit. limitations of various types. Operation. including knowledge of ARINC and other specifications. 5. Operation of typical memory devices. 5.12 Electrostatic Sensitive Devices Special handling of components sensitive to electrostatic discharges. airworthiness requirements and possible catastrophic effects of unapproved changes to software programmes. including Cathode Ray Tubes. Fibre optic data bus.14 Electromagnetic Environment Influence of the following phenomena on maintenance practices for electronic system: EMC-Electromagnetic Compatibility EMI-Electromagnetic Interference X 2 2 2 X 2 1 2 LEVEL B1. 5.10 Fibre Optics Advantages and disadvantages of fibre optic data transmission over electrical wire propagation.4 X X A X B2 2 X X X 2 X 1 1 2 X 2 X 2 1 2 2 2 Page 32 of 175 .8 Integrated Circuits Operation and use of encoders and decoders Function of encoder types Uses of medium. Awareness of risks and possible damage. Light Emitting Diodes and Liquid Crystal Display.1 B1. Couplers.2 B1.11 Electronic Displays Principles of operation of common types of displays used in modern aircraft. DIGITAL TECHNIQUES ELECTRONIC INSTRUMENT SYSTEMS 5. 5. large and very large scale integration. remote terminals. component and personnel anti-static protection devices. Terminations.13 Software Management Control Awareness of restrictions. 5.3 B1.9 Multiplexing Operation. control terminals. Application of fibre optics in aircraft systems. application and identification in logic diagrams of multiplexers and demultiplexers. 5.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 5. Fibre optic related terms. 5. Composite and Non.1 B1. fatigue strength and impact resistance. (b) Testing of ferrous materials for hardness.4 A B2 MODULE 6. (b) Testing of non-ferrous material for hardness.1 Aircraft Materials — Ferrous (a) Characteristics. Heat treatment and application of non-ferrous materials.Metallic 6.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 5. tensile strength. properties and identification of common alloy steels used in aircraft. properties and identification of common non-ferrous materials used in aircraft. Heat treatment and application of alloy steels. DIGITAL TECHNIQUES ELECTRONIC INSTRUMENT SYSTEMS HIRF-High Intensity Radiated Field Lightning/lightning protection 5.2 B1.3 B1. tensile strength.15 Typical Electronic/Digital Aircraft Systems 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 X 2 2 2 LEVEL B1.3. fatigue strength and impact resistance.2 Aircraft Materials — Non-Ferrous (a) Characteristics. MATERIALS AND HARDWARE 6.3 Aircraft Materials . 6.1 Composite and non-metallic other than wood and fabric (a) LEVEL A 1 B1 2 B2 1 X 1 1 1 2 1 X 1 1 1 2 2 Page 33 of 175 . 6. Types of defects in fabric. 6. Characteristics.2 Wooden structures Construction methods of wooden airframe structures. Thread forms. dimensions and tolerances for standard threads used in aircraft. stress. Material types. 6. properties and types of fabrics used in aeroplanes. Repair of composite and non-metallic material. Measuring screw threads. Causes of corrosion. (b) The detection of defects/deterioration in composite and non-metallic material. MATERIALS AND HARDWARE Characteristics. other than wood. (b) Types of corrosion and their identification. Sealant and bonding agents. Repair of fabric covering. microbiological. 6. Preservation and maintenance of wooden structure. Types of defects in wood material and wooden structures. 2 2 2 1 2 X LEVEL A B1 B2 1 2 X 1 2 X 1 1 1 2 3 2 Page 34 of 175 .3 Fabric covering Characteristics.1 Screw threads Screw nomenclature.5. properties and types of wood and glue used in aeroplanes. Formation by. Inspections methods for fabric.5 Fasteners 6.4 Corrosion (a) Chemical fundamentals. used in aircraft. galvanic action process. Repair of wooden structure.3.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 6. The detection of defects in wooden structure. properties and identification of common composite and nonmetallic materials. susceptibility to corrosion.3. 6. quick release fasteners. loads. international standards. pneumatic and air system pipes. 6. characteristics and applications.2 Bolts. locking plates.6 Pipes and Unions (a) Identification of. and types of rigid and flexible pipes and their connectors used in aircraft. Self tapping screws. heat treatment.7 Springs Types of springs.5. wire locking. split pins. identification and marking of aircraft bolts. 6. fuel. (b) Standard unions for aircraft hydraulic. Machine screws: aircraft specifications. insertion and removal. 6.5.9 Transmissions Gear types and their application. cotter pins.8 Bearings Purpose of bearings. mesh patterns. keys. idler gears. palnuts. End fittings. materials. 1 2 2 1 2 1 LEVEL A 2 B1 2 B2 2 2 2 2 2 2 2 2 2 1 X 2 1 1 2 2 1 2 1 Page 35 of 175 . chains and sprockets. reduction and multiplication gear systems. construction. 6. Types of bearings and their application.10 Control Cables Types of cables. Belts and pulleys. anchor. studs and screws Bolt types: specification. Nuts: self locking.3 Locking devices Tab and spring washers. dowels. standard types. turnbuckles and compensation devices. material.4 Aircraft rivets Types of solid and blind rivets: specifications and identification. 6. MATERIALS AND HARDWARE 6. 6.5. circlips. driven and driving gears. Gear ratios.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 6. Studs: types and uses. oil. 6. Identifying title block information LEVEL A 3 B1 3 B2 3 3 3 3 3 3 3 X 2 3 1 2 2 Page 36 of 175 . plugs. MATERIALS AND HARDWARE Pulleys and cable system components. identification codes. function and use of electrical general test equipment.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 6. Common power tool types. 7. High tension and co-axial cables. Also.11 Electrical Cables and Connectors Cable types.2 Workshop Practices Care of tools. gases especially oxygen. 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. 1 2 2 LEVEL A B1 B2 MODULE 7. use of workshop materials. MAINTENANCE PRACTICES 7. calibration standards. Aircraft flexible control systems. Operation. Lubrication equipment and methods.1 Safety Precautions-Aircraft and Workshop Aspects of safe working practices including precautions to take when working with electricity. tolerances and projections. Calibration of tools and equipment.4 Avionic General Test Equipment Operation. 7. 7. dimensions. insulators. Crimping. oils and chemicals. function and use of avionic general test equipment. Dimensions. current and voltage rating. Operation and use of precision measuring tools. standards of workmanship. their symbols. coupling. Bowden cables. allowances and tolerances. 6.3 Tools Common hand tool types. 7. Connector types. pins.5 Engineering Drawings. construction and characteristics. sockets. control of tools. Diagrams and Standards Drawing types and diagrams. 7. classes of fits. Installation and clamping of pipes.6 Fits and Clearances Drill sizes for bolt holes. repair. Standard methods for checking shafts.9 Pipes and Hoses Bending and belling/flaring aircraft pipes. Co-axial cables: testing and installation precautions. AN. Schedule of fits and clearances for aircraft and engines. shielding. Specification 100 of the Air Transport Association (ATA) of America.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 7. 7. 7. Testing of crimp joints. their inspection criteria and damage tolerance. maintenance and cleanliness standards. EWIS installations. 1 2 1 LEVEL A B1 B2 1 3 3 1 2 X 1 2 X 1 2 X Page 37 of 175 . protective sleeving techniques including heat shrink wrapping. MAINTENANCE PRACTICES Microfilm. Connector pin removal and insertion. bearings and other parts. Wiring diagrams and schematic diagrams. microfiche and computerised presentations. NAS and MIL. insulation and bonding techniques and testing. Aeronautical and other applicable standards including ISO. Inspection and testing of aircraft pipes and hoses. Identification of wire types. Common system of fits and clearances. 7. Wiring protection techniques: Cable looming and loom support.10 Springs Inspection and testing of springs. cable clamps. rivet spacing and pitch.8 Riveting Riveted joints. inspection. Use of crimp tools: hand and hydraulic operated. 7. MS. twist and wear.7 Electrical Wiring Interconnection System (EWIS) Continuity. Inspection of riveted joints. Limits for bow. Tools used for riveting and dimpling. backlash. Bonding methods and inspection of bonded joints. 7.11 Bearings Testing. Inspection of sheet metal work.16 Aircraft Weight and Balance (a) Centre of Gravity/Balance limits calculation: use of relevant documents.1 Sheet Metal Marking out and calculation of bend allowance. 7. Defects in bearings and their causes. Aircraft weighing. Inspection of belts and pulleys. Sheet metal working. Environmental conditions Inspection methods 7. (b) Preparation of aircraft for weighing. 7. Inspection and testing of control cables. X 2 X LEVEL A 1 B1 2 B2 X 1 2 X 1 2 X X 2 X X X 2 2 2 X X X 2 2 2 X Page 38 of 175 .14. Lubrication requirements of bearings. lever devices. aircraft flexible control systems. Bowden cables. MAINTENANCE PRACTICES 7. Soldering and Bonding (a) Soldering methods. Inspection of screw jacks. inspection of soldered joints. 7. push-pull rod systems. chains and sprockets. cleaning and inspection of bearings.12 Transmissions Inspection of gears. including bending and forming. 7. Brazing.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 7.2 Composite and non-metallic Bonding practices.14.14 Material handling 7. Inspection of welded and brazed joints. (b) Welding and brazing methods.15 Welding.13 Control Cables Swaging of end fittings. penetrant. fatigue and corrosion control programmes. Corrosion removal. securing and associated safety precautions. Effects of environmental conditions on aircraft handling and operation.17 Aircraft Handling and Storage Aircraft taxiing/towing and associated safety precautions. Maintenance Inspection/Quality Control/Quality Assurance. 2 3 2 X 2 X X 2 1 2 X 2 2 2 2 2 2 2 2 2 X 1 2 2 Page 39 of 175 . Aircraft jacking. (b) General repair methods. Aircraft storage methods. radiographic. Interface with aircraft operation.20 Maintenance Procedures Maintenance planning. Ageing. ultrasonic and boroscope methods. Electrical. (c) Non destructive inspection techniques including. assessment and reprotection. (d) Disassembly and re-assembly techniques. De-icing/anti-icing procedures.18 Disassembly. chocking. 7. Structural Repair Manual. 7. Repair and Assembly Techniques (a) Types of defects and visual inspection techniques. Inspection. Refuelling/defuelling procedures. Modification procedures.19 Abnormal Events (a) Inspections following lightning strikes and HIRF penetration. MAINTENANCE PRACTICES LEVEL A 2 B1 2 B2 2 7.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 7. Stores procedures. (e) Trouble shooting techniques 7. (b) Inspections following abnormal events such as heavy landings and flight through turbulence. Certification/release procedures. hydraulic and pneumatic ground supplies. eddy current. Steady state flights.2 Aerodynamics Airflow around a body. snow. wing shape and aspect ratio. ‘Murphy's’ law.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 7. relative airflow. upwash and downwash. MAINTENANCE PRACTICES Additional maintenance procedures. Aerofoil contamination including ice.4 Flight Stability and Dynamics Longitudinal. thrust and drag.1 Physics of the Atmosphere International Standard Atmosphere (ISA). frost. induced drag. Lift coefficient. wash in and wash out. centre of pressure. LEVEL A 1 B1 2 B2 2 1 2 2 1 2 2 1 2 2 MODULE 9. 8. fineness ratio. LEVEL A 1 B1 2 B2 2 Page 40 of 175 .3 Theory of Flight Relationship between lift. The terms: camber. angle of attack. Weight. chord. 8. performance. stall. flight envelope and structural limitations. application to aerodynamics. weight. BASIC AERODYNAMICS 8. Influence of load factor: stall. free stream flow. vortices. Drag coefficient. 8. HUMAN FACTORS 9. Glide ratio. Theory of the turn. mean aerodynamic chord. Generation of Lift and Drag: Angle of Attack. Aerodynamic Resultant. Lift augmentation. polar curve.1 General The need to take human factors into account. laminar and turbulent flow. stagnation. Control of life limited components LEVEL A B1 B2 MODULE 8. Thrust. lateral and directional stability (active and passive). Incidents attributable to human factors/human error. profile (parasite) drag. Boundary layer. ‘Culture’ issues. Stress: domestic and work related. Alcohol. HUMAN FACTORS 9. Complex systems. Repetitive tasks. Illumination. 9. Information processing. Management. Motion and vibration. 9. Claustrophobia and physical access.6 Tasks Physical work.2 Human Performance and Limitations Vision. drug abuse. Keeping up to date. 9. currency. Visual inspection. Time pressure and deadlines. 9. Attention and perception. medication.7 Communication Within and between teams. LEVEL A 1 B1 2 B2 2 1 1 1 2 2 2 1 1 1 1 1 1 2 2 2 Page 41 of 175 .by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 9. Hearing. Climate and temperature. Memory. Motivation and de-motivation. Team working. Workload: overload and underload. Working environment. Sleep and fatigue.4 Factors Affecting Performance Fitness/health. shiftwork. Peer pressure.3 Social Psychology Responsibility: individual and group. supervision and leadership 9.5 Physical Environment Noise and fumes. Work logging and recording. e accidents) Avoiding and managing errors.1 Regulatory Framework Role of International Civil Aviation Organisation. CAR-66. Types of error in maintenance tasks. 10. in particular regarding continuing airworthiness and maintenance. Operators Responsibilities.3 CAR-145 — Approved Maintenance Organisations Detailed understanding of CAR-145. 1 2 2 LEVEL A B1 B2 1 2 2 MODULE 10.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 9.8 Human Error Error models and theories.5 Aircraft Certification (a) General LEVEL A 1 B1 1 B2 1 1 2 2 2 2 2 1 1 1 X 1 1 Page 42 of 175 . 9. Documents to be carried on board.9 Hazards in the Workplace Recognising and avoiding hazards.2 CAR-66 Certifying Staff . 10. The Aircraft Rules ( Applicable to Aircraft Maintenance and Release) Aeronautical Information Circulars ( Applicable to Aircraft Maintenance and Release) CAR Sections 1 and 2 10. Relationship between CAR-21. Implications of errors (i. Aircraft Placarding (Markings). 9. Dealing with emergencies.Maintenance Detailed understanding of CAR-66. The Aircraft Act and Rules made there under Role of the DGCA. HUMAN FACTORS Dissemination of information.4 Aircraft Operations Commercial Air Transport/Commercial Operations Air Operators Certificates. CAR-M. 10. CAR-145. AVIATION LEGISLATION 10. Modifications and repairs. Category 2/3 operations and minimum equipment requirements. CAR-21 Design/Production Organisation Approvals.6 CAR-M Detailed understanding of CAR-M. RVSM. Minimum Equipment List. structural repair manual. Weight Schedule. Service Bulletins. Aircraft Modifications and repairs approval and certification Permit to fly requirements (b) Documents Certificate of Airworthiness.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 10.8 Safety Management System State Safety Programme Basic Safety Concepts Hazards & Safety Risks SMS Operation Page 43 of 175 x 2 2 LEVEL A B1 B2 2 2 2 1 2 2 X 1 1 2 2 2 . etc. Maintenance documentation: maintenance manuals. MNPS Operations All Weather Operations. Supplemental Type Certification. (b) Continuing airworthiness. 10. AVIATION LEGISLATION Certification rules: such as FAA & EACS 23/25/27/29. maintenance and dispatch requirements.. Type Certification. 10. Maintenance checks and inspections. 10. Test flights. ETOPS. manufacturers service information. Radio Station Licence and Approval. Dispatch Deviation Lists. maintenance and dispatch requirements RNP. Noise Certificate.7 Applicable National and International Requirements (a) Maintenance Programme. Master Minimum Equipment Lists. illustrated parts catalogue. Certificate of Registration. Airworthiness Directives. Structural classification. primary. Fail safe. Control using elevons. stall wedges or leading edge devices.1. lift dumpers.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 10. supersonic flight. 11. Operation and effect of trim tabs.9 Fuel Tank Safety Special Federal Aviation Regulations (SFARs) from 14 CFR SFAR 88 of the FAA and of JAA TGL 47 Concept of CDCCL. secondary and tertiary. damage tolerance concepts. transonic flight. Drag inducing devices. variable incidence stabilisers and canards. — yaw control. control surface bias. rudder limiters. saw tooth leading edges. Airworthiness Limitations Items (ALI) 2 2 2 LEVEL A B1 B2 MODULE 11A. servo tabs. mass balance. safe life. area rule. stabilators.1. flaperons.1 1 2 1 2 2 2 Page 44 of 175 .2 Airframe Structures — General Concepts (a) Airworthiness requirements for structural strength. TURBINE AEROPLANE AERODYNAMICS. spoilers.2 High Speed Flight Speed of sound.1 Aeroplane Aerodynamics and Flight Controls Operation and effect of: — roll control: ailerons and spoilers. slots. compressibility buffet. ruddervators. LEVEL A1 B1. flaps. speed brakes. Factors affecting airflow in engine intakes of high speed aircraft. spring tabs. Effects of sweepback on critical Mach number. vortex generators. balance and antibalance (leading) tabs. aerodynamic heating. STRUCTURES AND SYSTEMS 11. High lift devices. Effects of wing fences. subsonic flight. AVIATION LEGISLATION SMS Safety performance Safety Assurance 10. aerodynamic balance panels. Boundary layer control using. — pitch control: elevators. shock wave. 11. critical Mach number. Zonal and station identification systems. Mach number. slats.1 Theory of Flight 11. struts. such as chromating.3.4 Flight Control Surfaces (ATA 55/57) Construction and attachment. Wing. Doors and emergency exits: construction. ties. strain.3 Airframe Structures — Aeroplanes 11.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 11A. 11. bulkheads.3. stringers. Aircraft bonding (b) Construction methods of: stressed skin fuselage. Seat installation and cargo loading system. compression. bolting. Balancing — mass and aerodynamic. control surface and high lift/drag attachments.5 Nacelles/Pylons (ATA 54) 1 2 1 2 LEVEL A1 B1. 11. Structure assembly techniques: riveting. pylon. Fuel storage. reinforcement. 11.2 Wings (ATA 57) Construction. TURBINE AEROPLANE AERODYNAMICS. Surface cleaning. painting. Drains and ventilation provisions. STRUCTURES AND SYSTEMS Stress. beams. doublers. torsion. stabiliser.3. Lightning strike protection provision. 11. formers. hoop stress.3 Stabilisers (ATA 55) Construction. bending. wing. System installation provisions. Windows and windscreen construction and mechanisms. methods of skinning. Landing gear. Control surface attachment. pylon and undercarriage attachments. fatigue. tension. floor structures. anti-corrosive protection. empennage and engine attachments. bonding Methods of surface protection. mechanisms. operation and safety devices. longerons. 11.3. shear.1 1 2 1 2 1 2 1 2 Page 45 of 175 . frames. Airframe symmetry: methods of alignment and symmetry checks.3. anodising.1 Fuselage (ATA 52/53/56) Construction and pressurisation sealing. Compasses: direct reading. 11. 11.3 Pressurisation Pressurisation systems. 11. Flow.4.1 Instrument Systems (ATA 31) Pitot static: altimeter.6 Electrical Power (ATA 24) Batteries Installation and Operation. DC power generation.4.1 Air supply Sources of air supply including engine bleed. Gyroscopic: artificial horizon. stall warning systems. temperature and humidity control system. attitude director. 11.1 1 3 1 3 1 3 1 1 1 3 Page 46 of 175 . direction indicator. Communications (ATA 23). air speed indicator. 11.4. turn and slip indicator. Navigation Systems (ATA 34). Other aircraft system indication. Auto Flight (ATA 22). 1 2 1 2 LEVEL A1 B1. remote reading.2 Avionic Systems Fundamentals of system lay-outs and operation of. vertical speed indicator.2 Air Conditioning Air conditioning systems. 11. STRUCTURES AND SYSTEMS Construction. 11. Control and indication including control and safety valves. Engine mounts. Angle of attack indication.5 Instruments/Avionic Systems 11. Cabin pressure controllers. TURBINE AEROPLANE AERODYNAMICS.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 11A.4 Safety and warning devices Protection and warning devices. turn coordinator. Air cycle and vapour cycle machines Distribution systems.4.5. Firewalls.4 Air Conditioning and Cabin Pressurisation (ATA 21) 11. APU and ground cart.5. horizontal situation indicator. Power distribution. Active load control. electrical. Seats. 11. spoiler. rudder.9 Flight Controls (ATA 27) Primary controls: aileron. Stall protection/warning system. 11. transformers. Yaw damper.7 Equipment and Furnishings (ATA 25) (a) Emergency equipment requirements. LEVEL A1 B1. Balancing and rigging. gust locks systems. Equipment lay-out. Airstairs. Fire extinguishing systems. Artificial feel. 11. System operation: manual. Circuit protection.10 Fuel Systems (ATA 28) System lay-out. rectifiers. System tests. Trim control. Cabin entertainment equipment. Emergency power generation. speed brakes. TURBINE AEROPLANE AERODYNAMICS. pneumatic. External/Ground power. (b) Cabin lay-out. High lift devices. Mach trim. hydraulic. harnesses and belts. elevator. Voltage regulation.1 2 2 1 1 1 3 1 1 1 3 1 3 Page 47 of 175 . Cargo handling and retention equipment. (b) Portable fire extinguisher 11. Cabin Furnishing Installation. Lift dump. STRUCTURES AND SYSTEMS AC power generation. Inverters. rudder limiter. Galley installation.8 Fire Protection (ATA 26) (a) Fire and smoke detection and warning systems. fly-by-wire.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 11A. hot air. Hydraulic fluids. mechanical. Internal: cabin. antiskid and autobraking.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 11A. Emergency pressure generation. Probe and drain heating. Supply systems. Indications and warning. ice. pneumatic and chemical. 1 3 LEVEL A1 B1. Tyres. classification and detection. Power distribution.14 Lights (ATA 33) External: navigation. Dumping. landing. 11. Longitudinal balance fuel systems. venting and draining. cockpit. taxiing. 1 3 2 3 2 3 Page 48 of 175 . cargo. Cross-feed and transfer.1 11. TURBINE AEROPLANE AERODYNAMICS. Anti-icing systems: electrical. shock absorbing.11 Hydraulic Power (ATA 29) System lay-out. Refuelling and defuelling. Indications and warnings. Hydraulic reservoirs and accumulators. Emergency. STRUCTURES AND SYSTEMS Fuel tanks. brakes. Extension and retraction systems: normal and emergency. Rain repellant.13 Landing Gear (ATA 32) Construction. Pressure Control. Pressure generation: electric. Interface with other systems. De-icing systems: electrical. Wiper systems 11. 11. Steering. pneumatic.12 Ice and Rain Protection (ATA 30) Ice formation. anti-collision. Indication and warning systems. hot air and chemical. Wheels. by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 11A. variable incidence stabilisers and canards. supply. storage. ruddervators. LEVEL A1 1 B1. Electronic library system.17 Water/Waste (ATA 38) Water system lay-out. 1 2 MODULE 11B. cabin. servicing and draining.18 On Board Maintenance Systems (ATA 45) Central maintenance computers.1.2 subcategory. rudder limiters. — pitch control: elevators. stabilators. Data loading system. PISTON AEROPLANE AERODYNAMICS. Indications and warnings. ground supply. Printing. reservoirs. charging and distribution. Control using elevons.1 3 1 2 2 3 11. 11.2 Note: The scope of this Module should reflect the technology of aeroplanes pertinent to the A2 and B1. 11.1 Aeroplane Aerodynamics and Flight Controls Operation and effect of: — roll control: ailerons and spoilers. Toilet system lay-out. Indications and warnings. — yaw control. Supply regulation. TURBINE AEROPLANE AERODYNAMICS. 11. Sources. STRUCTURES AND SYSTEMS LEVELL A2 B1. Sources: engine/APU. Corrosion aspects. STRUCTURES AND SYSTEMS 11.15 Oxygen (ATA 35) System lay-out: cockpit. Structure monitoring (damage tolerance monitoring). flushing and servicing. distribution. compressors. Interfaces with other systems. Pressure control. Page 49 of 175 1 2 .16 Pneumatic/Vacuum (ATA 36) System lay-out. Distribution.1 Theory of Flight 11. methods of skinning. Effects of wing fences. torsion. anti-corrosive protection. Window and windscreen attachment. Doors and emergency exits: construction and operation. formers. Structure assembly techniques: riveting. empennage and engine attachments. shear. speed brakes. Operation and effect of trim tabs. compression. wing. frames. Methods of surface protection. painting. 11. bulkheads. beams. strain. spring tabs. reinforcement. aerodynamic balance panels. slots. balance and antibalance (leading) tabs. servo tabs. control surface bias. struts. bonding. primary. flaperons. Seat installation. stringers. spoilers. fatigue. tension. stall wedges or leading edge devices.1. bolting. Lightning strike protection provision. secondary and tertiary. mass balance. safe life. PISTON AEROPLANE AERODYNAMICS. damage tolerance concepts. longerons.2 High Speed Flight — N/A — 11. Drag inducing devices.3. bending. Aircraft bonding (b) Construction methods of: stressed skin fuselage.2 2 2 1 2 1 2 Page 50 of 175 .3 Airframe Structures — Aeroplanes 11. Surface cleaning. vortex generators. anodising. X X LEVELL A2 B1. saw tooth leading edges. floor structures. Structural classification. STRUCTURES AND SYSTEMS High lift devices. Fail safe. lift dumpers. Airframe symmetry: methods of alignment and symmetry checks. Drains and ventilation provisions.2 Airframe Structures — General Concepts (a) Airworthiness requirements for structural strength.1 Fuselage (ATA 52/53/56) Construction and pressurisation sealing. Boundary layer control using. 11. ties. such as chromating. Stress. flaps. slats. hoop stress. Zonal and station identification systems.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 11B. System installation provisions. tail-plane pylon and undercarriage attachments. Wing. doublers. Other aircraft system indication. Landing gear.5 Instruments/Avionic Systems 11. 11. turn coordinator. STRUCTURES AND SYSTEMS 11. 11.1 Instrument Systems (ATA 31) Pitot static: altimeter. control surface and high lift/drag attachments. protection and warning devices.3 Stabilisers (ATA 55) Construction.3.5. attitude director. — Navigation Systems (ATA 34).3. remote reading. Control surface attachment. stall warning systems. Cabin pressure controllers.4 Flight Control Surfaces (ATA 55/57) Construction and attachment.3.5.5 Nacelles/Pylons (ATA 54) (a) Nacelles/Pylons: — Construction. 11.2 Wings (ATA 57) Construction. Compasses: direct reading. turn and slip indicator.4 Air Conditioning and Cabin Pressurisation (ATA 21) Pressurisation and air conditioning systems. Angle of attack indication. — Firewalls. horizontal situation indicator. Balancing — mass and aerodynamic. — Communications (ATA 23).by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 11B. pylon. Fuel storage. direction indicator. 11. vertical speed indicator.3. 1 1 1 2 LEVELL A2 1 B1. — Engine mounts.2 2 1 2 1 2 1 2 1 3 Page 51 of 175 . PISTON AEROPLANE AERODYNAMICS. air speed indicator. Gyroscopic: artificial horizon. 11. 11.2 Avionic Systems Fundamentals of system lay-outs and operation of: — Auto Flight (ATA 22). LEVELL A2 1 B1. Inverters. High lift devices. 11. 11. System operation: manual. Gust locks. Seats. transformers. Trim tabs. rudder. Power distribution. Galley installation.2 3 2 2 1 1 1 3 1 1 3 3 1 3 Page 52 of 175 . STRUCTURES AND SYSTEMS 11. PISTON AEROPLANE AERODYNAMICS. Voltage regulation. System tests. Fire and smoke detection and warning systems. Cabin entertainment equipment. Cabin Furnishing Installation (level 2). Circuit protection.8 Fire Protection (ATA 26) (a) Fire extinguishing systems.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 11B. 11. Cargo handling and retention equipment.10 Fuel Systems (ATA 28) System lay-out. DC power generation. Stall warning system. (b) Portable fire extinguisher. 11. Fuel tanks. Balancing and rigging. (b) Cabin lay-out.6 Electrical Power (ATA 24) Batteries Installation and Operation. elevator. harnesses and belts.9 Flight Controls (ATA 27) Primary controls: aileron. Airstairs.7 Equipment and Furnishings (ATA 25) (a) Emergency equipment requirements. Equipment lay-out. 11.13 Landing Gear (ATA 32) Construction. Hydraulic fluids. 1 3 LEVELL A2 B1. 11. Cross-feed and transfer.16 Pneumatic/Vacuum (ATA 36) System lay-out. pneumatic and chemical. Probe and drain heating. anti collision. ice. 11. Indications and warnings. cargo. STRUCTURES AND SYSTEMS Supply systems.11 Hydraulic Power (ATA 29) System lay-out.12 Ice and Rain Protection (ATA 30) Ice formation. charging and distribution. Power distribution. Wheels. classification and detection. cockpit. De-icing systems: electrical. Wiper systems. Pressure generation: electric. 11. Tyres. landing.2 1 3 2 3 2 2 1 3 1 3 Page 53 of 175 . Sources. 11.14 Lights (ATA 33) External: navigation. Indications and warning. cabin. Indication and warning systems.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 11B. antiskid and autobraking. hot air. Supply regulation. storage. Pressure Control. PISTON AEROPLANE AERODYNAMICS. taxiing. Refuelling and defuelling. 11. Indications and warnings. Internal: cabin. mechanical. shock absorbing. Steering. Emergency. Hydraulic reservoirs and accumulators. brakes. Extension and retraction systems: normal and emergency.15 Oxygen (ATA 35) System lay-out: cockpit. Blade Dampers: Function and construction. Dissymmetry of lift. 12. Corrosion aspects. System operation: manual. servicing and draining. 11. Translating tendency and its correction.17 Water/Waste (ATA 38) Water system lay-out.3 A4 B1. overpitching. power settling. Vortex ring state. 2 3 LEVELL A2 B1. Coriolis effect and compensation. compressors.4 1 2 2 3 1 3 Page 54 of 175 . fixed and adjustable stabilisers. STRUCTURES AND SYSTEMS 12. Indications and warnings. Distribution. Trim control. electrical and flyby-wire.3 Blade Tracking and Vibration Analysis LEVEL A3 B1. Swashplate. hydraulic. Effects of gyroscopic precession. Yaw control: Anti-Torque Control. Pressure control. STRUCTURES AND SYSTEMS Sources: engine/APU. Artificial feel. Auto-rotation. reservoirs. supply. HELICOPTER AERODYNAMICS.2 Flight Control Systems Cyclic control. Toilet system lay-out. Collective control. Ground effect. Blade tip stall. Tail rotor. PISTON AEROPLANE AERODYNAMICS. Torque reaction and directional control. Interfaces with other systems. 12. Balancing and Rigging.1 Theory of Flight — Rotary Wing Aerodynamics Terminology. Rotor Blades: Main and tail rotor blade construction and attachment. ground supply. distribution.2 MODULE 12. flushing and servicing.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 11B. Main Rotor Head: Design and Operation features. bleed air. flexible couplings. bulkheads. safe life. Zonal and station identification systems. formers. Airframe symmetry: methods of alignment and symmetry checks.3 A4 B1. damage tolerance concepts. Tail rotor drive shafts. bolting. Fail safe. torsion. stabiliser and undercarriage attachments. (b) Construction methods of: stressed skin fuselage. Ground resonance.6 Air Conditioning (ATA 21) Page 55 of 175 1 3 LEVEL A3 B1. 12. Lightning strike protection provision. struts. secondary and tertiary. vibration reduction methods. Vibration types.4 2 2 1 3 . shear. free wheel units and rotor brake. Engine mounts. bearings. methods of skinning and anti-corrosive protection. Main and tail rotor tracking. floor structures. strain. 12. primary. main and tail rotors. frames. Static and dynamic balancing. STRUCTURES AND SYSTEMS Rotor alignment. hoop stress. Clutches. longerons. compression. Pylon. vibration dampers and bearing hangers 12. Stress. Firewalls. bending. fatigue.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 12. HELICOPTER AERODYNAMICS. doublers. Fuel storage. bonding. Surface cleaning. beams. Structure assembly techniques: riveting. System installation provisions. Drains and ventilation provisions. Doors: construction. ties. painting. operation and safety devices. such as chromating. Seat installation. Structural classification.5 Airframe Structures (a) Airworthiness requirements for structural strength. Windows and windscreen construction. tension.4 Transmissions Gear boxes. anodising. stringers. Methods of surface protection. reinforcement. mechanisms. vertical speed indicator. harnesses and belts. direction indicator. Navigation Systems (ATA 34). (b) Emergency flotation systems.1 Air supply Sources of air supply including engine bleed and ground cart. Cabin lay-out. External/Ground power. Distribution systems. transformers.6. Seats. Power distribution. 12. Emergency power generation.3 A4 B1.2 Avionic Systems Fundamentals of system layouts and operation of: Auto Flight (ATA 22). Compasses: direct reading. turn coordinator. 12. attitude director. DC power generation. Flow and temperature control systems. Inverters.6. HELICOPTER AERODYNAMICS. 1 3 1 2 1 1 2 2 1 1 Page 56 of 175 . Gyroscopic:artificial horizon.7. rectifiers. cargo retention.7. remote reading. Communications (ATA 23). Voltage regulation. horizontal situation indicator. STRUCTURES AND SYSTEMS LEVEL A3 B1. 12.4 1 2 12. Protection and warning devices.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 12.1 Instrument Systems (ATA 31) Pitot static:altimeter. Vibration indicating systems — HUMS.8 Electrical Power (ATA 24) Batteries Installation and Operation.7 Instruments/Avionic Systems 12. Other aircraft system indication. Lifting systems. AC power generation.2 Air Conditioning Air conditioning systems. Circuit protection.9 Equipment and Furnishings (ATA 25) (a) Emergency equipment requirements. turn and slip indicator. air speed indicator. 12. 12. 12. Pressure Control.12 Hydraulic Power (ATA 29) System lay-out.10 Fire Protection (ATA 26) Fire and smoke detection and warning systems. Hydraulic fluids. Fuel tanks. Cabin Furnishing Installation. HELICOPTER AERODYNAMICS.11 Fuel Systems (ATA 28) System lay-out. Rain repellant and removal.4 1 3 1 3 1 3 2 3 Page 57 of 175 . Cross-feed and transfer. Supply systems. Wheels. Dumping. pneumatic. tyres. Hydraulic reservoirs and accumulators.14 Landing Gear (ATA 32) Construction. brakes. venting and draining.3 A4 B1. Pressure generation: electric. Probe and drain heating. Extension and retraction systems: normal and emergency. Interface with other systems.13 Ice and Rain Protection (ATA 30) Ice formation. shock absorbing. Indications and warning. Fire extinguishing systems. Indications and warnings. 12. Emergency pressure generation. 12. STRUCTURES AND SYSTEMS Equipment lay-out. mechanical. Power distribution.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 12. hot air and chemical. Refuelling and defuelling. Wiper system 12. 1 3 LEVEL A3 B1. classification and detection. 12. Indication and warning systems. Anti-icing and de-icing systems: electrical. System tests. 3 A4 B1. Indications and warnings. STRUCTURES AND SYSTEMS Steering. floats.15 Lights (ATA 33) External: navigation. ice. reservoirs.16 Pneumatic/Vacuum (ATA 36) System lay-out. Emergency. taxiing.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 12. Interfaces with other systems.4 1 3 Page 58 of 175 . cargo.. Skids. 12. Internal: cabin. ground supply. Distribution. cockpit. Sources: engine. 12. compressors. 2 3 LEVEL A3 B1. Pressure control. landing. HELICOPTER AERODYNAMICS. 4 Communication/Navigation (ATA 23/34) 3 Page 59 of 175 . speed brakes. — yaw control. Autopilot navigation aids interface. Control using elevons. Automatic Landing Systems: principles and categories. approach. Yaw dampers. lift dumpers. control surface bias. 13. servo tabs. flaps. rudder limiters. 13. system monitors and failure conditions. land. (c) Rotary Wing Aerodynamics Terminology. Command signal processing. subsonic flight. Lightning strike protection provision. ruddervators. glideslope.1 Theory of Flight (a) Aeroplane Aerodynamics and Flight Controls Operation and effect of: — roll control: ailerons and spoilers. Modes of operation: roll. stabilators. Autothrottle systems. Stability Augmentation System in helicopters. Automatic trim control. modes of operation. goaround. STRUCTURES AND SYSTEMS 13. Operation and effect of trim tabs. High lift devices: slots. Operation and effect of cyclic. pitch and yaw channels. transonic flight. (b) Zonal and station identification systems. collective and anti-torque controls. critical Mach number.3 Autoflight (ATA 22) Fundamentals of automatic flight control including working principles and current terminology. — pitch control: elevators.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 13. AIRCRAFT AERODYNAMICS. supersonic flight. slats. Mach number. (b) High Speed Flight Speed of sound. Electrical bonding.2 Structures — General Concepts (a) Fundamentals of structural systems. variable incidence stabilisers and canards. Drag inducing devices: spoilers. LEVEL B2 1 1 1 1 2 3 13. — Weather avoidance radar. — Cockpit Voice Recorder. antennas. — Emergency Locator Transmitters. transformers. Power distribution. External/Ground power. transmission lines. Distance Measuring Equipment (DME). — Air Traffic Control transponder.5 Electrical Power (ATA 24) Batteries Installation and Operation. 13. communication. AIRCRAFT AERODYNAMICS. — Doppler navigation. — High Frequency (HF) communication. — Audio. receiver and transmitter. — Very High Frequency omnidirectional range (VOR). — Very Low Frequency and hyperbolic navigation (VLF/Omega). secondary surveillance radar. — Inertial Navigation System. Voltage regulation.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 13. — Microwave Landing System (MLS). RNAV systems. — ARINC communication and reporting. 3 LEVEL B2 Page 60 of 175 . — Flight Director systems. — Flight Management Systems. Global Navigation Satellite Systems (GNSS). rectifiers. — Automatic Direction Finding (ADF). — Global Positioning System (GPS). — Traffic Alert and Collision Avoidance System (TCAS). DC power generation. Circuit protection. Emergency power generation. STRUCTURES AND SYSTEMS Fundamentals of radio wave propagation. — Radio altimeter. — Instrument Landing System (ILS). AC power generation. Inverters. — Area navigation. Working principles of following systems: — Very High Frequency (VHF) communication. Direct reading pressure and temperature gauges. Artificial horizons. LEVEL B2 3 1 2 2 Page 61 of 175 . Air data computers. System operation: manual. Instrument pneumatic systems. AIRCRAFT AERODYNAMICS. Active load control. Terminology. Atmosphere. Electronic Flight Instrument Systems. 13.7 Flight Controls (ATA 27) (a) Primary controls: aileron. pneumatic. Slip indicators. Yaw damper. Directional gyros. gust locks. Temperature indicating systems. High lift devices. Trim control.6 Equipment and Furnishings (ATA 25) Electronic emergency equipment requirements. 13. fly by wire. spoiler. rudder limiter. Machmeters.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 13. speed brakes. Airspeed indicators. Cabin entertainment equipment. (b) System operation: electrical. Altimeters. Fuel quantity indicating systems. Compass systems. Vertical speed indicators. Pitot static systems. Ground Proximity Warning Systems. Altitude reporting/alerting systems. STRUCTURES AND SYSTEMS 13. Pressure measuring devices and systems. Stall protection systems. Artificial feel. Mach trim. hydraulic. Flight Data Recording systems. Gyroscopic principles. elevator.8 Instrument Systems (ATA 31) Classification. rudder. Lift dump. Engine speed. STRUCTURES AND SYSTEMS Instrument warning systems including master warning systems and centralised warning panels. 14. Engine torque. Printing. 13. Engine Thrust Indication: Engine Pressure Ratio. taxiing. landing. Oil pressure and temperature. Emergency. turbofan. 13. Manifold pressure. B2 1 2 2 Page 62 of 175 . (b) Electronic Engine control and fuel metering systems (FADEC). cargo.1 Turbine Engines (a) Constructional arrangement and operation of turbojet. Propeller speed. Electronic library system. Fuel pressure. AIRCRAFT AERODYNAMICS. cockpit.9 Lights (ATA 33) External: navigation.2 Engine Indicating Systems Exhaust gas temperature/Interstage turbine temperature systems. Vibration measurement and indication. engine turbine discharge pressure or jet pipe pressure systems. turboshaft and turbopropeller engines. Structure monitoring (damage tolerance monitoring). 3 LEVEL B2 2 LEVEL MODULE 14 PROPULSION 14.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 13. ice. Data loading system.10 On board Maintenance Systems (ATA 45) Central maintenance computers. Internal: cabin. Stall warning systems and angle of attack indicating systems. temperature and flow. Fan balancing. 15. 15. Methods of air flow control: bleed valves. limitations. Compressor ratio. Causes and effects of turbine blade stress and creep. Ice protection. specific fuel consumption. turboprop. Nozzle guide vanes. choked nozzle thrust. flat rating. net thrust. acceleration. thrust horsepower. variable stator vanes. velocity. resultant thrust.4 Compressors Axial and centrifugal types. power. 15. Constructional features and operating principles and applications. turboshaft. Engine ratings. 15. static thrust. energy. influence of speed. turbofan. kinetic energy. Pressure. temperature and velocity of the gas flow. work. rotating stator blades. thrust distribution. GAS TURBINE ENGINE 15. Brayton cycle.5 Combustion Section Constructional features and principles of operation. Newton's laws of motion.2 Engine Performance Gross thrust. 15. Operation: Causes and effects of compressor stall and surge. Blade to disk attachment.6 Turbine Section Operation and characteristics of different turbine blade types. Constructional arrangement and operation of turbojet. altitude and hot climate. By-pass ratio and engine pressure ratio.1 Fundamentals Potential energy. variable inlet guide vanes. equivalent shaft horsepower.3 Inlet Compressor inlet ducts Effects of various inlet configurations.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 15. LEVEL A 1 B1 2 X 2 2 2 1 2 1 2 2 2 Page 63 of 175 . Engine efficiencies. The relationship between force. GAS TURBINE ENGINE 15.11 Fuel Systems Operation of engine control and fuel metering systems including electronic engine control (FADEC). Thrust reversers. 15.14 Engine Indication Systems Exhaust Gas Temperature/Interstage Turbine Temperature. 15. 1 2 LEVEL A 1 B1 2 X 2 1 2 1 2 1 2 1 2 Page 64 of 175 . Engine speed. 15. Engine noise reduction.7 Exhaust Constructional features and principles of operation. Convergent. Engine Thrust Indication: Engine Pressure Ratio.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 15.9 Lubricants and Fuels Properties and specifications. Power.8 Bearings and Seals Constructional features and principles of operation.13 Starting and Ignition Systems Operation of engine start systems and components. 15. 15. engine turbine discharge pressure or jet pipe pressure systems. 15. Safety precautions. Oil pressure and temperature.10 Lubrication Systems System operation/lay-out and components. divergent and variable area nozzles. sealing and external air services. Torque. Systems lay-out and components. Maintenance safety requirements.12 Air Systems Operation of engine air distribution and anti-ice control systems. Fuel pressure and flow. Vibration measurement and indication. 15. Fuel additives. Ignition systems and components. including internal cooling. Integrated engine and propeller controls. Compressor washing/cleaning. reduction gearing. Trend (including oil analysis.15 Power Augmentation Systems Operation and applications. control cables and rods.20 Fire Protection Systems Operation of detection and extinguishing systems. vibration and boroscope) monitoring. 15. operation. 15. drive systems. GAS TURBINE ENGINE 15. 15. couplings. 15. Foreign Object Damage. feeders. wiring looms. protective systems. Afterburner systems. anti-vibration mounts. cowlings.17 Turbo-shaft engines Arrangements. Overspeed safety devices. lifting points and drains. water methanol. engine mounts.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 15. Inspection of engine and components to criteria. acoustic panels. 15. Interpretation of engine power output and parameters.16 Turbo-prop Engines Gas coupled/free turbine and gear coupled turbines.22 Engine Storage and Preservation Preservation and depreservation for the engine and accessories/ systems. 15. Reduction gears.18 Auxiliary Power Units (APUs) Purpose. 1 3 LEVEL A X B1 1 1 2 1 2 1 2 1 2 1 2 X 2 Page 65 of 175 . control systems. hoses.19 Powerplant Installation Configuration of firewalls. Water injection. connectors.21 Engine Monitoring and Ground Operation Procedures for starting and ground run-up. 15. pipes. tolerances and data specified by engine manufacturer. 4. Low and high tension systems.4. Magneto types. sumps. spark plugs.4 Engine Fuel Systems 16. Propeller reduction gearboxes. PISTON ENGINE 16. 16. Ignition harnesses.1 Fundamentals Mechanical. pre-ignition. construction and principles of operation. 4 stroke.4. Cylinder and piston assemblies. cam shafts. crank shaft.1 Carburetors Types.2 Fuel injection systems Types. 16. Systems lay-out and components. Icing and heating. Operating principles — 2 stroke.3 Electronic engine control Operation of engine control and fuel metering systems including electronic engine control (FADEC).6 Induction.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 16. Connecting rods. Otto and Diesel. Accessory gearbox. 16. pre-heat systems. Piston displacement and compression ratio. Exhaust and Cooling Systems LEVEL A 1 B1 2 1 2 1 2 1 2 1 2 1 2 1 2 1 2 Page 66 of 175 . inlet and exhaust manifolds. construction and principles of operation.2 Engine Performance Power calculation and measurement.5 Starting and Ignition Systems Starting systems. Factors affecting engine power. construction and principles of operation. 16. Valve mechanisms. Mixtures/leaning.3 Engine Construction Crank case. Engine configuration and firing order. 16. 16. thermal and volumetric efficiencies. 16. 16.10 Engine Indication Systems Engine speed. cowlings. System protection. Manifold pressure. System terminology. engine cooling systems — air and liquid. feeders. Oil pressure and temperature. pipes. control cables and rods. acoustic panels. Control systems. Exhaust systems. PISTON ENGINE Construction and operation of: induction systems including alternate air systems. engine mounts. Exhaust Gas Temperature.12 Engine Monitoring and Ground Operation Procedures for starting and ground run-up. Inspection of engine and components: criteria. Safety precautions. Cylinder head temperature. 16. 16. hoses.13 Engine Storage and Preservation Preservation and depreservation for the engine and accessories/ systems Page 67 of 175 X 2 1 2 LEVEL A B1 1 2 1 2 1 2 1 2 1 3 . and data specified by engine manufacturer. lifting points and drains.9 Lubrication Systems System operation/lay-out and components. Fuel additives.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 16. 16.8 Lubricants and Fuels Properties and specifications. tolerances.7 Supercharging/Turbocharging Principles and purpose of supercharging and its effects on engine parameters.11 Powerplant Installation Configuration of firewalls. wiring looms. 16. connectors. Coolant temperature. Interpretation of engine power output and parameters. Fuel pressure and flow. anti-vibration mounts. 16. 16. Construction and operation of supercharging/turbocharging systems. blade back and hub assembly. 17. Blade tracking. angle of attack. 17.2 Propeller Construction Construction methods and materials used in wooden. Assessment of blade damage. mechanical and electrical/electronic. blade shank. impact damage. 17. corrosion. composite and metal propellers. Aerodynamic.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MODULE 17. reverse angle.4 Propeller Synchronising Synchronising and synchrophasing equipment.1 Fundamentals Blade element theory. Blade station. erosion. PROPELLER 17. Relative airflow on blade angle of attack. Overspeed protection. Vibration and resonance. Propeller/spinner installation. Propeller engine running. Propeller treatment/repair schemes.3 Propeller Pitch Control Speed control and pitch change methods. 17. High/low blade angle.6 Propeller Maintenance Static and dynamic balancing. Fixed pitch. delamination. rotational speed. controllable pitch. 17. centrifugal. blade face. Torque. constant speeding propeller. and thrust forces. Propeller slip. Feathering and reverse pitch. 17.5 Propeller Ice Protection Fluid and electrical de-icing equipment.7 Propeller Storage and Preservation Propeller preservation and depreservation LEVEL A 1 B1 2 1 2 1 2 x 2 1 2 1 3 1 2 Page 68 of 175 . June and October) will be held in a calendar year at regional and sub-regional offices of DGCA located in New Delhi.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Appendix II . 1. gained at least three months of aeronautical engineering experience and desirous of appearing in knowledge examinations conducted by the DGCA are required to apply to CEO. Bangalore. Note: Allotment of Computer Number does not imply an applicant’s acceptance for appearing in the written basic knowledge examination. For appearing in the written examination. East Block III. ii) Should have gained at least six months of Aircraft Maintenance Experience in relevant category / sub-category from an approved maintenance organisation or completed six Page 69 of 175 .1 Candidates who have passed 10+2 examination with Physics. the applicant must meet the eligibility requirements. New Delhi 110 066.4 Computer number shall be quoted in all the applications and correspondence with DGCA for all examinations and issue / endorsement of AME licence. Bhopal. Applications for type examinations and skill test shall be made to the respective Regional Airworthiness Office. 1. Chennai. DGCA. 1. 2. O/o DGCA.3 The CEO. on CA Form 19-07 and shall obtain a permanent computer number. i) Should have a computer number allotted by the CEO. DGCA will allot the computer number in respect of applications received on or before 15th of a month. Guwahati.1 Candidates desirous of appearing in the (AME Licence) Basic Knowledge Examination shall satisfy the following requirements. Bhubaneswar. Mumbai. DGCA.Examination and Standard General: All basic knowledge examination shall be conducted by the Central Examination Organisation (CEO). Appearing in Basic Knowledge Examination 2. Lucknow. Chemistry and Mathematics from recognized board or university or its equivalent. All type examinations and skill test shall be conducted by the regional offices on need basis at a mutually agreed period. Hyderabad. Kolkata. by the end of the same month in which the application was received and in remaining cases it would be allotted by the second week of the following month. Three examination sessions (February. Kanpur. Ahmedabad and Kochi. 1. Patna.2 An application for allotment of computer number shall be forwarded by the Quality Manager of the approved AMO or Chief Instructor of approved training institute or Engineering in-charge of defence establishment. Computer Number: 1. Candidates shall have the option of changing the category / sub-category in the subsequent examination session. 2. the candidate should have gained minimum six months of further maintenance experience in the related field.1 All basic examinations must be carried out using the multiple choice question format as specified below. 3. 3. 2.2 Duly completed applications on CA Form 19-08 together with the enclosures and fees for appearing in the AME Licence examination shall be forwarded by the Quality Manager of the approved AMO or Chief Instructor of approved training establishment or Engineering In-charge of aircraft maintenance wing of a defence establishment. examination centre and cancellation of candidature are not permitted at any stage of processing the application by DGCA. The Last date for receipt of application for February. 2. examination modules. 15th April and 15th August respectively.4 Candidates scoring less than 35% marks in a particular basic knowledge examination module during two consecutive sessions will not be permitted to appear in the same module during the subsequent session.5 Candidates appearing in AME Licence examinations shall abide by the instructions issued to them by the DGCA 3.4 Penalty marking systems is not used to determine whether a candidate has passed.2 Each multiple choice question must have more than two alternative answers of which only one must be the correct answer and the candidate must be allowed a time per module which is based upon a nominal average of 75 seconds per question. Standardization Basis For Examinations 3. June and October Session are 15th December.3 The pass mark for CAR-66 module and sub-module multiple choice part of the examination is 75%. 3. Page 70 of 175 . iii) For appearing in additional category / sub-category basic knowledge examinations.by G T SELVAN Draft CAR-66 Dated 7th March 2011 months of training in an appropriate stream from an approved Aircraft Maintenance Training Establishment or completed five years of defence service in the capacity of Aircraft Maintenance personnel in the related category / sub-category. Note: Change of category. 2.3 Eligible candidates may appear for a maximum of four basic knowledge examination modules of their choice of the same category / sub-category during a particular session. by G T SELVAN Draft CAR-66 Dated 7th March 2011 3.1. 4. B1. 1 2 Subject Mathematics Physics Category All Categories All Categories A 3 Electrical Fundamentals B1 B2 A 4 Electronic Fundamentals B1 B2 A 5 Digital Techniques/Electronic Instrument Systems B1. Question Numbers and Examination Duration for the CAR-66 Appendix I Modules Module No.B1. except in the case of an approved maintenance training organisation which conducts a course of retraining tailored to the failed subjects in the particular module. the failed module may be retaken after 30 days.5 All CAR-66 modules that make up a complete CAR-66 aircraft maintenance engineer’s licence category or subcategory must be passed within a 5 year time period of passing the first module except in the case specified in paragraph 3.6 The 5 year time period specified in paragraph 3.3 B1.6.4 B2 A 6 Materials and Hardware B1 B2 7 Maintenance Practices A Multiple choice Questions Time allowed (Minutes) Not Applicable Not Applicable 50 50 50 75 75 75 Not Applicable 40 40 30 30 30 70 60 60 60 70 60 60 45 45 45 105 90 90 90 105 Page 71 of 175 .2. A failed module may not be retaken for at least 90 days following the date of the failed module examination following the date of the failed module examination. In such case. 3.5 does not apply to those modules which are common to more than one CAR-66 aircraft maintenance engineer’s licence category or subcategory and which were previously passed as part of another such category or subcategory examination. 3 / B1.4 B2 A 13 Aircraft Aerodynamics.2 B2 A3 / A4 11B 12 Helicopter Aerodynamics. Subject Category B1 B2 A Multiple choice Questions 70 70 30 30 30 30 30 30 40 40 40 100 100 0 100 100 0 100 100 0 0 0 100 0 0 30 Time allowed (Minutes) 105 105 45 45 45 45 45 45 60 60 60 150 150 0 150 150 0 150 150 0 0 0 150 0 0 45 Page 72 of 175 8 Basic Aerodynamics B1 B2 A 9 Human factors B1 B2 A 10 Aviation Legislation B1 B2 11A Turbine Aeroplane Aerodynamics. Structures and Systems B1. Structures and Systems Piston Aeroplane Aerodynamics. Structures and Systems B1 B2 A 14 Propulsion B1 B2 . Structures and Systems A1 B1.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Module No.1 B2 A2 B1. 5. 5. Skill Test 6. Subject Category A Multiple choice Questions 100 100 0 70 70 0 30 30 0 Time allowed (Minutes) 150 150 0 105 105 0 45 45 0 15 Gas Turbine Engine B1 B2 A 16 Piston Engine B1 B2 A 17 Propeller B1 B2 5.1 To appear in skill test conducted by DGCA. 5.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Module No. passed respective aircraft type examination in the preceding two years Page 73 of 175 . a candidate should have passed all the relevant basic knowledge examination pertaining to the category in the preceding five years. 6.1 To appear in a written aircraft type examination conducted by DGCA separately or as a part of approved type training. 5.4 The type examination shall meet the standards stipulated in Appendix III of this CAR.5 The result of type examination shall have a validity of 2 years. a candidate should have i) ii) passed the basic knowledge examinations relevant to the category / subcategory in the preceding five years.2 Duly completed applications on CA form 19-08 for appearing in the Type Examination along with enclosures and fees shall be submitted at least two weeks prior to the mutually agreed date of examination.Type Examination 5.6 Failed candidates may retake the type examination after 30 days from the date of examination. by G T SELVAN Draft CAR-66 Dated 7th March 2011 iii) iv) evidence to prove that aircraft maintenance experience of the relevant type of aircraft covering an acceptable cross section of tasks from Addendum II to AMC had been acquired six months of recent experience on the type of aircraft 6. Such certificate shall be issued within 30 days of receipt of application.1 Results of the written basic knowledge examination will be published on the DGCA website within 30 working days of the last day an examination session. candidates may request the CEO for issuance of a duplicate result sheet. 8. 7. Page 74 of 175 .2 Candidates meeting the above requirements may apply to the respective regional / sub-regional office on CA form 19-09 6.3 The skill test shall be conducted in accordance with Appendix III paragraph 4 and aim at assessing the ability of the candidate to exercise the privileges of the category and subcategory of the licence for which the application has been made. In the event of non-receipt of a result sheet even after 30 days of declaration of result. 6. DGCA on Form CA 19-11 for the issuance of Basic Knowledge Examination Certificate. The pass marks shall be 75%.2 Individual result sheets shall be forwarded to the passed candidates only.4 Failed candidates may reappear in the skill test after 3 months from the date of examination. 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. 7 EXAMINATION RESULTS 7. 7.3 Results of the written aircraft type examination and skill test will be published within a week’s time of the conduct of the examination by the regional airworthiness office. the student will be able to: 1. Identify maintenance practices important to the airframe. 1. the student will be able to identify safety precautions related to the airframe. 4. Page 75 of 175 . Course objectives: In addition to the information contained in the Level 1 General Familiarization course. Type training levels The three levels listed below define the objectives that a particular level of training is intended to achieve. Level 2 Ramp and transit Basic system overview of controls. its systems and powerplant. Level 1 General familiarization A brief overview of the airframe. 3. powerplant and systems. (b) Electrical power supplies. (d) Auxiliary power unit. windows and hatches. 2. principal components including their location and purpose.Type training and Examination Standard 1. Define the general layout of the aircraft's major systems. 2. (c) Fuel. indicators. Identify special tooling and test equipment used with the aircraft. Demonstrate knowledge of the main ramp and transit (through-flight) activities of the following: (a) Doors. Recall the safety precautions to be observed when working on or near the aircraft. at the completion of this Level 2 Ramp and Transit training. 5. Define the general layout and characteristics of the powerplant. its systems and powerplant. Course objectives: Upon completion of the course.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Appendix III . servicing and minor troubleshooting. systems and powerplants as outlined in the Systems Description Section of the Aircraft Maintenance Manual. 7. Oxygen. (j) Flight controls. 5. 6. operation. including terminology and nomenclature. Course objectives: In addition to the information contained in Level 1 and Level 2 training. at the completion of Level III Line and Base Maintenance training. 8. (g) Environmental Control Systems. (n) Avionics. Water/Waste. Explain the normal functioning of each major system.by G T SELVAN Draft CAR-66 Dated 7th March 2011 (e) Powerplant. 4. 3. 9. Locate those procedures for replacement of components for ramp and transit activities identified in objective 2. Demonstrate proficiency in use of crew reports and on-board reporting systems (minor troubleshooting) and determine aircraft airworthiness per the MEL/CDL. component location. (m) Flight and service interphone. Perform the procedures for ramp and transit servicing associated with the aircraft for the following systems: Fuel. Level 3 Line and base maintenance training Detailed description. Identify and use appropriate documentation. (f) Fire protection. (o) Cabin equipment/furnishings. the student will be able to: (a) Perform system. component and functional checks as specified in the maintenance manual. (l) Oxygen. Hydraulics. removal/installation and bite and troubleshooting procedures to maintenance manual level. Identify the locations of the principal components. power availability and sources. Describe systems and aircraft handling particularly access. (k) Water/waste. (h) Hydraulic power. engine. Page 76 of 175 . Power Plants. Landing Gear. (i) Landing gear. by G T SELVAN Draft CAR-66 Dated 7th March 2011 (b) Correlate information for the purpose of making decisions in respect of fault diagnosis and rectification to maintenance manual level. Type training standard Type training must include a theoretical and practical element. all subsequent courses for extension in the same category need only be to level 1 standard. Additional elements introduced due to technological changes shall also be included.1. Training levels are those levels defined in paragraph 1 above. Under the later circumstances the level of training shall be a level lower than the one described below for a B1 Category type course. Theoretical element As a minimum the elements in the Syllabus below that are specific to the aircraft type must be covered. 2. (c) Describe procedures for replacement of components unique to aircraft type. 2. After the first type course for category C certifying staff. Personnel desirous of obtaining Category / Sub-category “A” licence with type rating shall pass appropriate type examination conducted by DGCA or where applicable shall successfully complete an approved type training. Introduction Module Title General Aircraft(dimensions/weights MTOW etc) Time limits/maintenance checks Leveling and weighing Towing and taxiing Parking/mooring Servicing Standard practices-only type particular Fuel tank Safety B2 module-safety items/mechanical interface B1 module-safety items/avionics interface Page 77 of 175 . Operation: Electrical/Flyby-Wire Fuel Systems x x x x x x 3 3 3 3 3 3 3 3 1 3 3 3 3 3 2 3 3 x 3 3 3 3 C x x x x x x 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 Aeroplane Piston B1 x x x x x x 3 3 3 3 3 3 3 3 1 3 3 x x 3 2 3 3 x 3 3 x 3 C x x x x x x 1 1 1 1 1 1 1 1 1 1 1 x x 1 1 1 1 x 1 1 x 1 Helicopter turbine B1 3 3 3 3 3 3 x x x x x x x x 1 3 3 x x 3 2 3 3 x 3 3 x 3 C 1 1 1 1 1 1 x x x x x x x x 1 1 1 x x 1 1 1 1 x 1 1 x 1 Helicopter Piston B1 3 3 3 3 3 3 x x x x x x x x 1 3 3 x x 3 2 3 3 x 3 3 x 3 C 1 1 1 1 1 1 x x x x x x x x 1 1 1 x x 1 1 1 1 x 1 1 x 1 Avionics B2 x x 1 x x x 1 x x x x x x x 1 1 1 1 1 3 3 3 x 3 1 2 3 1 Page 78 of 175 . & Cabin Entertainment Equipment Fire Protection Flight Controls Sys.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Aeroplanes Turbine B1 Blade tracking and vibration analysis Transmissions Airframe structure Main rotor Tail rotor/rotor drive Rotor flight control Airframe Structure Fuselage Doors Fuselage Fuselage Windows Wings Stabilizers Flight Control Surfaces Nacelles/Pylons Zonal & Station Identification Systems Air Supply Air Conditioning Pressurization Safety & Warning Devices Instrument Systems Avionics Systems Electrical Power Equipment & Furnishings Electronic Emergency Equip. Aeroplanes Turbine B1 Hydraulic Power Ice & Rain Protection Landing Gear Lights Oxygen Pneumatic/Vacuum Water/Waste On-board Maintenance Systems Turbine Engines: Constructional arrangement and operation Engine Performance Inlet Compressors Combustion Section Turbine Section Exhaust Bearings and Seals Lubricants and Fuels Lubrication Systems Fuel Systems Engine controls FADEC Air Systems Starting & Ignition Systems Engine Indicating Systems Power Systems Augmentation 3 3 3 3 3 3 3 3 C 1 1 1 1 1 1 1 1 Aeroplane Piston B1 3 3 3 3 3 3 3 3 C 1 1 1 1 1 1 1 1 by G T SELVAN Draft CAR-66 Dated 7th March 2011 Helicopter Helicopter Avionics turbine Piston B1 3 3 3 3 x 3 x x C 1 1 1 1 x 1 x x B1 3 3 3 3 x 3 x x C 1 1 1 1 x 1 x x B2 1 1 1 3 1 1 1 3 x 3 3 3 3 3 3 3 3 3 3 3 2 3 3 3 3 3 x 3 3 x 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 x 1 1 x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x 3 3 3 3 3 3 3 3 3 3 3 2 3 3 3 x x 3 x 3 x 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 x x 1 x 1 x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x 1 1 x x x x x x x x 1 1 3 x x 3 x x x 1 x Page 79 of 175 Turbo-prop Engines Turbo-shaft Engines Auxiliary Power Units (APUs) Powerplant Installation . Exhaust and Cooling Systems Supercharging / Turbocharging Lubricants and Fuels Lubrication Systems Engine Indication Systems Powerplant Installation Engine Monitoring Ground Operation Engine Storage Preservation Propellers: Propeller — General Propeller Construction Propeller Pitch Control Propeller Synchronizing Propeller Electronic control Propeller Ice Protection Propeller Maintenance 3 3 3 3 2 3 3 1 1 1 1 1 1 1 and and x x x x x x x x x x x x x x x x x x x x x x x x x x x x and and 3 3 3 C 1 1 1 Aeroplane Piston B1 x x x C x x x by G T SELVAN Draft CAR-66 Dated 7th March 2011 Helicopter Helicopter Avionics turbine Piston B1 3 3 3 C 1 1 1 B1 x x x C x x x B2 1 x x 3 3 3 3 3 3 1 1 1 1 1 1 x x x x x x x x x x x x 3 3 3 3 3 3 1 1 1 1 1 1 1 1 1 x x x 3 3 3 3 3 3 3 3 1 1 1 1 1 1 1 1 x x x x x x x x x x x x x x x x 3 3 3 3 3 3 3 3 1 1 1 1 1 1 1 1 x x x x x x x x 3 3 3 3 2 3 3 1 1 1 1 1 1 1 x x x x x x x x x x x x x x x x x x x x x x x x x x x x 1 x x x 3 x x Page 80 of 175 .Aeroplanes Turbine B1 Fire Protection Systems Engine Monitoring Ground Operation Engine Storage Preservation Piston Engines: Engine Performance Engine Construction Engine Fuel Systems Carburetors Fuel injection systems Engine controls FADEC Starting and Ignition Systems Induction. Each multiple-choice question must have more than two alternative answers of which only one must be the correct answer. the examination must be written and comply with the following: Format of the examination is of the multiple-choice type. including any on-wing maintenance activity. The competent authority of the DGCA will assess number and level of questions on a sampling basis when approving the course. The time for answering is based upon a nominal average of 120 seconds per level 3 question and 75 seconds per level 1 or 2 question. Page 81 of 175 . for example troubleshooting.by G T SELVAN Draft CAR-66 Dated 7th March 2011 2. The examination must be of the closed book type.2. rigging and functional checks such as engine run. etc. 3. perform removal and replacement of components and modules unique to type. if required. The examination pass mark is 75%. Correctly use specialist/special tooling and test equipment. The number of questions must be at least one question per hour of instruction subject to a minimum of two questions per Syllabus subject. repairs. No reference material is permitted. adjustments. replacements. Practical element The practical training element must consist of the performance of representative maintenance tasks and their assessment in order to meet the following objectives: Ensure safe performance of maintenance. Penalty marking is not to be used to determine whether a candidate has passed. Correctly use all technical literature and documentation for the aircraft. End of module phase examinations cannot be used as part of the final examination unless they contain the correct number and level of questions required. An exception will be made for the case of examining a B1 or B2 candidate's ability to interpret technical documents. Type training examination standard Where aircraft type training is required. inspections and routine work according to the maintenance manual and other relevant instructions and tasks as appropriate for the type of aircraft. Page 82 of 175 . written or practical assessment based. Oral examination questions must be open. Written examination questions must be multiple-choice questions. repairs. Correctly use all technical literature and documentation for the aircraft. A written report must be made by the examiner to explain why the candidate has passed or failed. rigging and functional checks such as engine run. at the indicated level.by G T SELVAN Draft CAR-66 Dated 7th March 2011 4. or a combination thereof. inspections and routine work according to the maintenance manual and other relevant instructions and tasks as appropriate for the type of aircraft. including any on-wing maintenance activity. replacements. adjustments. if required. for example troubleshooting. Examination subjects must be on a sample of subjects drawn from paragraph 2 type training/examination syllabus. Ensure safe performance of maintenance. Type examination standard where type training is not required: The examination must be oral. etc. perform removal and replacement of components and modules unique to type. The examination must ensure that the following objectives are met: Properly discuss with confidence the aircraft and its systems. Practical assessment must determine a person's competence to perform a task. Correctly use specialist/special tooling and test equipment. 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 83 of 175 .by G T SELVAN Draft CAR-66 Dated 7th March 2011 Appendix IV .3 B1.1 B1.1 NONE 6 months 6 months 6 months X 6 months 6 months 6 months 1 year B1.2 B1.Experience requirements for extending a CAR CAR-66 Aircraft Maintenance Engineer’s Licence The table below shows the experience requirements for adding a new category or subcategory to an existing CAR CAR-66 licence.3 6 months 6 months NONE 6 months 6 months 6 months X 6 months 1 year 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 X 6 months 2 years 1 year 2 years 6 months 2 years A4 6 months 6 months 6 months X 2 years 1 years 2 years 6 months 2 years B1.2 6 months NONE 6 months 6 months 2 years X 2 years 6 months 2 years B1. The experience must be practical maintenance experience on an operating aircraft in the subcategory relevant to the application The experience requirement will be reduced by 50 % if the applicant has completed an approved CAR -147 course relevant to the category To: A1 A2 A3 A4 B1. ..66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE DGCA INDIA CA Form 19-01 Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes......………………………………………………… 2................…………………………………………………………… …………………………………………………………………………………………………………………………PIN Code................. B2. B1........... *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...... E-mail……...1.........4....... Fields marked with an asterisk * are mandatory and must be completed in all cases.....B1.....A2........ B1...... C and required type ratings as per addendum I to AMC of CAR – 66) Category/Sub-category of License applied for Mechanical A B 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 examination/ defence experience................2................…………………………………………………...………………....3.....................A3.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Appendix V –Applications and Formats APPLICATION FOR INITIAL ISSUE OF CAR................. E-mail……....... PERSONAL DETAILS CEO Computer No.... *Name in full *Date of birth *Educational Qualification * Nationality * Details of Fees Paid ……………………………………………...........A4.............. …………………………………………………………………………………………………………. *Address for Communication (if different from above)……………………….................................1................ Name of the Current Employer……………………………………………………………………………………………………………………… Contact Phone Number of Employer ………………………........ Page 84 of 175 ...B1.. Applicant Contact Phone Number ………………………….........PIN Code....... Use Date Format – DD-MM-YYYY 1............ Affix recent passport size photo graph duly attested on the front side *Permanent address…………………………………………….....…………………………………………………………………………………………………………………… Examination credit due equivalent exam certificates.. by G T SELVAN Draft CAR-66 Dated 7th March 2011 4. ii) I never had a CAR 66 AMEL issued which was revoked or suspended by DGCA iii) I am not in possession of any other AMEL issued by DGCA. *Details of skill test passed Aircraft Type / Series Date of Exam Name of DGCA office that conducted the test *Relevant certificates/documents required to be submitted as enclosures in Section 7 6. iv) I did not apply earlier to the office of DGCA for issue of my AMEL and the request was not turned down.*DECLARATION I hereby confirm that: i) I apply for initial issue 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.* Details of Type Rating courses certificates Aircraft Type / Series Engine Type course approval details 5b.( Attach additional sheet indicating detail of practical experience obtained in cross representation section of maintenance task as per Addendum II to AMC of CAR 66 ) Date From To Aircraft Engine(s) and Organisation /or Equipment Description of Work 5.* Details of basic knowledge certificate if any issued by CEO/DGCA Category Sub-category Modules Passed 5a. PHYSICAL DISABILITY / DISORDER Known Physical disability or disorder 7. PLACE DATE SIGNATURE NAME Page 85 of 175 . *SUMMARY OF EXPERIENCE . Propeller F.Digital Techniques/ Electronic Systems 6. Materials & Hardwares 7. Module No. instrument Enclosure No.DETAILS OF ENCLOSURES A. Chemistry. course completion certificate and organisation approval certificate. Structures and Systems 12. Electronic Fundamental 5. Turbine Engine Aeroplane Aerodynamics.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Instruction and Checklist CHECKLIST 8. Aircraft Aerodynamics. Aviation Legislation 11A. Propulsion 15. Structures and Systems 14. Piston Engine 17. Electrical Fundamentals 4. Piston Engine Aeroplane Aerodynamics. Roll No. DGCA Remarks Sat/Unsat IV V V (3) V (4) V (5) V (6) V (7) V (8) V (9) V (10) V (11A) V (11B) V (12) V (13) V (14) V (14) V (16) V (17) VI - Page 86 of 175 . Structures and Systems 13. Certified true copy of 10+2 with Physics. Certified true copy of Passport or any photo identity card issued by the Government D. Helicopter Aerodynamics. I II III Enclosure Page No. Certified true copy of Course completion from approved aircraft maintenance training organization / Degree in Engineering certificate is applicable / Defence experience certificate and organisation approval certificate E. Gas Turbine Engine 16. Human Factors 10. passed 3. Structures and Systems 11B. Maintenance Practices 8. Certified true copy proof of Date of Birth certificate B. Mathematics or equivalent C. Type course examination result sheet. Basic Aerodynamics 9. Certified true copies of basic knowledge examination result sheet / certificate if any issued by CEO Session No. licence. Certified true copies of Logbook / Work records on CA form 19-10 I. to a fine of one Lakh Rupees and/or imprisonment for a term not exceeding three months. please refer to CAR-66. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. permission or other document. with intent to deceive. The detail of experience should indicate practical experience obtained in cross representation section of Maintenance task as per Addendum II to AMC of CAR-66.A. issue. Section :8 Assign annexure number as indicated and continuous page numbers to the enclosures and indicate it under column 3 against each item Page 87 of 175 . 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. Certified true copy of skill test result H. renewal or extension of any certificate. on summary conviction. Section :5b Indicate details of Name of the DGCA office conducted the skill test. Medical fitness certificate issued by MBBS doctor on CA form 19-06 J.DETAILS OF ENCLOSURES G.30. Please refer to current notification for details of fees required.A. Section :5Indicate 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. it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentats enclosed. Persons doing so render themselves liable. Section 4: This section is required for DGCA record purposes and should provide a brief summary of experience applicable to your application. approval. any false representations for the purpose of procuring the grant.25 and CAR-66. Completed application with the checklist should be posted along with the required documentation to: The Directorate General of Civil Aviation.by G T SELVAN Draft CAR-66 Dated 7th March 2011 CHECKLIST 8. VII VIII IX Enclosure Page No. In order that DGCA can process the licence application as quickly as possible. 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 Addendum I to AMC of CAR-66 Section 3: credit claimed for exemptions from passing module or experience. You will still need to submit detailed maintenance experience records in addition to this information. 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. Fees Enclosure No. DGCA Remarks Sat/Unsat INSTRUCTION TO CA FORM 19-01 It is an offence to make. Opposite Safdarjung Airport. All original documents submitted will be returned through the self addressed cover affixed with necessary postal stamp (Speed post) provided by the applicant. 2 copies of the recent photographs with the name of the applicant on the back side K. DGCA will not contact you for clarification of details on applications and therefore it is most important that you have the correct information before applying. APPLICATION FOR EXTENSION OF CAR- 66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE by G T SELVAN Draft CAR-66 Dated 7th March 2011 DGCA INDIA 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 *AME LICENCE No. *Fees Paid 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. *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 addendum I to AMC of CAR – 66) Category/Sub-category of License applied for Mechanical A B 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 experience..…………………………………………………………………………………………………………………………………………………. 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 Addendum II to AMC of CAR 66 ) Date From To Aircraft Engine(s) and Organisation /or Equipment Description of Work Page 88 of 175 by G T SELVAN Draft CAR-66 Dated 7th March 2011 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 Aircraft Type / Series Date of Exam Name of DGCA office that conducted 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 AMEL issued which was revoked or suspended by DGCA iii) I am not in possession of any other AMEL issued by DGCA. iv) I did not apply earlier to the office of DGCA for extension of my AMEL and the request was not turned down. PLACE DATE SIGNATURE NAME Page 89 of 175 by G T SELVAN Draft CAR-66 Dated 7th March 2011 INSTRUCTION AND CHECKLIST 8. CHECKLIST TO CA FORM 19-02 DETAILS OF ENCLOSURES A. Original CAR-66 Aircraft Maintenance Engineer’s licence B. Certified true copies of basic knowledge examination result sheet / certificate issued by CEO C. Certified true copy of Passport or any photo identity card issued by the Government Module No Session No. passed Roll No. IV(a) IV(b) IV(c) D. Type course examination result sheet, course completion certificate and organisation approval certificate E. Certified true copy of skill test and oral cum practical examination F. Certified true copies of Logbook / Work records on CA form 19-10 G. Fees V VI Enclosure Enclosure No. Page No. I II III DGCA Remarks Sat/Unsat Page 90 of 175 Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. The detail of experience should indicate practical experience obtained in cross representation section of Maintenance task as per Addendum II to AMC of CAR 66. Section 8: Assign annexure number as indicated and continuous page numbers to the enclosures and indicate it under column 3 against each item Page 91 of 175 . with intent to deceive. DGCA 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. 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 effectively and with less risk of errors or rejections. Please refer to current notification for details of fees required. approval. In order that DGCA can process the licence application as quickly as possible.25 and CAR-66. You will still need to submit detailed maintenance experience records in addition to this information.by G T SELVAN Draft CAR-66 Dated 7th March 2011 INSRUCTION TO CA FORM 19-02 It is an offence to make. 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.A. renewal or extension of any certificate. Persons doing so render themselves liable. to a fine of one Lakh Rupees and/or imprisonment for a term not exceeding three months. any false representations for the purpose of procuring the grant. All original documents submitted will be returned through the self addressed cover affixed with necessary postal stamp (Speed post) provided by the applicant. 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. it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation enclosed.A. licence. Section 5b: Indicate details of Name of the DGCA office conducted the skill test. please refer to CAR-66.30. permission or other document. Section 4: This section is required for DGCA record purposes and should provide a brief summary of experience applicable to your application. 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 Addendum I to AMC of CAR 66 Section 3: credit claimed for exemptions from passing module or experience. on summary conviction. issue. ………………………………………………......66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE by G T SELVAN Draft CAR-66 Dated 7th March 2011 DGCA INDIA CA Form 19-03 Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes.......APPLICATION FOR RENEWAL OF CAR.................. Fields marked with an asterisk * are mandatory and must be completed in all cases............... DETAILS OF REFRESHER COURSE ATTENDED 4.......... Contact Phone Number of Employer ……………………….*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.……………………………………………………………… Expiry Date …………………………………………………………………………………………………………………………PIN Code.. *Relevant certificates/documents required to be submitted as enclosures in Section 5 4..PIN Code................... *SUMMARY OF AERONAUTICAL EXPERIENCE PRECEEDING TWENTY FOUR MONTHS Date From To Organisation Aircraft Description of Work ………………………..... Applicant Contact Phone Number Name of the Current Employer 2....... *Name in full Details of Fees *Permanent address (in case of any change).......... PERSONAL DETAILS AME Licence No................E-mail…….... *APPLICATION I wish to apply for Renewal of CAR-66 Aircraft Maintenance License as indicated and confirm that the information contained in this form was correct at the time of application 3..................... ………………………………………………………………………………………………………….......... …………………………………………………………………………………………………………...........………………........……………………………………………….......... *Address for Communication ………………………....... ii) I never had a CAR 66 AMEL issued which was revoked or suspended by DGCA iii) I did not apply earlier to the any other Page 92 of 175 .............E-mail……...... Use Date Format – DD-MM-YYYY 1.................................... by G T SELVAN Draft CAR-66 Dated 7th March 2011 office of DGCA for renewal of my AMEL and the request was not turned down. Please refer to current notification for details of fees required. Page 93 of 175 . 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 Enclosure Enclosure No. it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation enclosed. All original documents submitted will be returned through the self addressed cover affixed with necessary postal stamp (Speed post) provided by the applicant. renewal or extension of any certificate. issue. with intent to deceive. Persons doing so render themselves liable. to a fine of one Lakh Rupees and/or imprisonment for a term not exceeding three months. 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 DGCA office to renew the licences more effectively and with less risk of errors or rejections. licence. Fee paid It is an offence to make. I II III IV DGCA Remarks Sat/Unsat Section 1: Indicate personal details as required. Section 3: Indicate aircraft maintenance and certification work done during the period. DGCA 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. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. approval. Copies of refresher training corresponding to the previous five years 4. Original CAR 66 Aircraft Maintenance Engineer’s licence 2. on summary conviction. any false representations for the purpose of procuring the grant. In order that DGCA can process the licence application as quickly as possible. permission or other document. Certified true copies of Logbook / Work records for the corresponding period 3. PLACE DATE SIGNATURE NAME INSTRUCTION AND CHECKLIST CHECKLIST TO CA FORM 19-03 DETAILS OF ENCLOSURES 1. Page No. Medical fitness certificate 4. Use Date Format – DD-MM-YYYY .........……………….............. ………………………………………………………………………………………………………….............PIN Code.E-mail……. *2(a) AMELICENCE HELD 2(b) DETAILS OF CAR-66 AME LICENCE APPLIED FOR Category Type Rating Category A/c Type Rating Limitation Code Page 94 of 175 ...………………………………………………………...E-mail……............ Fields marked with an asterisk * are mandatory and must be completed in all cases................................……………………………………………………........ Address for Communication (if different from above)……………………….............. Applicant Contact Phone Number …………………….. Name Date of birth Permanent Address Expiry Date Nationality Computer No........…………………………………………………………… …………………………………………………………………………………………………………………………PIN Code....by G T SELVAN Draft CAR-66 Dated 7th March 2011 APPLICATION FOR CONVERSION/REMOVAL OF LIMITATIONS OF CAR..66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE *1.. Contact Phone Number of Employer……………………….. PERSONAL DETAILS AME Licence No............................................. DGCA INDIA CA Form 19-04 Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Name of the Current Employer ………………………………………………………………………………………………………………................................. DETAILS OF LIMITATION CODE TO BE REVOKED License Held Category Type Rating Limitation Code Examination Module Endorsed Completed *4. SUMMARY OF AERONAUTICAL EXPERIENCE GAINED WITH RESPECT TO THE LIMITATION OF AMEL Date From To Organisation Aircraft Description of Work 5.by G T SELVAN Draft CAR-66 Dated 7th March 2011 *2(a) AMELICENCE HELD 2(b) DETAILS OF CAR-66 AME LICENCE APPLIED FOR Category Type Rating Category A/c Type Rating Limitation Code *3. PLACE DATE SIGNATURE NAME Page 95 of 175 .DECLARATION I hereby confirm that: i) I apply for Conversion/Removal of limitation as indicated and confirm that the information contained in this form was correct at the time of application. licence. In order that DGCA can process the licence application as quickly as possible. issue. and should detail aircraft types by airframe/engine combination. any false representations for the purpose of procuring the grant. I II III IV V VI VII DGCA Remarks Sat/Unsat Instruction to complete CA Form 19-04 It is an offence to make. Two copies of passport size photograph duly attested on its back side. Original Pre . 6. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. renewal or extension of any certificate. Please enter the limitation (s) in the appropriate column. All original documents submitted will be returned through the self addressed cover affixed with necessary postal stamp (Speed post) provided by the applicant. Enclosure Enclosure No. 2.. to a fine of one Lakh Rupees and/or imprisonment for a term not exceeding three months. 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.CAR 66 AME licence. it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation enclosed. Page No. Type course completion certificate. 5. Enter only one airframe/engine per line. Persons doing so render themselves liable. Certified true copies of Logbook / Work records as applicable. Copy of skill test result relating to the limitation of the licence 7. Section 4: Provide details of experience gained corresponding to the limitation code & aircraft type Page 96 of 175 . Certified true copies of documentary evidence of experience. on summary conviction.by G T SELVAN Draft CAR-66 Dated 7th March 2011 INSTRUCTION AND CHECKLIST CHECKLIST TO CA FORM 19-04 DOCUMENTS ENCLOSED 1. 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. 4. (for conversion) 3. skill test (where applicable). Opposite Safdarjung Airport. permission or other document. with intent to deceive. Completed application with the checklist should be posted along with the required documentation to: The Directorate General of Civil Aviation. Section 3: This section should be used if applying for the removal of limitation(s) from type rating(s). DGCA will not contact you for clarification of details on applications and therefore it is most important that you have the correct information before applying. approval. Certified true copies of Knowledge Examination modules (where applicable) result sheets/ certificates. where applicable. ..PIN Code.. *Permanent address ........ Use Date Format – DD-MM-YYYY 1. ………………………………………………………………………………………………………….......... PERSONAL DETAILS *Name in full AME Licence No..........E-mail…….………………………………………………… If the licence was lost provide a brief account of circumstances under which the licence was lost: 4........ Fields marked with an asterisk * are mandatory and must be completed in all cases.66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE DGCA INDIA CA Form 19-05 Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes... 3....... *Reason for issue of duplicate AMEL( Mark √ as applicable) LOST MUTILATED ………………….by G T SELVAN Draft CAR-66 Dated 7th March 2011 APPLICATION FOR ISSUE OF DUPLICATE CAR.....…………………………………………………………… …………………………………………………………………………………………………………………………PIN Code......... Applicant Contact Phone Number Name of the Current Employer 2.E-mail…….................. Contact Phone Number of Employer ………………………...………………........................*DECLARATION I hereby confirm that: i) I apply for issue of duplicate CAR-66 Aircraft Maintenance Engineer’s Licence as indicated and confirm that the information contained in this form is correct at the time of application...……………………………………………………. *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........ *Address for Communication (if different from above)………………………........................ PLACE DATE SIGNATURE NAME Page 97 of 175 ............... …………………………………………………………………………………………………………................. ii) My CAR 66 AMEL 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 AMEL and the request was not turned down....................... Details of fee paid as per Rule 62 I II III IV V Please refer to current notification for details of fees required. Directorate General of Civil Aviation. 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. Copy of AMEL if available in case of loss 4. Two copy of recent photograph 5. PHOTOGRAPH AND FEE ENCLOSURES Enclosure No.. New Delhi 110003. Copy of FIR lodged with the police station in case of loss of AMEL 3. In order that Licensing & Training Standards can process your licence application as quickly as possible. Completed application should be posted along with the required documentation to: Licensing & Training Standards. Notes: Having clear concise supporting data will enable Licensing & Training Standards to issue licences more effectively and with less risk of errors or rejections. All original documents submitted will be returned through the self addressed cover affixed with necessary postal stamp ( for speed post) . Instruction on how to complete CAR-66 Licence issue of duplicate Application Form (CA Form 19-05).DETAILS OF DOCUMENTS. it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation submitted. Tick Mark DGCA Remarks 1. Page 98 of 175 . Section 3: Tick whether the AMEL is lost or mutilated Section 4: By signing the declaration you are confirming that all of the information is correct and true.by G T SELVAN Draft CAR-66 Dated 7th March 2011 5. Opposite Safdarjung Airport.Original Mutilated AMEL or Affidavit duly notarized by Authorized notary in case of loss of AMEL 2. Please note failure 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. Section 2: Indicate what type of licence you are applying for. Dr.. (1) Pseudo – Isochromatic plates (2) Approved Lantern test (3) Any other test applicable ( Strikeout whichever is not applicable) Signature of the Doctor………………………………. / Ms _________________________ whose signature is appended below. He/She has …………………………………………………………………………………………………………………………………………. and certify that his colour vision is Normal/Defective safe/Defective unsafe. Designation Signature of the Applicant with date Date Page 99 of 175 . Registration No. /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. _______________________ hereby certify that I have examined Mr. Designation Signature of the Applicant with date Date MEDICAL CERTIFICATE FOR COLOUR VISION I. He/She has been assessed medically fit / unfit to function as an Aircraft Maintenance Engineer.by G T SELVAN Draft CAR-66 Dated 7th March 2011 MEDICAL CERTIFICATE (To be provided by a Registered Medical Practitioner holding at least MBBS) DGCA INDIA CA Form 19-06 Mr. The colour vision has been tested with. ( Strikeout whichever is not applicable) Signature of the Doctor……………………………….………… physical disabilities or disorder / no physical disabilities or disorder. Registration No. ............. .by G T SELVAN Draft CAR-66 Dated 7th March 2011 DGCA INDIA APPLICATION FOR ALLOTMENT OF COMPUTER NUMBER CA Form 19-07 FOR APPEARING IN AME LICENCE EXAMINATIONS Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes....... ………………………………………………………………………………………………………….. E-mail……...………………………………………….................. E-mail……....................... *Address for Communication (if different from above)………………………..*PERSONAL DETAILS FIRST NAME MIDDLE NAME SURNAME …………………………………. Fields marked with an asterisk * are mandatory and must be completed in all cases... * AIRCRAFT MAINTENANCE EXPERIENCE / DURATION OF STUDY IN AN APPROVED TRAINING ESTABLISHMENT Maintenance Organization/ Approved Institute Type of aircraft/ engine/ system Duration From To Period in months Page 100 of 175 ......................................………………......... Chemistry & Mathematics 2....…………………………………………..... Use Date Format – DD-MM-YYYY Paste recent passport size photograph (WITHOUT ATTESTATION) (attested partly covering photograph & Page of this application) Paste recent passport size photograph * FOR OFFICE USE .……………………… Employer/ Training School Contact Phone Number …………...... *Applicant Contact Phone Number …………...........Computer Number Allotted (Allotment of Computer Number does not indicate the acceptance of the applicant’s candidature in Basic Knowledge Examination) E1...PIN Code...............………………………………………………………............. SIGNATURE *Name in full *Date of Birth *Permanent address * Nationality SEX (Male/ Female) Fathers Name …………………………………………………………………………………………………………………………………PIN Code....................... *Subject studied and Name of the Year of Passing Details of the School passed in 10+2 or Education Board equivalent Physics... any false representations for the purpose of procuring the grant. my candidature shall be rejected and further action can be taken against me by DGCA as deemed fit. DATE: PLACE: (SEAL OF ORGANISATION) SIGNATURE………………………………………………………………… NAME …………………………………………………………………. Instruction to complete application for allotment of computer No. / Ms ___________________________ has been verified by me and found correct. it renders the person permanently ineligible to have an Aircraft Maintenance Engineer’s Licence. renewal or variation of any certificate. Designation………………………………………………………………… Enclosure No. Certified true copy proof of Date of Birth certificate 2. with intent to deceive. for appearing in CAR-66 basic knowledge examination (CA Form 19-07).by G T SELVAN Draft CAR-66 Dated 7th March 2011 3.*DETAILS OF DOCUMENTS. I declare that I have read and understood the INSTRUCTIONS. on summary conviction. *CERTIFICATE [To be certified by QM/ CI/ Chief Engg. In order that CEO can process your licence application as quickly as possible. Mathematics or II equivalent 3. Certified true copy of Passport or any photo identity card issued by the III Government 4. Failure to submit a correctly completed application form and the required documentation will lead to the rejection of your application. Certified true copy of Course completion from AME institute/ Degree in IV Engineering certificate is applicable Completed application should be posted along with the required documentation to the Central Examination Organisation. I Tick Mark DGCA Remarks 4. East block II. Chemistry. PLACE DATE SIGNATURE NAME It is an offence to make. *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. O/o the Directorate General of Civil Aviation. PHOTOGRAPH AND FEE ENCLOSURES 1. issue. Further. I understand that if any of my particulars/ entries are found false or incorrect before or after the examination. permission or other document. R K Puram. Page 101 of 175 . Further. licence. New Delhi 110066. approval. Officer(in case of serving defence candidates)] It is certified that the particulars claimed by Mr. it is important that all sections marked with an asterisk on the application form are completed and the required supporting documents submitted. Certified true copy of 10+2 with Physics. to a fine of one Lakh Rupees and/or imprisonment for a term not exceeding three months. Persons doing so render themselves liable. Digital Techniques/ Electronic instrument Systems 6. Turbine Engine Aeroplane Aerodynamics. Gas Turbine Engine Page 102 of 175 . Propulsion 15.4 B2 3. Electrical Fundamentals 4. Structures and Systems 13. Aircraft Aerodynamics.2 B1. Materials & Hardwares 7. Date of Issue ENAME: FIRST NAME MIDDLE NAME SURNAME *CATEGORY/ SUB-CATEGORY OF EXAMINATION (Tick appropriate box(s) Category A Aeroplane Turbine A1 Aeroplane Piston Helicopter Turbine Helicopter Piston Avionic A2 A3 A4 B B1. *EXAMINATION PAPERS (Please tick box(es) against the module(s) you wish to take at this examination) Module 3. Structures and Systems 12.1 B1. Maintenance Practices 8.*PERSONAL DETAILS COMPUTER NO: EXAMINATION SESSION & CENTRE MONTH YEAR CENTRE Demand Draft/ Banker’s Cheque No.3 B1.) Name of Bank 2.by G T SELVAN Draft CAR-66 Dated 7th March 2011 DGCA INDIA APPLICATION FOR APPEARING IN WRITTEN PAPER(S) OF CA Form 19-08 CAR 66 BASIC KNOWLEDGE EXAMINATION Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Basic Aerodynamics Module 11A. Piston Engine Aeroplane Aerodynamics. Fields marked with an asterisk * are mandatory and must be completed in all cases. Structures and Systems 11B. Structures and Systems 14. Use Date Format – DD-MM-YYYY 1. Electronic Fundamental 5.* FEE DEAILS: Amount (in Rs. Helicopter Aerodynamics. Human Factors 10. Aviation Legislation by G T SELVAN Draft CAR-66 Dated 7th March 2011 16. Propeller 4. Page 103 of 175 .* 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. *CERTIFICATE [To be certified by QM/ CI/ Chief Engg. to a fine of one Lakh Rupees and/or imprisonment for a term not exceeding three months. I understand that if any of my particulars/ entries are found false or incorrect before or after the examination. PLACE DATE SIGNATURE NAME It is an offence to make. Persons doing so render themselves liable. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. permission or other document. any false representations for the purpose of procuring the grant. Further. 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.9. / Ms ___________________________ has been verified by me and found correct. Officer(in case of serving defence candidates)] It is certified that the particulars claimed by Mr. issue. approval. renewal or variation of any certificate. SIGNATURE NAME Designation DATE: (SEAL OF ORGANISATION) Instruction to complete application form for CAR-66 AMEL Knowledge (written) examination (CA Form 19-08). on summary conviction. my candidature shall be rejected and further action can be taken against me by DGCA as deemed fit. licence. I declare that I have read and understood the INSTRUCTIONS. Please note failure 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. * DETAILS OF AERONAUTICAL ENGINEERING EXPERIENCE: Type of aircraft/ engine/ system Organization/ Approved Institute Area or Work Duration From To Period in months 5. with intent to deceive. Piston Engine 17. Fields marked with an asterisk * are mandatory and must be completed in all cases. ( If held) SURNAME AMEL RTR 2. *DETAILS OF PREVIOUS SKILL TEST (For the same Airframe and Engine combination): AIRCRAFT TYPE DATE of EXAMINATION CENTRE CAT/ SUB-CAT Page 104 of 175 . Use Date Format – DD-MM-YYYY Roll Number Allotted 1.APPLICATION FOR APPEARING IN SKILL TEST OF CAR-66 AME LICENCE by G T SELVAN Draft CAR-66 Dated 7th March 2011 DGCA INDIA CA Form 19-09 Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes.*DETAILS OF SKILL TEST APPLIED FOR: CAT/ SUB-CAT AIRCRAFT TYPE EXAMINATION CENTRE 3. E Licence No. DETAILS OF LICENCE HELD ( If held) CAT/ SUB-CAT AIRCRAFT TYPE CAT/ SUB-CAT AIRCRAFT TYPE 3.*PERSONAL DETAILS FIRST NAME MIDDLE NAME COMPUTER No. *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.*EXAMINATION MODULE(S) passed relevant to Cat/ Sub-Cat applied for ) Module Session Module Session Module Session 5. I declare that I have read and understood the INSTRUCTIONS. SIGNATURE PLACE DATE NAME Page 105 of 175 . Name of Bank 8.*DETAILS OF SPECIFIC PAPER / OF TYPE COURSE PASSED: CAT/ SUB-CAT AIRCRAFT TYPE SESSION / Name of the Approved Organisation Level of the Course MARKS secured RESULT 6. I understand that if any of my particulars/ entries are found false or incorrect before or after the examination. * DETAILS OF AIRCRAFT TYPE MAINTENANCE EXPERIENCE Type of aircraft/ engine/ system Duration Organization Area or Work From To Period in months 7. Further. my candidature shall be rejected and further action can be taken against me by DGCA as deemed fit. *FEE DEAILS: Fees Date of Issue ROLL NUMNER ALLOTED Demand Draft/ Banker’s Cheque No.by G T SELVAN Draft CAR-66 Dated 7th March 2011 4. Propulsion 15. Piston Engine 17. Structures and Systems 12. Aircraft Aerodynamics. Human Factors 10. Structures and Systems 14. Session No. Maintenance Practices 8. Electrical Fundamentals 4. I(1) I(2) I(3) I(4) I(5) I(6) I(7) I(8) I(9) I(10) I(11) I(12) I(13) I(14) I(15) I(16) II III IV Page 106 of 175 . Piston Engine Aeroplane Aerodynamics. Basic Aerodynamics 9. and Paper 3. Structures and Systems 13. passed by G T SELVAN Draft CAR-66 Dated 7th March 2011 Enclosure Tick DGCA No Mark Remarks I Module No. Turbine Engine Aeroplane Aerodynamics.Digital Techniques/ Electronic instrument Systems 6. Materials & Hardwares 7. Aviation Legislation 11A.9. Structures and Systems 11B. Details of DGCA Examinations passed. Electronic Fundamental 5. Certified true copy of skill test result 4. Propeller 2. Helicopter Aerodynamics. Type course completion certificate with examination result sheet 3. Gas Turbine Engine 16.*DETAILS OF ENCLOSURES 1. Certified true copies of Logbook / Work records on CA Form 19-10 Roll No. Completed application should be posted along with the required documentation to the respective regional / sub-regional office . Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. 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. licence. Page 107 of 175 . Persons doing so render themselves liable. issue.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Please refer to current notification for details of fees required. any false representations for the purpose of procuring the grant. to a fine of one Lakh Rupees and/or imprisonment for a term not exceeding three months. It is an offence to make. All original documents submitted will be returned through the self addressed cover affixed with necessary postal stamp ( for speed post) . Notes: Having clear concise supporting data will enable regional office to process the application more effectively and with less risk of errors or rejections. on summary conviction. permission or other document. with intent to deceive. renewal or variation of any certificate. approval. Failure to submit a correctly completed application form and the required documentation will lead to the rejection of your application and fee submitted would be utilized for processing the application. by G T SELVAN Draft CAR-66 Dated 7th March 2011 FOR OFFICIAL USE NAME OF CANDIDATE CAT/ SUB-CAT Candidate was examined on the following topics: ROLL NUMBER AIRCRAFT TYPE 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 Examination Board Name: Date: (Signature) Member of Examination Board Name: Date: (Signature) Member of Examination Board Name: Date: Page 108 of 175 . .....by G T SELVAN Draft CAR-66 Dated 7th March 2011 DGCA INDIA FORMAT OF AIRCRAFT MAINTENACE ENGINEER WORK RECORD / LOG BOOK CA Form 19-10 1.. Changed Address for Communication: Applicant Contact Phone Number …………………………............................... Name of the Current Employer……………………………………………………………………………………………………………………… Contact Phone Number of Employer ………………………... E-mail…….. Page 109 of 175 ......…………………………………………………. Affix recent passport size photo graph duly attested on the front side Address……………………………………………........................................ *Name in full *Date of birth *Educational Qualification *Permanent GENDER * Nationality M/F AMEL No............................... E-mail…….....PIN Code...... Changed Permanent Address *Address for Communication (if different from above)………………………... Signature ……………………………….....………………………………………………… Log Book Owners Name………………………………………………………………………..………………. PERSONAL DETAILS CEO Computer No..... ………………………………………………………………………………………………………….................................…………………………………………………………… …………………………………………………………………………………………………………………………PIN Code.................. by G T SELVAN Draft CAR-66 Dated 7th March 2011 2. Record of Training: Training Completed Training Establishment and Location From To Result Page 110 of 175 . 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 111 of 175 . 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) .by G T SELVAN Draft CAR-66 Dated 7th March 2011 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). Persons doing so render themselves liable. Aircraft Reg. with intent to deceive. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. Page 112 of 175 . approval. on summary conviction. to a fine of one Lakh Rupees and/or imprisonment for a term not exceeding three months. ACCESSOY GEAR BOX c. renewal or variation of any certificate. PLACE DATE SIGNATURE NAME It is an offence to make. *Check Chip detector Organization (4) All the applicable aircraft maintenance tasks listed under Addendum II to AMC of CAR-66 should be reproduced under column (1). any false representations for the purpose of procuring the grant. Details of tasks performed should be furnished under column 2.by G T SELVAN Draft CAR-66 Dated 7th March 2011 4.*DECLARATION I hereby confirm that the information contained in this form was correct at the time of application. permission or other document. 4 and 5 Maintenance tasks not performed should be indicated as “ NOT PERFORMED” 5. licence.BASIC SKILL Supervisor Name and AMEL No. Date on which *Typical Maintenance Tasks CATEGORY No & Type (2) performed (3) (1) I. issue. Time limit/ Maintenance # # LV. 3. ................by G T SELVAN Draft CAR-66 Dated 7th March 2011 APPLICATION FOR ISSUE OF BASIC KNOWLEDGE EXAMINATION CERTIFICATE DGCA INDIA CA Form 19-11 Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes............. *Name in full *Permanent address ........…………………………………………………… 2.....E-mail……............. *PERSONAL DETAILS CEO Computer No....................... *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 required category / subcategory of basic knowledge certificate) Category/Sub-category of License applied for Mechanical Avionic A B Page 113 of 175 .....E-mail……..…………………………………………………………… …………………………………………………………………………………………………………………………PIN Code..……………………………………………………… Name of the Current Employer………………………………………………………………………………………………………………………......................... Fields marked with an asterisk * are mandatory and must be completed in all cases............... Contact Phone Number of Employer ………………………... *Address for Communication (if different from above)………………………................PIN Code...………………....... …………………………………………………………………………………………………………..................... Use Date Format – DD-MM-YYYY 1. Applicant Contact Phone Number ………………………................... licence. Exam Session in which Passed 4 *FEE DEAILS: Fees Date of Issue 5. permission or other document. issue. renewal or variation of any certificate. Persons doing so render themselves liable. Name of Bank DATE NAME It is an offence to make. to a fine of one Lakh Rupees and/or imprisonment for a term not exceeding three months. with intent to deceive. Exam Session in which Passed Category/subcategory Module No. any false representations for the purpose of procuring the grant.by G T SELVAN Draft CAR-66 Dated 7th March 2011 3. *Details of basic modules/papers relevant to modules passed Category/subcategory Module No.*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. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence. approval. Page 114 of 175 . PLACE SIGNATURE Demand Draft/ Banker’s Cheque No. on summary conviction. Mark Remarks I Roll No.*DETAILS OF DOCUMENTS. Aviation Legislation 11A. Electronic Fundamental 5. Materials & Hardwares I (d) 7. Basic Aerodynamics I (f) 9. Maintenance Practices I (e) 8. Aircraft Aerodynamics.Digital Systems Techniques/ Electronic instrument I (b) I (c) 6.Turbine Engine Aeroplane Aerodynamics. Electrical Fundamentals I (a) 4. Piston Engine Aeroplane Aerodynamics. Propulsion I (m) Page 115 of 175 . Human Factors I (g) 10. Structures and System 11B. passed by G T SELVAN Draft CAR-66 Dated 7th March 2011 Enclosure Tick DGCA No. 3. Structures and Systems 13. Structures and Systems I (h) I (i) I (j) I (k) I (l) 14. Helicopter Aerodynamics.5. PHOTOGRAPH AND FEE ENCLOSURES Details of DGCA Examinations passed : Module No. Structures and Systems 12. and Paper Session No. New Delhi 110066.by G T SELVAN Draft CAR-66 Dated 7th March 2011 15. Completed application should be posted along with the required documentation to the Central Examination Organisation. R K Puram. All original documents submitted will be returned through the self addressed cover affixed with necessary postal stamp (for speed post). Page 116 of 175 . 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. Propeller I (p) Please refer to current notification for details of fees required. Notes: Having clear concise supporting data will CEO to issue licences more effectively and with less risk of errors or rejections. Gas Turbine Engine I (n) 16. Piston Engine I (o) 17. O/o the Directorate General of Civil Aviation. East block II. 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. ..2011 (for the Director General of Civil Aviation Aviation) Stamp of the Issuing Authority : X... This licence when endorsed with an aircraft type rating meets the intent of ICAO Annex 1 g...... Page 117 of 175 ..... GOVERNMENT OF INDIA DIRECTORATE GENERAL OF CIVIL AVIATION Aircraft Maintenance Engineer’s Licence Licence number Name of holder in full STAMP SIZE PHOTO IX.... Date of Issue: . 1937 . Endorsement of aircraft types on the page (s) entitled LICENCE (SUB) CATEGORIES means the holder is qualified to issue a certificate of release to service for such aircraft from the date of endorsement in conjunction with a valid approved maintenance organisation’s organ authorisation or so authorized by the Director General. powerplant....by G T SELVAN Draft CAR-66 Dated 7th March 2011 Appendix VI ..Aircraft Maintenance Engineer’s Licence referred to in Rule 61 of The the Aircraft Rules. III. Date of birth Address of holder VI... 1937 subject to complying with the said rule and the licence holder is familiar with all the relevant information relating to the maintenance and airworthiness of the particular aircraft for which the licence holder is signing a aft Maintenance Release.. XI. e. . VII.... (c) whilst in compliance with the Aircraft Rule 61 and CAR-66 unless previously suspended or revoked. Nationality Signature of Holder …………………………………………………..... 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 render him/her una unable to safely and properly exercise these privileges............ c. CONDITIONS a. Signature of Issuing Authority .. endorsement or alteration in the licence shall be made by any person not specially authorized for this purpose by the Director purpo General III... or such airframe.... This licence remains current until the expiry date specified at item XIV. b... No entry. II.. 2 IVa. Certified that the holder is authorized to exercise the privileges of the licence as given in Rule 61 of the Aircraft Rules. Issued in accordance with the provisions of the Aircraft Act 1934.. VIII..LIC No.. the Aircraft Rules 1937 for the time being in force and in conformity with ICAO Annex 1 to the convention on International Civil Aviation signed on 7th December 1944.. V... f.CA Form 26 GOVERNMENT OF INDIA DIRECTORATE GENERAL OF CIVIL AVIATION CAR-66 AIRCRAFT MAINTENANCE ENGINEER’s LICENCE I... This licence is not valid unless it bears the signature of the holder... d..... aircraft system or component and aircraft avionic system or component which the licence holder is certifying as being airworthy.. IV. AIRCARFT TYPE RATING A/c TYPE OR GROUP CATEGORY STAMP & DATE XII.1 A1.3 B1.4 B2 C III. AIRCARFT TYPE RATING A/c TYPE OR GROUP CATEGORY STAMP & DATE III.2 B1.LIC No. 4 A A1.4 B1. LICENCE (SUB) CATEGORIES CATEGORIES AEROPLANES TURBINE AEROPLANES PISTON AEROPLANES TURBINE AEROPLANES PISTON HELICOPTERS TURBINE HELICOPTERS PISTON HELICOPTERS TURBINE HELICOPTERS PISTON AVIONICS AIRCRAFT III.1 B1. 6 Page 118 of 175 .LIC No. AIRCARFT TYPE RATING A/c TYPE OR GROUP CATEGORY STAMP & DATE XII. LIC No.3 A1. 3 A1.: 5 III.LIC No.by G T SELVAN Draft CAR-66 Dated 7th March 2011 XII.2 B1 B2 C DATE XII. : 7 III.: 10 Page 119 of 175 . 8 XIV. ANNEXURE TO THE LICENCE PRIVILEGES INHERITED FROM THE AME LICENCE HELD PRIOR TO CAR-66 LICENCE III. LIC No. LIMITATIONS A/c TYPE OR GROUP Category Limitation Code Signature with Date [Removal of limitation] XIV. LIC No.by G T SELVAN Draft CAR-66 Dated 7th March 2011 XIII. LICENCE VALIDITY DATE OF EXPIRY SIGNATURE WITH DATE SEAL III.: 9 III.LIC No. LICENCE VALIDITY DATE OF EXPIRY SIGNATURE WITH DATE SEAL XIV. LIC No. 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 ensuring that no unauthorized entries are made. 1937 . Each page issued shall be in this format and contain the specified information for that page. 6. 4. If there are no limitations applicable.by G T SELVAN Draft CAR-66 Dated 7th March 2011 1. DGCA may choose not to issue the licence until the first aircraft type rating needs to be endorsed. 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 and may result in prosecution under relevant Indian Penal Code. 3. Page 120 of 175 . the LIMITATIONS page will be issued stating ‘No limitations’. The Annex to CA Form 26 is optional and may only be used to include Privileges not covered by Rule 61. where such privileges were covered by the regulation in force prior to the implementation of Rule 61 of the Aircraft Rules. 2. 5. With regard to the aircraft type rating page. Training and Skill Test pertaining to the imposed limitation(s). To remove limitations imposed on CAR-66 licence. 2. 7.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Appendix VII Conversion of AME Licence Issued Prior to the CAR-66 Coming Into Force 1. The “Table 2 & 3” also establish the credits that can be claimed by the Basic Aircraft Maintenance Engineer’s Licence / Basic Aircraft Maintenance Engineer Certificate or those who had passed all the basic knowledge examination of a particular stream (Paper I. New Delhi-110003. Applicants desirous of converting the AME licence held by them to CAR-66 Licence shall meet the requirements specified in the corresponding ‘Table 1’ of this appendix. 5. Opposite Safdarjung Airport. CAR 66. 3. 8. Basic Aircraft Maintenance Engineer’s Licence / Basic Aircraft Maintenance Engineer Certificate shall not be converted. Paper II and Paper III) of erstwhile AME licence qualifying system. The conversion process will confer the privileges exercised by an AME Licence holder prior to the introduction of CAR66. 4.70 has provision for conversion of an existing Aircraft Maintenance Engineer’s Licence into a CAR-66 Aircraft Maintenance Engineer Licence (CAR. Experience. All existing Type rated AME Licences shall be converted into either full or restricted CAR-66 AMEL depending upon the type ratings already endorsed on these Licences. the converted Licence would be issued with “Limitation(s)”. 6. The limitation (s) shall be removed after the applicant has fully met the requirements of Knowledge Examination.A.66 AMEL). Knowledge Examination Modules which are deemed to have been covered by virtue of existing Licence held by the AME and those required to be covered to meet the requirements of CAR-66 AMEL are given in “Table 2” and “Table 3” in respect of Category B1 and B2 respectively. Where an applicant does not meet full requirements of “Table 2” or “Table 3”. where protected rights do not directly convert to a full CAR-66 Category/sub-category licence. Applications to remove limitations on a basic Category/ sub-category Page 121 of 175 . No fee will be charged for conversion of old Licences into new format. Paper II and Paper III of a particular stream of the erstwhile AME licence qualifying system shall not be awarded. Holders of type rated AME licence may apply on CA Form 19-04 with suitable evidences for conversion of their AME licence to a CAR-66 AMEL to the Director General of Civil Aviation (Attention: Airworthiness Directorate). the relevant conversion module examinations must be passed and appropriate experience requirements as in addendum II to AMC of CAR-66 are met. Credit for passing of one or two papers amongst Paper I. by G T SELVAN Draft CAR-66 Dated 7th March 2011 must cover all the limitations. Knowledge Paper Modules/sub modules required to be completed for removing these limitation(s) are specified in “Table 4”. Codes pertaining to Limitations endorsed on the converted Licences are detailed in “Table 5”. 9. To receive the full certification privileges exercised by the AME prior to the CAR-66 coming into force, the applicants are required to provide full details of type endorsement held and privileges exercised by them in the application form along with supporting documentary evidences. Categories/ Ratings held on the existing Licences will be transferred with or without limitation under appropriate category or Section XIV(b) of the CAR-66 licence. 10. Endorsements of Type Ratings in existing “A” “B”,”D” and “X” Category of Licences covering Gliders, Balloons, Aircraft, Engine, Propeller and items of equipment that are not covered by CAR-66, shall be transferred to Section XIV(b) of the “CAR 66 AMEL” along with privileges to issue CRS. 11. Licences with open rating shall be converted with appropriate group rating provided the holder of such licence produces suitable evidence of having exercised the licence privileges on various aircraft types. Otherwise, the open rated AME licence will be converted to a CAR-66 licence conferring the privileges exercised by the AME in the past on specific aircraft 12. Endorsements of Type Ratings in respect of obsolete types of aircraft not listed in the CAR66 will not be transferred to the new Licence. However, to recognize such qualification, the same shall be recorded in Column XIV(b) of new Licence indicating that the holder had these Type Ratings endorsed in his earlier Licence. 13. Cutoff date for conversion of the existing Licences is 31st December 2012. All existing Licence holders will continue to exercise the privileges of old Licences until this cutoff date, after which they will cease to hold the privileges unless converted into CAR66 AMEL. However, there is no time limit for removal of limitations on converted Licences. 14. Once an AME Licence is converted into a CAR-66 AMEL and the Ratings, Limitations and Privileges on the new Licences are accepted by the holder, previously held AME Licence will be rendered invalid. All CAR-66 Licences shall be deemed to have been accepted by the applicant, if no written objection is received by the DGCA within one month of the date of its receipt. Page 122 of 175 by G T SELVAN Draft CAR-66 Dated 7th March 2011 REQUIREMENTS FOR ISSUE OF CAR-66 LICENSE BASIC KNOWLEDGE EXAMINATION MODULES Category Description 3 4 5 6 7 8 9 10 11A 11B 12 13 14 15 16 17 TABLE - 1 Practical Maintenance experience Type Training Ref. : CAR 66 Appendix III/ Addendum II to AMC of CAR-66 A1 A2 A A3 A4 B1.2 B1.4 B1 B1.1 B1.3 B2 Aeroplanes Piston Helicopters Turbines Helicopters Piston Aeroplanes Piston Helicopters Piston Aeroplanes Turbines Helicopters Turbines Avionics X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X 4 years/3 Years as per para (a) 1 of CAR 66.A.30 Aeroplanes Turbines X X X X X X X X X X C 5 years 5 years/ 4 /3 Years as per Years as per para para (a)(3) of CAR (a) (2) of CAR 66.A.30** 66.A.30 X ** For Large Aircraft (i) 3 years of experience in exercising category B1.1, B1.3 or B2 privileges on Large Aircraft or as support staff in base maintenance or a combination of both OR (ii) 5 years of experience in exercising B1.2 or B1.4 privileges on Large Aircraft or as support staff in base Maintenance or a combination of both. For Non Large Aircraft 3 years of experience category B1 or B2 privileges on Non Large Aircraft or as support staff in base maintenance or a combination of both. Note : The above experience shall include 12 months of Recent Experience as B1 or B2 Base Maintenance support staff. Page 123 of 175 SKILL TEST by G T SELVAN Draft CAR-66 Dated 7th March 2011 KNOWLEDGE EXAMINATION MODULES WHICH ARE DEEMED TO HAVE BEEN COVERED BY VIRTUE OF EXISTING LICENCE – CATEGORY B1 B1.1 - Aeroplanes - Turbine Pre- CAR 66 Licence Cat “A” & “C” (Heavy Aircraft & Jet Engine) Modules deemed Covered 3 3,4,5,6,7,8,9,10, 11A, 15,17 X 4 X 5 X 6 X 7 X 8 X Modules Required 9 X 10 X 11A 11B 12 X 13 TABLE - 2 14 15 X 16 17 X Cat “A” & “C” (Light Aircraft & Jet Engine) Cat “A” (Heavy Aircraft) Cat “C” (Jet Engine) 3,4,5,6,7,8,9,10, 11B, 15,17 3,4,5,6,7,8,9,10, 11A 3,4,5,6,7,9, 10,15, 17 X X X X X X X X F X X X X X X X X X X X X X X F X X X X X F F X F X B1.2 - Aeroplanes - Piston Cat “A” & “C” 3,4,5,6,7,8,9,10, (Light Aircraft 11B,16,17 & Piston Engine) Cat “A” 3,4,5,6,7,8,9,10, (Light 11B Aircraft) Cat “C” 3,4,5,6,7,9,10,16,17 (Piston Engine) B1.3 - Helicopter - Turbine Cat “A” & “C” (Helicopter & Jet engine) Cat “A” (Helicopter) Cat “C” (Jet Engine) 3,4,5,6,7,9,10,12,15, 17 3,4,5,6,7,9,10,12 3,4,5,6,7,9,10,15,17 X X X X X X X X X X X X X X X X F F X X X X X X X X F X F X X X X X X X X X X X X X X X X X X X X X X X X X F X X X X X F F X F X Page 124 of 175 6. KNOWLEDGE EXAMINATION MODULES WHICH ARE DEEMED TO HAVE BEEN COVERED BY VIRTUE OF EXISTING LICENCE CATEGORY B2 TABLE .CAR 66 Licence Modules deemed Covered 3.12.13.4 .5.16.5.6.12 X X X X X X X X F F (Helicopter) Cat “C” 3. Paper II and Paper III of the knowledge examination conducted by DGCA under the examination system existed prior to the introduction of CAR-666.6.13.4.9 Excluding 13.4 Excluding 13.already covered by virtue of existing license.8.4.Avionics Pre.9 F F F F Cat.10 3.4.CAR 66 Licence Modules deemed Covered Modules Required 3 4 5 6 7 8 9 10 11A 11B 12 13 TABLE .9.6.2 14 15 16 17 Cat “A” & “C” 3.9.Helicopter . “I” 3. “E & R” ( Electrical & Radio Navigation) 3. F-full module required. X X X X X F X X F X X (Piston 17 Engine) X.5.by G T SELVAN Draft CAR-66 Dated 7th March 2011 KNOWLEDGE EXAMINATION MODULES WHICH ARE DEEMED TO HAVE BEEN COVERED BY VIRTUE OF EXISTING LICENCE – CATEGORY B1 B1.9.4.10.7.7.10.10 X X X X X F X X F Page 125 of 175 . “E” ( Electrical) X X X X X X X X X X X X X X X X X X X X F X X F X X F X X F X X Excluding 13.10 (Instruments) Cat.9.7.7.9.7.10 Modules Required 3 4 5 6 7 8 9 10 11A 11B 12 13 14 15 16 17 Cat. First column may be substituted by corresponding Paper I.7. “E & I” (Eectrical & Instruments) Cat.10.4.6.5.4.6.13. (Helicopter & 16.5.5.5.6. 13.5.4.9 Excluding1 3.5.9.Piston Pre.6.3 B2 .5. R”(Radio Navigation) Cat.4.7.10 3. 13.7.9.17 X X X X X X X X X X X (Piston engine) Cat “A” 3.9.8 Excluding 13. 13.4.5.6. I.9.8 X F Cat.5.10 X X X X X F X X Excluding1 3.7.by G T SELVAN Draft CAR-66 Dated 7th March 2011 KNOWLEDGE EXAMINATION MODULES WHICH ARE DEEMED TO HAVE BEEN COVERED BY VIRTUE OF EXISTING LICENCE CATEGORY B2 TABLE .CAR 66 Licence Cat.5.6.14 X X X X X X X X X.4.10.already covered by virtue of existing license.&R”3. 13.8. Paper II and Paper III of the knowledge examination conducted by DGCA under the examination system existed prior to the introduction of CAR-666.6.9. First column may be substituted by corresponding Paper I.7.3 B2 . V/ “E. “I &R” (Instrument & Radio Navigation) Modules deemed Covered Modules Required 3 4 5 6 7 8 9 10 11A 11B 12 13 14 15 16 17 3. F-full module required.Avionics Pre. X ( Avionics) 13.4. Page 126 of 175 .4. Instrument & Radio) Cat “E” (Electrical) Cat “I” (Instrument) B2 .4 B1.1 B1.3 B1. Excluding airframe. NIL Excluding engine. Excluding airframe.R” (Electrical.2 B1.CAR 66 Licence Cat “A” & “C” (Heavy Aircraft & Jet Engine) Cat “A” & “C” (Light Aircraft & Jet Engine) Cat “A” (Heavy Aircraft) CAR 66 Licence TABLE . NIL Excluding instrument systems. Excluding autopilot systems on aeroplanes.by G T SELVAN Draft CAR-66 Dated 7th March 2011 CONVERSION & LIMITATIONS Pre . Excluding radio radar systems.2 B1. Excluding airframe.I. NIL Excluding engine. Excluding airframe. Excluding autopilot systems on helicopters.2 B1. Excluding electrical power generation & distribution systems.4 Limitation(s) NIL Limitation Code 10 11 10 11 10 11 10 11 10 2 3 4 5 6 7 1 B1.4 B1. Excluding engine.1 B1.4 B2 B2 Excluding airframe. INS/IRS and Flight Directors systems.3 B1.1 B1. “V” ( Avionics)/” E. Excluding radio communication/navigation and radar systems. Page 127 of 175 Cat “C” (Jet Engine) Cat “A” & “C” (Light Aircraft & Piston Engine) Cat “A” (Light Aircraft) Cat “C” (Piston Engine) Cat “A” & “C” (Helicopter & Jet Engine) Cat “A” (Helicopter) Cat “C” (Jet Engine) Cat “A & C” (Helicopter & Piston Engine) Cat “A” (Helicopter) Cat “C” (Piston Engine) Cat.3 B1. NIL Excluding engine.1 B1. Excluding automatic landing and auto throttle systems on aeroplanes. CAR 66 Licence CAR 66 Licence TABLE . Excluding radio radar systems. INS/IRS and Flight Directors systems. Excluding autopilot systems on helicopters. Excluding autopilot systems on helicopters. Excluding instrument systems. Excluding radio radar systems. Excluding autopilot systems on aeroplanes. Excluding electrical power generation & distribution systems. Excluding instrument systems. Cat “I & R” (Instrument & Radio Navigation) B2 1 Page 128 of 175 . INS/IRS and Flight Directors systems. Excluding automatic landing and auto throttle systems on aeroplanes.4 Limitation(s) Limitation Code 6 7 1 2 3 4 5 Cat “R”( Radio Navigation) B2 Cat “E & I” (Electrical & Instrument) Cat “E & R” (Electrical & Radio Navigation) B2 6 7 2 3 4 5 B2 Excluding radio communication/ navigation and radar systems. Excluding autopilot systems on aeroplanes.by G T SELVAN Draft CAR-66 Dated 7th March 2011 CONVERSION & LIMITATIONS Pre . Excluding automatic landing and auto throttle systems on aeroplanes. Excluding electrical power generation & distribution systems. Excluding radio communication/ navigation and radar systems. 5.5.7 1.5 6.CAR-66 Licence Held CAR 66 Licence Issued with Limitation TABLE .8). 7 2.2 B1. 13 (Excluding 13. 13 (Excluding 13. 13.9).4).9). 11A 16.5 Limitation Code(s) Endorsed on CAR-66 Licence 10 11 10 11 10 11 10 11 10 2.3 B1.3.6.1 B1.6. 12 8.13.14 8.5 Module to be passed to remove ‘Limitations’ 11A 15.2.4.4 B1.3.8).6.16 8. 14 8.4.5.5. 12 8.3 B1. 13.1 B1.by G T SELVAN Draft CAR-66 Dated 7th March 2011 KNOWLEDGE EXAMINATION MODULES REQUIRED TO BE PASSED TO REMOVE LIMITATIONS Pre. 14 8. 17 8.4.4. 13.7 1. 13 (Excluding 13. 17 8. 15 8. 14 8. 13. 13 (Excluding 13. 14 Cat “A” (Light Aircraft) & Cat “C” (Jet Engine) Cat “A” (Heavy Aircraft) B1.8. 13 (Excluding 13.3. 13 (Excluding 13.2 B1.4 B2 B2 B2 B2 B2 B2 Cat “C” (Jet Engine) Cat “A” (Light Aircraft) Cat “C” (Piston Engine) Cat “A” (Helicopter) Cat “C” (Jet Engine) Cat “A” (Helicopter) Cat “C” (Piston Engine) Cat “E” (Electrical) Cat “I” (Instrument) Cat “R”( Radio Navigation) Cat “E & I” (Electrical & Instrument) Cat “E & R” (Electrical & Radio Navigation) Cat “I & R” (Instrument & Radio Navigation) 1 Page 129 of 175 . 13.4. 13.9).1 B1. 11B 8. 14 8. INS/IRS and Flight Directors systems. 9. the holder is not authorized to exercise the privileges of the licence on specific system denoted (in the 2nd column of Table-6) by the ‘Limitation Code’ of the particular type of aircraft Page 130 of 175 . 7. 5. * Endorsement of the ‘Limitation Code’ on an AMEL implies that. Excluding instrument systems. 3. 11. Excluding radio radar systems. Excluding engine. Reserved. 2. 10. Excluding airframe. Excluding automatic landing and auto throttle systems on aeroplanes. 8. 4. Excluding autopilot systems on helicopters. Excluding autopilot systems on aeroplanes.by G T SELVAN Draft CAR-66 Dated 7th March 2011 IMPLICATION OF LIMITATIONS CODES ENDORSED ON A CONVERTED LICENCE Limitation CODE* 1. TABLE . 6.6 Restriction Imposed on the ‘Certification Privilege’ of the Licence Excluding electrical power generation & distribution systems. Excluding avionic LRUs. Excluding radio communication/navigation and radar systems. Page 131 of 175 .by G T SELVAN Draft CAR-66 Dated 7th March 2011 Appendix VIII – Requirements and Procedures for Grant of Approvals Approval to persons employed in an organization approved by DGCA to carry out maintenance work on aircraft. shall be granted in accordance with. requirements and procedures specified in CAR Section 2 Series L Part X and procedures approved in the Maintenance Organization’s Exposition until publication of specific requirements under CAR-66. engine or components and issue certification thereof. requirements and procedures specified in CAR Section 2 Series L Part IX until publication of specific requirements under CAR-66.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Appendix IX – Requirements and Procedures for Grant of Authorizations Authorization to aircraft maintenance personnel by DGCA to certify maintenance work carried out on an aircraft shall be granted in accordance with. Page 132 of 175 . by G T SELVAN Draft CAR-66 Dated 7th March 2011 Appendix X – Requirements and Procedures for Grant of Certificate of Competency Certificate of Competency to persons employed in an organization approved by DGCA to carry out and certify specialized processes and nondestructive inspections shall be granted in accordance with, requirements and procedures specified in CAR Section 2 Series L Part XIV until publication of specific requirements under CAR-66. Page 133 of 175 by G T SELVAN Draft CAR-66 Dated 7th March 2011 Acceptable Means of Compliance (AMC) to SECTION A of CAR 66 AMC 66.A.10 Application AMC 66.A.10 (a) Maintenance experience should be written in a manner that the reader has a reasonable 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 experience is desirable and be kept. It is acceptable to cross refer in the CA Form 19-01 to other documents containing information on maintenance. Applicants claiming the maximum reduction in 66.A.30 (a) total experience based upon having successfully completed approved basic training should include the certificate of approval with its validity schedule of the training establishment. Applicants claiming reduction in 66.A.30 (a) total experience based upon having successfully 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.20 (a) Privileges The following definition of line and base maintenance should apply: Line maintenance is any maintenance that is carried out before flight to ensure that the aircraft is fit for the intended flight. It may include: trouble shooting; defect rectification; Component replacement with use of external test equipment if required. Component replacement may include components such as engines and propellers; Scheduled maintenance and/or checks including visual inspections that will detect obvious unsatisfactory conditions/discrepancies but do not require extensive in depth inspection. It may also include internal structure, systems and power plant items which are visible through quick opening access panels/doors; minor repairs and modifications which do not require extensive disassembly and can be accomplished by simple means; For temporary or occasional cases (airworthiness directives, hereinafter AD; service bulletins, hereinafter SB) the quality manager may accept base maintenance tasks to be Page 134 of 175 by G T SELVAN Draft CAR-66 Dated 7th March 2011 performed by a line maintenance organization provided all requirements are fulfilled. Conditions under which these tasks may be performed shall form part of the Approved Maintenance Organization’s Exposition. Maintenance tasks falling outside these criteria are considered to be base maintenance. Note: Aircraft maintained in accordance with "progressive" type programmers need to be individually 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. 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 requirements 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: - 6 months continuous employment within the same organisation; or - 6 months split up into different blocks, employed within the same or in different organisations. The 6 months period can be replaced by 100 days of maintenance experience in accordance with the privileges, whether they have been performed within an approved organisation 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 competent authority. 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 utilization, 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: Page 135 of 175 . which means equally equipped with the following (as applicable to the licence category): a) Propulsion systems (piston or turboprop or turbofan or turboshaft or jet-engine or push propellers). . 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. for every aircraft included in the authorization the experience should be on that particular aircraft or on a similar aircraft within the same licence subcategory. . the experience should include exercising the privileges. and d) Structure (manufactured of metal or composite or wood).Trouble-shooting. and b) Flight control systems (only mechanical controls or hydro-mechanically powered controls or electro-mechanically powered controls). . including servicing. construction and comparable systems.Releasing aircraft to service.Servicing.In the case of B1 licence endorsed with group ratings (either manufacturer group or full group) as defined in 66.Changing component. . and c) Avionic systems (analog systems or digital systems).A.Repairing. For category A certifying staff.Inspection. wood).45(g) the holder may show experience on at least one aircraft type per group and per aircraft structure (metal.Modifying. . Page 136 of 175 . component changes and simple defect rectifications. the following activities are considered relevant for maintenance experience: .Operational and functional testing. For category B1 and B2.Supervising these activities.30 (g).by G T SELVAN Draft CAR-66 Dated 7th March 2011 Depending on the category of the aircraft maintenance engineer’s licence. As an alternative to the above: . Two aircraft can be considered as similar when they have similar technology. . composite. .A. B2 or C. construction and with comparable systems: . . For category C. For a combination of categories. registration.A. and . structural repair. The experience should be documented in an individual log book or in any other recording system (which may be an automated one) containing the following data: a) Date and time. release.e.e. line.Maintenance technical support/engineering. supervise.A. base.by G T SELVAN Draft CAR-66 Dated 7th March 2011 . 100 FH check. b) Aircraft type. This experience requirement does not apply to: . c) Aircraft identification i.Certifying staff issuing a certificate of release of aircraft as per M.e. f) Type of maintenance i. .A30 (j) and Appendix IV of CAR-145. engine oil check and complement. g) Type of activity i.A. SB embodiment.607 (b). . h) Category used A.45 (g) the holder may show experience on at least one aircraft type per group. STC embodiment….Pilot-owner certifying tasks according to M. the experience should include some activities of the nature shown in paragraph 2 in each category.e.Aircraft maintenance related training as an instructor/assessor or as a student. trouble shooting. perform. A maximum of 20% of the experience duration required may be replaced by the following relevant activities on an aircraft type of similar technology. e) Operation performed i. Page 137 of 175 . B1. MLG wheel change.In the case of a B2 licence endorsed with group ratings (either manufacturer group or full group) as defined in 66.Certifying staff according to 145.Maintenance management/planning. the experience should cover at least one of the aircraft types endorsed on the authorization.803. d) ATA chapter. 25 Basic knowledge requirements Knowledge gained and examinations passed during previous experiences on case to case basis. he/she was engaged in aircraft maintenance or associated activities including training and operation for a period of six months. it is however essential that any applicant to a category C holding a B1 or B2 licence demonstrate at least 12 months experience as a B1 or B2 base maintenance support staff.A.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Experience should be supported by documentary evidence. The training would include the use of tools and measuring devices.40 Continued validity of the aircraft maintenance engineer’s licence Renewal of AME Licence 1. involving the manufacture. AMC 66. at least 50% of the required 12 month experience should be gained within the 12 month period prior to the date of application for the CAR66 aircraft maintenance license. Renewal of current AME Licence a) The Aircraft Maintenance Engineer’s licence becomes invalid five years after its last issue or renewal and may be renewed for a further period of five years if the applicant establishes that.A. overhaul or inspection of mechanical.A. AMC 66. Credit to Basic knowledge examinations passed by an applicant who has qualified for issuance of an AME Licence prevailed prior to the CAR-66 coming into force. 2. Page 138 of 175 . The remainder of the experience should have been gained within the 5 year period prior to application. and iii) he/she has no known physical disability / disorder. acceptable to DGCA. may be claimed in accordance with Appendix VII to the CAR-66. will be credited where DGCA is satisfied that such knowledge and examinations are equivalent to that required by Appendix I to CAR-66. repair. AMC 66. AMC 66.A. A skilled worker is a person who has successfully completed a course of training.30 (d) Experience requirements To be considered as recent experience.30 (a) Experience requirements 1. ii) he/she had attended necessary refresher training with respect to the type of aircraft endorsed on the licence. 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. electrical or electronic equipment. i) during the preceding twenty four months. Imparting training to Pilots. 2. Opposite Sufdarjung Airport. Applications of AMEs employed in DGCA approved maintenance organization may be submit by their Quality Manager as per the procedure detailed in the organizations exposition. Such licences will be renewed from the date of completion of processing of the application for a period of five years. 3. Production. not before 60 days of its expiry. d) Application for renewal of AMEL may be made 30 days in advance but. planning. Holders of Aircraft Maintenance Engineer Licence. Fees as prescribed by Rule 62 of the Aircraft Rules. Such organisation may submit the necessary documents on behalf of the Aircraft Maintenance Engineer licence holder after verifying the contents of the application and the authenticity of the documents attached. b) If the AME is not meeting licence renewal requirements of paragraph 1(a) and the licence had remained lapse for a period upto 2 years. then the licence may be Page 139 of 175 . The application should be duly countersigned and Quality Manager of the firm. confirming that the AME concerned was not engaged in aircraft maintenance and certification function during the lapsed period of AMEL. Applications of the Quality Manager or the chief engineer of a flying club may be certified by the Accountable Manager. Aircraft Maintenance Engineers.by G T SELVAN Draft CAR-66 Dated 7th March 2011 b) AMEs employed in any of the following organization are deemed to meet the intent of above paragraph (a)(i) for the purpose of renewal of AME licence. the licence may be renewed after a skill test in respect of each type rating endorsed on the licence provided the AME applies for the same on CA Form 19-09. Note: However. as a member of the flying crew. Renewal of Expired Licence a) An AMEs meeting the licence renewal requirements of paragraph 1(a). to exercise the privileges of the licence. The application should be accompanied by a self declaration and a certificate issued by the Quality Manager of the Approved Maintenance Organisation. 1937 along with experience certificate. an AME is required to have actual aircraft maintenance experience in respect of each type rated endorsement or met the provisions for issue of appropriate privileges. Flight Engineers. 1. New Delhi. 2. c) Holders of Aircraft Maintenance Engineers’ Licences may apply to the respective Regional / Subregional Office of DGCA on CA Form 19-03 with the original AMEL. quality departments of operators/manufacturers/maintenance agencies of aircraft/aircraft components and items of equipment. but less than 5 years. but did not exercise the privileges of licence during the lapsed period of validity. c) If the AME is not meeting licence renewal requirements of paragraph 1(a) and the licence had remained lapse for a period more than 2 years. details of refresher course under gone and medical fitness certificate. may apply on CA Form 19-03 to the respective regional airworthiness office with the original Aircraft Maintenance Engineer’s Licence. 110 003. employed abroad. may apply to ‘The Directorate General of Civil Aviation. Theoretical and practical training should also take into account critical aspects such as Critical Design Configuration Control Limitations. . AMC 66. moisture. For category A certifying staff specific training on each aircraft type will be required reflecting the authorized task(s) as indicated under 66. in service experience on the aircraft type.A. 4. d) If the AME licence had remained lapse for a period more than 5 years.A. engine ground running and computer-based training (CBT) etc may also be utilized. including the engines. equipment.45 (a) Type/task training and ratings 1.A. including training in the systems in use for technical manuals and maintenance procedures. etc. Guidance is provided for training in Addendum IV to AMC to 66. the licence may be renewed after the applicant has satisfied the initial licence issue requirements. but this can be reduced to a minimum of two weeks for applicant with such previous experience. Ground simulator time. systems. wind. Theoretical training should be supported by training aids such as aircraft system components.45 (d) Type/task training and ratings 1. Appropriately approved maintenance organisation means an organisation approved in compliance with the CAR 145 or subpart F of CAR M. Knowledge is also recommended of relevant inspections and limitations as applicable to the effects of environmental factors such as cold and hot climates. 2. interior and applicable components. its main parts. The course should also take into account the following: a) b) c) d) 2.A. 5. feedback from in-service difficulties/occurrence reporting etc. Known human factors issues associated with the particular aircraft type.45(d). AMC 66. significant airworthiness directives and/or service bulletins.by G T SELVAN Draft CAR-66 Dated 7th March 2011 renewed after a type course or type examination followed by a skill test in respect of each type rating endorsed on the licence provided the AME applies for the same on CA Form 19-08 & 19-09. The training should give adequate detailed theoretical knowledge of the aircraft.20 (a) 1. The practical training should comprise a period of four months for applicants with no recent recorded previous practical experience of aircraft of comparable construction and systems. Page 140 of 175 3. Where the practical training element is conducted by a maintenance organization approved under CAR-145. The logbook should be designed such that tasks may be countersigned by the supervisor. The duration of the practical type training element should take into account significant differences between types and be acceptable to DGCA. Alternatively. depending on the individual’s previous experience. etc. the following elements: Fly by wire. glass cockpit avionics. in the case of a structured OJT. under its own responsibility. Such records may take the form of an individual training logbook. but are not limited to. The list of tasks should be accepted directly for each individual. These differences will require considerably more practical training for certifying staff who are not familiar with the new techniques and technologies. Before grant of the aircraft type. it should be considered as part of the approved course and as such. its acceptance by DGCA should be supported by a detailed syllabus showing its content and duration. In this case the maintenance organization approved under CAR-145 should provide applicants for a type rating a logbook indicating a list of tasks to be performed under supervision.by G T SELVAN Draft CAR-66 Dated 7th March 2011 6. The individual practical training records should be designed in a manner that they demonstrate compliance with the detailed practical training syllabus. which. The individual practical training records should be designed in a manner that they demonstrate compliance with the detailed practical training syllabus. 7. Where the practical training element is conducted by or under the responsibility of the training organization under DGCA approval or a direct type course approval. significant structural differences. or indirectly through the acceptance of a procedure giving delegation to the maintenance organization. In all cases the practical element should include an acceptable cross section of maintenance tasks. the applicant should be able to: Page 141 of 175 . Some examples of differences may include. The logbook should be designed such that tasks may be countersigned by the training school or other course provider. can be tailored to accommodate the operating profile of the CAR-145 organization whilst also supplementing the theoretical course elements. The means by which the practical element is supervised and the control of the standard should be acceptable to DGCA. A programme of structured on-job-training (OJT) may be prepared to satisfy the practical training requirement. its acceptance by DGCA should be supported by a detailed syllabus showing its content and duration. the practical training element may consist of a structured OJT programme. this should be reduced to 30%. this should be reduced to 20%. repairs. flight guidance systems.A.A. c) d) 8. perform removal and replacement of components and modules unique to type.g. EFIS (Electronic flight instrument system). For example trouble shooting. as applicable to the concerned aircraft type and licence category should be performed. adjustments. etc. variable pitch propeller. The practical assessment should also ensure safe performance of maintenance. replacements and functional /operational checks etc including engine operation (ground running) if required. AMC 66.by G T SELVAN Draft CAR-66 Dated 7th March 2011 a) b) demonstrate by knowledge examination a detailed understanding of applicable systems. For the first aircraft type of each manufacturer group. Page 142 of 175 . For the second aircraft type of each manufacturer group. “Aircraft types representative of a group” means that: for the A and B1 category the aircraft type should include typical systems and engines relevant to the group (e. etc.45 (h) Type/task training and ratings 1. including any on-wing maintenance activity. for the B2 category the aircraft type should include complex avionics systems such as radio coupled autopilot. - 2. etc A “multiple engines” group automatically includes the corresponding “single engine” group. their operation and maintenance. for the type of aircraft. Correctly use specialist/special tooling and test equipment. inspections and routine work according to the maintenance manual and other relevant instructions and tasks as appropriate for the type of aircraft.45 (g) Type/task training and ratings 1. repairs. pressurization. Type experience should cover an acceptable cross section of tasks from Addendum II ( to AMC). correctly use all technical literature and documentation for the aircraft. for the single piston engine metal subgroup) and. adjustments (rigging). For subsequent aircraft types of each manufacturer group. ensure safe performance of maintenance. retractable undercarriage. rigging and functional checks such as engine run. for example trouble shooting. at least 50% of the Addendum II to AMC) tasks. as appropriate. AMC 66. inspections and routine work according to the maintenance manual and other relevant instructions and tasks. if required. replacements. A.by G T SELVAN Draft CAR-66 Dated 7th March 2011 2.. AMC 66. AMC 66.71 Duplicate AME Licence a) If an AME has lost the original AMEL. 1937 to Director General of Civil Aviation. when an applicant has satisfactorily fulfilled the relevant conversion examination and gained relevant experience. opposite Safdarjung Airport. iii) fee as per Rule 62 of the Aircraft Rules. New Delhi – 110003 for issue of duplicate licence. as appropriate. opposite Safdarjung Airport New Delhi – 110003 for issue of duplicate licence. b) If the original AMEL had mutilated. Type experience should be demonstrated by the submission of records or logbook showing the Addendum II ( to AMC) tasks performed by the applicant as specified by DGCA.70 Conversion provisions Technical limitations will be deleted. 1937 iv) copy of AMEL if available. the holder of the licence may apply on CA Form 1905 with the mutilated AMEL and fee as per Rule 62 of the Aircraft Rules. i) Affidavit duly notarized by Authorized notary.A. ii) Copy of FIR lodged with the police station for the loss. Page 143 of 175 . he/she may apply on CA Form 19-05 enclosing following supporting documents to Director General of Civil Aviation. eligible for type examinations and manufacturer group ratings 4 Aeroplanes single turbine engine (ASTE) of 5700 kg and below. In the following table.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Addendum I to AMC of CAR-66 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. such information should be first passed on to the DGCA daw@dgca. the ratings on the AME licences may be modified at next renewal or when the licence is received for endorsement /re-issued. requiring type training and individual type rating (A-tr) 3 Aeroplanes multiple turbine engines (AMTE) of 5700 kg and below. Notes: When a modification is introduced to an aircraft type rating or to an engine designation in the rating which affect licences already issued. this list is only intended for the maintenance purposes.nic. 49A and CAR-21. 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. In order to keep this list current and type ratings consistent. Aeroplanes with a maximum take-off mass of more than 5700 kg. eligible for type examinations and group ratings Page 144 of 175 .in by affected personnel or organizations to issue a type rating that is not included in this list. the groups of aircraft are defined as follows: List No. Aircraft: 1 Large aircraft (LA). requiring type training and individual type rating 2 Aeroplanes of 5700 kg and below. eligible for type examinations and group ratings 5 Aeroplane multiple piston engines – metal structure (AMPE-MS). by G T SELVAN Draft CAR-66 Dated 7th March 2011 6 Aeroplane single piston engine – metal structure (ASPE-MS). Column 3 includes the relevant individual type rating.eligible for type examinations and group ratings 10 Aeroplane single piston engine – composite structure (ASPE.CS). FAA or other). eligible for type examinations and group ratings 11 Multi. Page 145 of 175 . eligible for type examinations and group ratings Column 1 includes the TC holder as defined in the TCDS (EASA. requiring type training and individual type rating 12 Helicopters – Single turbine engine (HSTE . the Column 2 includes the aircraft models as defined in the relevant TCDS (EASA. eligible for type examinations and group ratings 13 Helicopters – Single piston engines( H SPE) . FAA or other). For aeroplanes of group 1 and 2 and helicopters. eligible for type examinations and group ratings 7 Aeroplane multiple piston engines – wooden structure (AMPE-WS). eligible for type examinations and group ratings 8 Aeroplane single piston engine – wooden structure/metal tube-fabric (ASPEWS). eligible for type examinations and group ratings 9 Aeroplane multiple piston engines – composite structure (AMPE-CS ) . Note: aircraft STC data are not included in this table. The following column includes the “commercial designation” when available.engine helicopters (MEH . Only the designations of ratings in column 3 should be used for endorsing individual type ratings on CAR-66 licences. by G T SELVAN Draft CAR-66 Dated 7th March 2011 1. requiring type training and individual type rating Commercial 1. TC holder 2 Aeroplanes Model 3 Type Rating Endorsement Designation A310-304 A310-324 A318-110 series A319-110 series A320-111 A320-210 series A321-110 series Airbus A321-210 series A319-130 series A320-230 series A321-130 series A321-230 series A330-200 series Airbus A330 (GE CF6) A330-300 series A330-220 series A330-320 series AIRCRAFT INDUSTRIES Let L-410 (Walter M601) Airbus A330 (PW 4000) Airbus V2500) A319/A320/A321 (IAE Airbus (CFM56) A318/A319/A320/A321 Airbus A310 (GE CF6) Airbus A310 (PW 4000) L-410 UVP-E9 ATR 42-200 ATR 42-320 Turbolet ATR 42-200/300 PW120) series (PWC ATR-GIE Avions de Transport Régionals ATR 72-212 ATR 42-500 ATR 72-212 A 42-500 72-500 ATR 72-200 series (PWC PW120) ATR 42-400/500/72-212A (PWC PW120) Page 146 of 175 . Large aircraft (LA). Aeroplanes with a maximum take-off mass of more than 5700 kg. Aeroplanes with a maximum take-off mass of more than 5700 kg.by G T SELVAN Draft CAR-66 Dated 7th March 2011 1.748 Series 2 HS748 (RRD Dart) HS 748 Series 2A HS 748 Series 2B B737-200 B737-400 B737-700 B737-800 Boeing 737-700/800/900 (CFM56) B737-900 B737-900ER B747-400 B747-400F/SF(BCF) Boeing B757-200 B757-200PF B757-300 B757-200 B777-200 B777-200LR B777-300ER Boeing 777-200/300 (GE 90) Boeing 757-200 (RR RB211) Boeing 757-200/300 (PW 2000) Boeing 747-400 (PW 4000) Boeing 737-/200 (PW JT8D) Boeing 737-400 (CFM56) B777-200 Boeing 777-200/300 (PW 4000) B777-300 Page 147 of 175 . TC holder 2 Aeroplanes Model 3 Type Rating Endorsement Designation BAe 146/ AVRO 146-RJ (Honeywell AVRO 146-RJ70 ALF500 Series) HS. requiring type training and individual type rating Commercial 1. Large aircraft (LA).748 Series 1 BAE SYSTEMS HS. Large aircraft (LA). requiring type training and individual type rating Commercial 1. TC holder 2 Aeroplanes Model 3 Type Rating Endorsement Designation Bombardier BD-100-1A10 BD-100-1A10 Challenger 300 (Honeywell AS907) Bombardier BD-700 Series (RRD BD-700-1A10 Global Express BR710) BD-700-1A11 CL-600-2B16 (CL 604 Variant) CL-600-2B16 (CL 604 Variant) CL-600-2B19 CRJ 200 CL-600-2C10 CL-600-2D15 525B 525C 550 560 560 550 S550 560 560 560XL 560 XLS 650 650 Dassault Aviation Falcon 900EX Regional Jet Series 700/701/702 Regional Jet Series 705 Citation Jet CJ3 Cessna 525B/C (Williams FJ 44) CESSNA AIRCRAFT Company Citation Jet CJ4 Citation Bravo Citation Encore Citation Encore + Citation II Citation S/II Cessna 550/560 (PWC JT15D) Citation V Citation Ultra Citation Excel Cessna 560XL/XLS (PWC PW545) Citation XLS Citation III – VI IV Cessna 650 (Honeywell TFE731) Citation VII Falcon 900EX (Honeywell TFE731) Cessna 550/560 (PWC PW530/535) Global 5000 Challenger-604 (MSN < 5701) Challenger-605 (MSN > 5701) Regional Jet Series 100/200 Bombardier CL-600-2B16 (variant CL 604) (GE CF34} BOMBARDIER Bombardier CL-600-2B19 (GE CF34) Bombardier CRJ 200(GE CF34) Bombardier CL-600-2C10/-2D15/2D24/-2E25 (GE CF34) Page 148 of 175 .by G T SELVAN Draft CAR-66 Dated 7th March 2011 1. Aeroplanes with a maximum take-off mass of more than 5700 kg. Large aircraft (LA).125 series 700 Hawker 750 Hawker 800XP "Hawker Siddeley" Hawker 750 Hawker 800XP Page 149 of 175 . requiring type training and individual type rating Commercial 1. Aeroplanes with a maximum take-off mass of more than 5700 kg. TC holder 2 Aeroplanes Model 3 Type Rating Endorsement Designation Falcon 900EX Falcon 900EX Falcon 900EX Falcon 2000 Falcon 2000EX Falcon 2000EX Falcon 2000EX Falcon 2000EX Falcon 7X RUAG Aerospace GmbH (DORNIER) EMBRAER ERJ 170-100 LR FOKKER SERVICES F27 Mark 100 F27 Mark 200 F27 Mark 300 F27 Mark 400 F27 Mark 500 GULFSTREAM AEROSPACE LP (GALP) c/o Israel Aircraft Industries HAWKER BEECHCRAFT Corporation 228-200 series EMB-135BJ Legacy 600 Legacy 650 ERJ-170 Friendship Friendship Friendship Friendship Friendship Fokker F27 / Fairchild F-27/FH-227 (RRD Dart) F2000EX EASy F2000DX F2000LX Falcon 7X (PWC PW307A) Dornier 228 (Honeywell TPE331) Embraer EMB-135 (RR AE3007A) Embraer ERJ-170 (GE CF34) Corp Falcon 2000EX EASy (PWC PW308) F900EX EASy F900DX F900LX Falcon 2000 (CFE 738) Falcon 2000EX (PWC PW308) Falcon 900EX EASy (Honeywell TFE731) Gulfstream Galaxy 200 / Galaxy 200 Gulfstream (IAI) 200/Galaxy (PWC PW306) BAe 125 Series 700 (Honeywell TFE731) BAe 125 750/800XP/850XP/900XP (Honeywell TFE731) Series HS.by G T SELVAN Draft CAR-66 Dated 7th March 2011 1. by G T SELVAN Draft CAR-66 Dated 7th March 2011 1. Aeroplanes with a maximum take-off mass of more than 5700 kg. TC holder 2 Aeroplanes Model 3 Type Rating Endorsement Designation Hawker 850XP Hawker 900XP 300 300LW B300 B300C 400 400A 1900 1900C 1900D 4000 Learjet 45 Lear Jet Learjet 40 LJ45 Hawker 850XP Hawker 900XP Super King Air Super King Air Beech 300 Series (PWC PT6) Super King Air 350 Super King Air 350 C Beechjet Beechjet 400XP) Airliner Airliner Airliner Hawker 4000 LJ45 Hawker 4000 (PWC PW308) Learjet Model TFE731) 45 (Honeywell Beech 1900 (PWC PT6) (Hawker Beech 400 / Mitsubishi MU-300 (PWC JT15) Page 150 of 175 . Large aircraft (LA). requiring type training and individual type rating Commercial 1. ) B200 B200C B200GT 390 P180 P180 PC-12 DHC-6-1 DHC-6-100/110 DHC-6-200/210 DHC-6-300/310/320 DHC-6-400 Twin Otter Twin Otter Twin Otter Twin Otter Twin Otter De Havilland DHC-6 (PWC PT6) Premier 1.by G T SELVAN Draft CAR-66 Dated 7th March 2011 2. Aeroplanes of 5700 kg and below. 1A Avanti Avanti II Beech 200 Series (PWC PT6) Beech 390 (Williams FJ44) King Air King Air King Air Beech 90 Series (PWC PT6) Turbolet Turbolet Citation Jet CJ1 Citation Jet CJ2 Phenom 100 Embraer EMB-500 (PWC PW617) Cessna 525/525A (Williams FJ 44) Let L-410 LW (Walter M601) PIAGGIO Aero Industries PILATUS AIRCRAFT VIKING AIR (Bombardier) (De Havilland) Piaggio P180 Avanti/Avanti II (PWC PT6) Pilatus PC-12 (PWC PT6) Page 151 of 175 . requiring type training and individual type rating (A-tr) 1 TC Holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation AIRCRAFT INDUSTRIES L-410M L-410 UVP 525 Cessna Aircraft Company EMBRAER Empresa Brasileira Aeronautica HAWKER BEECHCRAFT Corporation 525A EMB-500 de 65-90 C90 C90A HAWKER BEECHCRAFT Corporation (cont. Aeroplanes single turbine engine (ASTE) of 5700 kg and below. eligible for type examinations and manufacturer group ratings TC holder B-N GROUP Ltd. eligible for type examinations and group ratings TC holder CESSNA AIRCRAFT Company Type rating endorsement 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) 5. (Britten-Norman) Type rating endorsement Britten-Norman BN2T Series (RR Corp 250) PIPER AIRCRAFT Corporation Piper PA-31TSeries (PWC PT6) 4. eligible for type examinations and group ratings TC holder AEROSTAR AIRCRAFT Corporation CESSNA AIRCRAFT AVIATION Company/ REIMS Type rating endorsement Piper PA-60/61 Series (Lycoming) Cessna 310/320 Series (Continental) Cessna 336 (Continental) Cessna 421 (Continental) Cessna T303 (Continental) Beech 55 Series (Continental) Beech 58 Series (Continental) Beech 58P (Continental) Beech 65-80 Series (Lycoming) Beech 76 (Lycoming) Beech 95 Series (Lycoming) Page 152 of 175 .by G T SELVAN Draft CAR-66 Dated 7th March 2011 3. Aeroplane multiple piston engines – metal structure (AMPE-MS). Aeroplanes multiple turbine engines (AMTE) of 5700 kg and below. by G T SELVAN Draft CAR-66 Dated 7th March 2011 5. Aeroplane multiple piston engines – metal structure (AMPE-MS). eligible for type examinations and group ratings TC holder Type rating endorsement Piper PA-30 Series (Lycoming) Piper PA-31 Series (Lycoming) Piper Aircraft Piper PA-31P (Lycoming) Piper PA-34 Series (Lycoming) Piper PA-34 Series (Continental) VULCANAIR Dakota Vulcanair P. eligible for type examinations and group ratings TC holder CESSNA AIRCRAFT Company/ REIMS AVIATION Type rating endorsement Cessna 150 Series (Rotax) Cessna/Reims-Cessna 150/F150 Series (Continental) Cessna/Reims-Cessna 152/F152 Series (Lycoming) Cessna/Reims-Cessna 172/F172 Series (Lycoming) Cessna/Reims-Cessna 172/F172 Series (Continental) Cessna 172 Series (Thielert) Cessna 175 Series (Lycoming) Cessna 175 Series (Continental) Cessna 177 Series (Lycoming) Cessna 180 Series (Continental) Cessna/Reims-Cessna 182/F182 Series (Lycoming) Cessna/Reims-Cessna 182/F182 Series (Continental) Cessna/Reims-Cessna 182/F182 Series (SMA) Cessna 185 Series (Continental) Cessna 206 Series (Continental) Cessna 206 Series (Lycoming) HAWKER BEECHCRAFT Corporation Beech 35 Series (Continental) Page 153 of 175 .68 Series (Lycoming) Dakota DC-3 (PW R-1830-92) 6. Aeroplane single piston engine – metal structure (ASPE-MS). Aeroplane single piston engine – wooden structure/metal tube-fabric (ASPE-WS). eligible for type examinations and group ratings TC holder Type rating endorsement No Aircraft in this list Page 154 of 175 .A (Laviasa) PILATUS AIRCRAFT PIPER AIRCRAFT Type rating endorsement Beech 36 Series (Continental) Piper PA-25 Series (Lycoming) Pilatus PC-6 Series (Lycoming) Piper PA-24 Series (Lycoming) Piper PA-28 Series (Lycoming) Piper PA-28 Series (Continental) Piper PA-28 Series (Thielert) Piper PA-32 Series (Lycoming) Piper PA-36 Series (Lycoming) Piper PA-36 Series (Continental) SKY Int Aviat Husky A (Lycoming) Zlin Z-143 L (Lycoming) Zlin Aircraft (Moravan Aviation) Zlin Z-242 L (Lycoming) 7. Aeroplane single piston engine – metal structure (ASPE-MS). eligible for type examinations and group ratings TC holder LAVIA Argentina S.by G T SELVAN Draft CAR-66 Dated 7th March 2011 6. 8. eligible for type examinations and group ratings TC holder Type rating endorsement No aircraft in this list. Aeroplane multiple piston engines – wooden structure (AMPE-WS). Aeroplane single piston engine – composite structure (ASPE-CS). eligible for type examinations and group ratings TC Holder Type Rating Endorsement CIRRUS Design Corporation Cirrus SR20 (Continental) Cirrus SR22 Series (Continental) DIAMOND AIRCRAFT Industries Diamond DA40 (Lycoming) Diamond DA40 D (Thielert) Diamond DA40 (Austro Engine) NATIONAL AEROSPACE LABORATORIES Hansa 3 ( Rotax) Page 155 of 175 . Aeroplane multiple piston engines – composite structure (AMPE-CS). eligible for type examinations and group ratings TC holder DIAMOND AIRCRAFT Industries Type rating endorsement Diamond DA42 Series (Thielert) Diamond DA42 Series (Austro Engine) 10.by G T SELVAN Draft CAR-66 Dated 7th March 2011 9. by G T SELVAN Draft CAR-66 Dated 7th March 2011 11. Multi-engine helicopters (MEH). requiring type training and individual type rating 1 TC Holder AGUSTA 2 Aeroplanes Model A109E A109S Commercial Designation 3 Type rating endorsement Agusta A109 PW206/207) Series (PWC AW109SP A109 A109A AW139 BELL TEXTRON HELICOPTER 212 412 412EP 412CF BELL CANADA HELICOPTER 427 222 222B 222U 230 230 Executive 230 Utility 230 EMS 429 430 EUROCOPTER AS 355 E AS 355 F AS 355 F1 Agusta A109 Series (RR Corp 250) Agusta AW139 (PWC PT6) Bell 212 / Agusta AB212 (PWC PT6) Bell 412 / Agusta AB412 (PWC PT6) Bell 427 (PWC PW207D) Bell 222 (Honeywell LTS 101) Bell 230 (RR Corp 250) Bell 429 (PWC PW207D) Bell 430 (RR Corp 250) Eurocopter AS 355 (RR Corp 250) Page 156 of 175 . MD HELICOPTERS.by G T SELVAN Draft CAR-66 Dated 7th March 2011 11. requiring type training and individual type rating 1 TC Holder 2 Aeroplanes Model AS 355 F2 Commercial Designation 3 Type rating endorsement Eurocopter Cont… AS 355 N AS 355 NP SA 365 N SA 365 N1 AS 365 N2 AS 365 N3 EC 155 B EC 155 B1 EC 135 P1 Series EC 135 P2 Series Dauphin Dauphin Dauphin Eurocopter AS 355 (Turbomeca Arrius 1) Eurocopter SA 365 (Turbomeca Arriel 1) N Eurocopter SA 365 N1. Multi-engine helicopters (MEH). AS 365 N2 (Turbomeca Arriel 1) Eurocopter AS 365 (Turbomeca Arriel 2C) N3 Eurocopter EC 155 (Turbomeca Arriel 2) Eurocopter PW206) EC 135 (PWC EUROCOPTER Deutschland GMBH EC 635 P2+ MBB-BK 117 C2 EC145 Eurocopter MBB-BK 117 C2 (Turbomeca Arriel 1) DHRUV MD Helicopters MD900 (PWC PW206/207) M1 172 .Klimo TV/TB-3-117 VM/BM S-76C+ S-76C++ Sikorsky Arriel 2) S-76C(Turbomeca HINDUSTAN AERONAUTICS Ltd. MOSCOW HELICOPTERS PLANT DHRUV MD900 MI 172 S-76C S-76C SIKORSKY AIRCRAFT S-76C Sikorsky Arriel 1) S-76C(Turbomeca Page 157 of 175 . INC. (MDHI) MD 60N MD 60N (ALLISON 250C47M) Page 158 of 175 .by G T SELVAN Draft CAR-66 Dated 7th March 2011 12. Helicopters – Single turbine engine (HSTE). eligible for type examinations and group ratings 1 TC Holder AGUSTA BELL HELICOPTER CANADA 2 Helicopter Model A119 407 AB 206A Commercial Designation Koala 3 Type Rating Endorsement Agusta A119/ (PWC PT6) Bell 407 (RR Corp 250) AGUSTA BELL HELICOPTER TEXTRON CANADA LIMITED THE ENSTROM HELICOPTER CORPORATION EUROCOPTER AB 206B 206 series from A to L 480 480B AS 350 AS 350 B1 AS 350 B2 AS 350 BA AS 350 BB AS 350 B3 AS 350 D EC 120 B EC 130 B4 SA 315 B SA 316 B 500N Lama Alouette III Colibri Ecureuil Agusta AB206 / Bell 206 (RR Corp 250) Enstrom 480 (RR Corp 250) Eurocopter AS 350 (Turbomeca Arriel 1) Eurocopter AS 350 (Turbomeca Arriel 2B) Eurocopter AS 350 (Honeywell LTS 101) Eurocopter EC 120 (Turbomeca Arrius 2F) Eurocopter EC 130 (Turbomeca Arriel 2B) Eurocopter SA 315B (Turbomeca Artouste) Eurocopter SA 316 B (Turbomeca Artouste) MD Helicopters 500N N/ AMD500N (RR Corp 250) MD HELICOPTERS INC. by G T SELVAN Draft CAR-66 Dated 7th March 2011 13. Helicopters – Single piston engines (HSPE). eligible for type examinations and group ratings 1 TC Holder THE ENSTROM HELICOPTER CORPORATION SEI (BREDA-NARDI) 2 Helicopter Model F-28 series NH 300C Commercial Designation 3 Type rating endorsement Enstrom F-28 (Lycoming) Model 300C Schweizer / Breda Nardi (Hughes) 269/300 (Lycoming) 269A 269B SCHWEIZER AIRCRAFT CORPORATION 269C R 44 ROBINSON HELICOPTER COMPANY Robinson R44 Series (Lycoming) Page 159 of 175 . III a. Check accumulator pressure. h. Check operation of air conditioning/heating system Check operation of pressurization system Troubleshoot faulty system Auto flight Install servos. b. f. h. Perform symmetry check. Position aircraft in dock. Air Conditioning Replace combustion heater. Placards and Markings Check aircraft for correct placards. d. Replace outflow valve. b. Check tire pressures. k. b. c. Clean outflow valves. Grease aircraft. Review records for compliance with airworthiness directives. Jack complete aircraft. i. g. Service toilet/water system Perform pre-flight/daily check Vibration and Noise Analysis Analyze helicopter vibration problem. secure and cover aircraft. IX a. j. Rig bridle cables Page 160 of 175 . Lifting and Shoring Assist in : Jack aircraft nose or tail wheel. Check oil level. Replace cabin blower. Secure rotor blades. V a. c. 100 hour check (general aviation aircraft). “B” or “C” check (transport category aircraft). Analyze noise spectrum. b. Check hydraulic fluid level. Sling or trestle major component. Check aircraft against equipment list. l. Procedure for Inspection following heavy landing. Review records for compliance with component life limits. d. Prepare weight and balance amendment. e. b. f. Servicing Refuel aircraft. k. j. Defuel aircraft. X a.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Addendum II to AMC of CAR-66 Aircraft type practical experience list of tasks Time checks a. Leveling /Weighing Level aircraft. limits/Maintenance I VII a. Be part of aircraft towing team. f. c. i. Replace pressurization controller. Procedure for Inspection following lightning strike. d. e. VI a. VIII a. b. b. Towing and Taxiing Tow aircraft. d. Park. Replace air cycle unit. Replace vapour cycle unit. d. b. Connect ground power. II a. c. g. e. Parking and mooring Tie down aircraft. Dimensions/Areas Locate component(s) by station number. Weigh aircraft. b. c. b. d. b. Replace heat exchanger. Check aircraft for correct markings. Charge pneumatic system. XI a. IV a. c. e. d. h. g. n. f. Check for correct assembly and locking. Perform operational check of passenger address system. Replace passenger seats. l. Amend electrical load analysis report. h. d. g. XIII a. c. k. Replace elevator. d. Charge ni-cad battery. Check emergency equipment. j. k. d. Replace switches. m. f. k. i. f. Perform antenna VSWR check. Troubleshoot faulty system XIV a. Troubleshoot faulty system. g. Check battery capacity. Deep-cycle ni-cad battery. l. Functionally check audio integrating system. Replace powered flying control unit Replace flat actuator Adjust trim tab. d. Replace generator/alternator. Check operation of yaw damper. Repair co-axial cable. Check cabin fire extinguisher contents. l. Replace amplifier. h. Repair toilet waste container. Replace circuit breakers. Install new fire bottle. Replace rudder. j. Electrical Power Charge lead/acid battery. f. b. Check seats/belts for security. c. Fire protection Check fire bottle contents. i. Replace trim tabs. Check operation of warning system. i. Replace HF com unit. Adjust voltage regulator. g. Replace static discharge wicks. Replace existing antenna. Check operation of auto-pilot. b. h. j. Check and adjust servo clutch. Check operation of radios. b. f. Repair upholstery. Check control range and sense of movement. g. g. Troubleshoot faulty system. i. Install control cable and fittings. e. Perform mach trim functional check. Equipment/Furnishings Replace pets Replace crew seats. c. d. b. Change cabin configuration. f. Inspect engine fire wire detection systems Flight Controls Replace horizontal stabilizer. Perform autopilot gain adjustments. XII a. Repair/replace electrical feeder cable. Perform Selcal operational check. k. j. Replace aileron. c. Troubleshoot faulty system. Check operation of auto-throttle. e. Check lavatory smoke detector system. XVI a. Check inertia reels. e. Replace flaps. XV a. Replace controller. n. h. e. m. e. Adjust control cable tension. Check auto land system Check flight management systems Check stability augmentation system Communications Replace VHF com unit. c. j. b. Troubleshoot faulty system. Page 161 of 175 . i. h.by G T SELVAN Draft CAR-66 Dated 7th March 2011 c. Check ELT for compliance with regulations. Replace fire bottle squib. g. Repair/replace interior lights. Flow check system. Check operation of shut off valve. f. p. c. Test outbrake system Lights Repair/replace rotating beacon. d.by G T SELVAN Draft CAR-66 Dated 7th March 2011 XVII a. i. Replace FDR. e. Check operation of directional gyro. Functional check inertial nav system. Check pitot static system for leaks. Page 162 of 175 . Functional check weather radar. XVIII a. m. Replace brake control valve. Perform emergency lighting system checks. Replace accumulator. Replace shock strut seals. b. d. Check operation feed/selectors Troubleshoot faulty system. Ice and rain protection Replace pump. j. XX a. h. Replace VOR unit. e. e. c. n. b. Test gear retraction. i. Bleed brakes. Replace nose wheel. c. g. Replace shimmy damper. c. Change bungees. c. Functional check TCAS. f. Install wiper motor. b. Perform functional checks. c. e. f. Troubleshoot faulty system. Troubleshoot faulty system. d. o. o. k. Replace fuel selector. Replace master caution unit. f. d. g. Replace HSI. Check indicating systems. k. Troubleshoot faulty system Navigation Calibrate magnetic direction indicator. h. Functional check DME Functional check ATC Transponder Functional check flight director system. Repair/replace landing lights. Check filters. Charge struts. Troubleshoot faulty system. l. e. h. Check operation of systems. Replace main wheel. XXIII a. Troubleshoot faulty system. Perform FDR data retrieval. Hydraulics Replace engine driven pump. i. Repair/replace navigation lights. b. Replace altimeter. f. n. g. Check calibration of fuel quantity gauges. f. d. j. XXI a. Replace timer. Rig nose wheel steering. d. Replace ADI. Replace standby pump. Adjust micro switches. g. Replace clock. e. Replace brake unit. e. b. d. XIX a. Replace air data computer. m. c. XXII a. Repair/replace emergency lighting system. Implement ESDS procedures Inspect for HIRF requirements Landing Gear Build up wheel. Fuel Replace booster pump. Functional check Doppler. b. h. Replace fuel tank cells. p. g. l. Replace airspeed indicator. h. Indicating/recording systems Replace flight data recorder. Replace cockpit voice recorder. Test anti skid unit. Check filters. b. by G T SELVAN Draft CAR-66 Dated 7th March 2011 q. XXXI a. b. d. Replace compressor. Airborne Auxiliary power Install APU. Replace tip. Repair transparency. Replace CMU. Windows Replace windshield. Wooden repair. Check/replace filters. b. d. c. c. c. b. w. XXXIII d. u. b. b. Water/Waste Replace water pump. c. Troubleshoot faulty system. c. h. r. XXIV a. Perform static functional checks. Recover fabric control surface. d. XXV a. Check calibration of pitot static instruments. Inspect hot section. Structures Sheet metal repair. c. Central Maintenance System a. b. Check calibration of pressure altitude reporting system. g. XXVIII Complete quadrantal error correction of ADF system. Perform Bite check. d. Check operation during ground run. Check incidence/rig. d. c. XXX a. g. Adjust regulator. b. Propeller Assemble prop after transportation. f. c. e. Purge and recharge oxygen system. f. v. Vacuum systems Replace vacuum pump. XXVII a. f. s. Replace rib. x. b. Test door warning system. d. Perform auto oxygen system deployment check. Check track. e. Replace propeller. Recharge desiccators. Replace oxygen generator. y. t. g. Fabric repair. Check for leaks. b. e. Troubleshoot faulty system. c. XXIX a. Treat corrosion. Update flight management system database. XXVI a. Check operation of emergency exits. Replace tap. c. e. Troubleshoot faulty system. Page 163 of 175 . Test crew oxygen system. e. Adjust air stair system. Fibre glass repair. z. Replace window. Troubleshoot faulty system. Troubleshoot faulty system. Recover fabric wing. b. Replace governor. XXXII a. XXXI a. Replace regulator. f. Doors Rig/adjust locking mechanism. Troubleshoot faulty system. Troubleshoot faulty system Check marker systems Compass replacement direct/indirect Check Satcom Check GPS Test AVM Oxygen Inspect on board oxygen equipment. c. Retrieve data from CMU. Wings Skin repair. Adjust regulator. Adjust governor. Troubleshoot faulty system. XXXIV a. d. Apply protective treatment. b. Pneumatic systems Replace filter. Replace toilet pump. XXXVI a. Install helicoil. Page 164 of 175 . Engine ground run. Clean injector nozzles. Install drive assembly. c. Establish reference power. d. Install mixing box. XXXV a. j. Trend monitoring/gas path analysis. e. f. b. g. Replace engine driven pump. Replace damper assembly. h. g. Check carburetor float setting. b. XL a. h. Power Plant Build up ECU. e. b. Clean/test fuel nozzles. Adjust FCU. g. g. Rotorcraft flight controls Install swash plate. Piston Engines Remove/install reduction gear. Troubleshoot faulty system. Replace clutch/freewheel unit Replace drive belt. Overhaul main gearbox. Troubleshoot. piston Replace engine driven pump. c. Install main gearbox. Replace universal joints.by G T SELVAN Draft CAR-66 Dated 7th March 2011 h. d. Troubleshoot. Check dynamic balance. d. e. d. Check setting of micro switches. Replace blades. Repair cooling baffles. f. Tail Rotor Drive Replace bevel gearbox. Repair cowling. e. Replace blades. b. f. i. d. Replace drive coupling. g. Adjust cowl flaps. Rotor Drive Replace mast. b. c. Adjust carburetor/injector. f. Clean/replace filters. c. Replace engine. Turbine Engines Replace module. d. Adjust AMC. Troubleshoot. Establish/check reference RPM. b. XLIV a. Hot section inspection. b. c. Perform ground run. Overhaul bevel gearbox. b. b. Troubleshoot faulty system. turbine Replace FCU. Check track. c. Adjust pitch links. d. Dynamically balance prop. h. XXXVII a. e. Dress out blade damage. XLII a. Troubleshoot. Check gearbox chip detectors. Install carburetor/injector. k. Rig collective system. Repair faulty wiring. f. e. Rig anti-torque system. Check controls for assembly and locking. XXXIX a. Replace primer line. d. c. g. i. i. Check compression. Troubleshoot. Fuel and control. Check crankshaft run-out. c. XLIII a. e. c. j. f. Check controls for operation and sense. Check static balance. Extract broken stud. XXXVIII a. Adjust ABC. XLI a. i. Check tappet clearance. Rig cyclic system. e. Troubleshoot faulty system. Check chip detectors. Tail Rotors Install rotor assembly. b. e. Main Rotors Install rotor assembly. Fuel and control. f. d. c. i. Test plugs. Flow check water/methanol system. c. Replace oil pump. leads. Replace drive shaft. Check controls for assembly and locking. Check Chip detector Check controls for range and sense of operation. Replace firewall shut off valve. Replace oil temperature bulb. Replace oil cooler. f. LIV a. LII a. turbine Change jet pipe. Change ignition vibrator. XLVI a. turbine Check glow plugs/ ignitors. b. Check system bonding. Rig RPM control. LIII a. Change plugs. f. d.T. d. i. Replace ignition unit. Ignition systems. Troubleshoot faulty system. Exhaust. Check calibration. Inspect welded repair. g. Check H. piston engines Replace PRT. c. Replace start relay. Rig power lever. Adjust pressure relief valve. Install trimmers. c. Replace thermocouples. b. b. LV a. g. b. Replace heat shields. b. Troubleshoot faulty system. Engine Controls Rig thrust lever. Troubleshoot faulty system. Troubleshoot faulty system. e. b. Troubleshoot faulty system. e. e. c. Adjust pedestal micro-switches. b. d. Replace waste gate. Check control sync (multi-eng). Pressure check cabin heater muff. piston Change magneto. b. Troubleshoot faulty system. f. Replace turbo-blower.T. c. Check filter(s). g. Check cranking speed. b. XLV a. i. h. c. b.by G T SELVAN Draft CAR-66 Dated 7th March 2011 f. d. Check fluid for quality. Ignition systems. Adjust water/methanol control unit. Perform oil dilution. Engine Indicating Replace engine instruments(s). Page 165 of 175 . Change shroud assembly. Starting Replace starter. Check timing. b. Troubleshoot faulty system Accessory gear boxes Replace gearbox. e. d. XLIX a. Check ignition unit. XLVII a. c. Rig mixture HP cock lever. L a. piston Replace exhaust gasket. Exhaust. Adjust density controller. c. Oil Change oil. d. c. e. e. Install new leads. d. c. c. Check H. Engine water injection Replace water/methanol pump. leads. correct d. Troubleshoot faulty system. XLVIII a. h. e. h. Replace oil tank. Turbines. e. d. Troubleshoot faulty system. LI a. Replace start control valve. by G T SELVAN Draft CAR-66 Dated 7th March 2011 Addendum III to AMC of CAR-66 Reserved Page 166 of 175 . identify the components or parts or the aircraft subject to FTS from the manufacturer’s documentation. Continuing training The interval between continuing training shall be established by the organisation employing such personnel. Level 2 Detailed training Objectives: The attendant should. but should not exceed two years. 2. use easily the manufacturer’s documentation from various sources and apply corrective action where appropriate. The continuing training shall include knowledge on evolution of material. such as Service Bulletins.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Addendum IV to AMC of CAR-66. 1. Airworthiness Directives. 4. have detailed information on how the above items affect the aircraft in the scope of the activity of the organisation or in the fleet.A. tools.45(d) Fuel Tank Safety training This appendix includes general instructions for providing training on Fuel Tank Safety issues. The personnel directly involved in Fuel Tank Safety (FTS) systems shall be qualified according to the following table: Page 167 of 175 . plan the action or apply a Service Bulletin and an Airworthiness Directive. 3. have the capacity to combine and apply the separate elements of knowledge in a logical and comprehensive manner. 5. Level of training required by this Annex is only level 2. Aircraft Maintenance Manual. 2. Airworthiness Limitations Items (ALI) and using theoretical fundamentals and specific examples. after the completion of the training: 1. documentation and manufacturer’s or competent authority’s directives. understand and carry out activities with the use of manufacturer and regulatory authority data providing instructions on design and maintenance. be able to give a detailed description of the concept of CDCCL. Component Maintenance Manual etc. 6. 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. systems and parts affected by FTS issues and having access to aircraft or component where typical examples of FTS issues can be shown. 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. 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 during the last 10 years.Explain 2 concepts to prevent explosions: (1) ignition source prevention and (2) flammability reduction. interpret and handle the improvements that have been made or are being made during fuel tank system maintenance. 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. c) awareness of any hazards working on the Fuel System. 4. The training should be made in appropriate facilities containing examples of components. and especially with a Flammability Reduction System using nitrogen. Part-66 licence holders in Maintenance aircraft and component organisation support maintenance organisations and certifying staff 2 Yes 3. energy needed for ignition etc.A. a).707. Page 168 of 175 . . the ‘fire triangle’. the effects of temperature and pressure. films and practical examples of the maintenance on fuel tank system is recommended. the behavior of those mixtures in an aviation environment. The use of pictures. The training shall include a representative number of repair and inspections as required by the maintenance programme showing the necessity of using the manufacturer’s data.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Organisation Personnel Level of knowledge 2 Continuing training Yes Part-66 licence holders in a The airworthiness continuing airworthiness review staff as required management organisation by M. and b) how in maintenance organisations mechanics can recognize. wire separation. bonding of components etc.1000. in fact improvement by a factor 100. iv) Explain the concepts that are being used: the results of SFAR 88 of the FAA and JAA INT/POL 25/12: modifications. their effects. clean working environment. v) Where relevant information can be found by the mechanics and how to use and interpret this information (maintenance manuals. and what was the ultimate goal. recording measures and results of inspections. safety precautions in maintenance/working with an FRS.by G T SELVAN Draft CAR-66 Dated 7th March 2011 ii) The major accidents and accident investigations and their conclusions. to identify unsafe conditions and to correct them. component maintenance manuals) vi) Fuel Tank Safety and Maintenance: fuel tank entry and exit procedures. to systematically improve fuel tank maintenance). what is meant by configuration control. the hazards of an FRS using nitrogen for maintenance. vii) Flammability reduction systems: reason for their presence. margins of fuel system safety improvements (from 106 to 10-9. viii) recording maintenance actions. Page 169 of 175 . airworthiness limitations and CDCCL. iii) SFARs from 14 CFR SFAR 88 of the FAA and JAA Internal Policy INT POL 25/12: reason of these documents. 1937. (f) (g) (h) (i) 2 All application forms referred in CAR-66 are placed at Appendix V Fees payable to DGCA on any count in accordance with Rule 62 of the Aircraft Rules. Basic Knowledge.by G T SELVAN Draft CAR-66 Dated 7th March 2011 Guidance Material (GM) to SECTION A of CAR-66 GM 66. Ministry of Civil Aviation. two passport size photographs and fees3 prescribed under Rule 62 of the Aircraft Rules. DGCA in the relevant category. Proof of Date of Birth. 3 Demand Draft should be drawn in favour of “Pay and Accounts Office. Certified true copies of logbook/ Work records indicating details of experience gained in cross representation section of maintenance tasks (as per Addendum to AMC of CAR 66 on form 19-10) related to the category of licence for which application is made. Copy of type Rating Course examination result sheet and course completion certificate. on CA Form 19-01.A. New Delhi”. 1937 may be paid in the form of scheduled Bank Demand Draft (DD) not drawn thirty days prior to the date of submission of application. Certified true copy of skill test result.10(a) Application2 1. copy of Course Completion Certificate issued by an Approved ab-initio AME Training organisation and copy of the concerned Training organisation’s “Certificate of Approval and Validity Schedule” or Degree in the relevant field of Engineering. Opposite Safdarjung Airport. New Delhi. stating that the candidate is medically fit and does not have colour blindness. Director General of Civil Aviation. (a) (b) (c) (d) (e) Certified true copy of Passport or voter ID or any other photo identity card issued by the Government. Page 170 of 175 . The name of the applicant and purpose for which the instrument is being tendered may be written on the back side of DD. In case of an applicant claiming one year experience relaxation. Issue of Aircraft Maintenance Engineers’ Licences Applicants meeting the eligibility. Medical fitness certificate on CA Form 19-06 issued by a physician holding at least MBBS Degree. 110003. Certified true copies of passing required modules from CEO or Basic Knowledge Certificate issued by CEO. Certified true copy of 10+2 certificate. Experience and other requirements stipulated in CAR-66 for issue of Aircraft Maintenance Engineers Licence shall apply to ‘The Director General of Civil Aviation (Attention: Airworthiness Directorate). with the following supporting documents. In case of an applicant claiming 50% experience relaxation. Original Aircraft Maintenance Engineer’s licence. e. The following titles shown against each category designator below are intended to provide a readily understandable indication of the job function: Category A: Line maintenance certifying engineer Category B1: Maintenance certifying engineer. Certified true copies of passing required modules from CEO or Basic Knowledge Certificate issued by CEO.A.by G T SELVAN Draft CAR-66 Dated 7th March 2011 2. c.20(a)Privileges 1. For the purposes of category A minor scheduled line maintenance means any minor check up to but not including the A check where functional tests can be carried out by the aircrew to ensure system serviceability. 2. Category C: Base maintenance certifying engineer 2. a. d.Avionic. 1937.A. Individual aircraft maintenance engineer’s licence holders need not be restricted to a single category. CAR-145 contains a typical example list of such tasks. copy of Course Completion Certificate issued by an Approved Training Organisation & copy of the concerned Training organisation’s “Certificate of Approval and Validity Schedule”. Category B2: Maintenance certifying engineer. experience and skill requirements for extension of an AME Licence and desirous of seeking extension of the AMEL held by them to cover additional “Category / Sub-Category Type Ratings” shall apply to the respective Regional / SubRegional Offices of DGCA on CA Form 19-02 with the following supporting documents and fees prescribed under Rule 62 of the Aircraft Rules. DGCA in the relevant category. any combination of categories may be granted. Extension of Aircraft Maintenance Engineer Licence Aircraft Maintenance Engineers meeting the knowledge. b.Mechanical. GM 66. Certified true copy of type rating course examination result and course completion certificate. In the case of an aircraft type not controlled by a Page 171 of 175 .A. to be certified under the category A certification authorisation as of minor scheduled maintenance or simple defect rectification are as specified in CAR-145 and agreed by DGCA. GM 66.20(a) Privileges 1. Certified true copy of skill test result. Tasks permitted by 66. Certified true copies of logbook/ Work records indicating details of experience gained in cross representation section of maintenance tasks (as per Addendum to AMC of CAR 66 on form 19-10) related to the category of licence for which application is made. Provided that each qualification requirement is satisfied.20 (a) 1. f. whereas category B1 and B2 should demonstrate Page 172 of 175 . which means that category A should demonstrate a limited but adequate level of knowledge.by G T SELVAN Draft CAR-66 Dated 7th March 2011 maintenance programme based upon the A/B/C/D check principle.A. The basis for this certification is that the maintenance has been carried out by competent mechanics and both category B1 and B2 staff have signed for the maintenance under their respective specialization.other than a simple go/no-go decision . minor scheduled line maintenance means any minor checks up to and including the weekly check or equivalent. 3. The category B2 will need to be qualified as category A in order to carry out simple mechanical tasks and be able to make certifications for such work. Defect rectification involving test equipment which requires an element of decision making in its application . other on-board test systems/equipment or by simple ramp test equipment. In all cases. 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. which can be understood by those with whom they are normally required to communicate.20 (b) 3. 4. − make written technical entries and any maintenance documentation entries. the level of understanding should be compatible with the level of certification privileges exercised.25 (a) Basic knowledge requirements The levels of knowledge are directly related to the complexity of certifications appropriate to the particular 66.A. GM 66. Category C personnel who also hold category B1 or B2 qualifications may perform both roles in base maintenance. GM 66.A. − communicate at such a level as to prevent any misunderstanding when exercising certification privileges. providing the serviceability of the system can be established by a simple self-test facility. The principal function of the category C certifying staff is to ensure that all required maintenance has been called up and signed off by the category B1 and B2 staff before issue of the certificate of release to service. Privileges 1.cannot be certified. The category B1 licence also permits the certification of work involving avionic systems. 2. The category C certification authorization permits certification of scheduled base maintenance by the issue of a single certificate of release to service for the complete aircraft after the completion of all such maintenance. − read and understand the maintenance organisation procedures. Holders of a CAR-66 aircraft maintenance engineer’s licence may not exercise certification privileges unless they have a general knowledge of the language used within the maintenance environment including knowledge of common aeronautical terms in the language.1 category. The experience should be acquired under the direct supervision of appropriately licenced or approved or authorised personnel on one to one basis. Filed visits and demonstrations carried out to group of students should be treated as an extension of theoretical class and not towards practical experience. While it is not feasible to establish a formula giving the required training duration in all cases. -recency on type.45(d) Type/task training and ratings 1. GM 66. Such experience may be combined with approved training so that periods of training can be intermixed with periods of experience rather like the apprenticeship. 2. line maintenance environment with one aircraft per week would permit limited experience compared with the constant base maintenance check environment.by G T SELVAN Draft CAR-66 Dated 7th March 2011 a complete level of knowledge in the appropriate subject modules. etc.A. Category C certifying staff should meet the relevant level of knowledge for B1 or B2. For example experience gained will depend upon the environment e. GM 66. -the quantity of the practical experience. the required duration may be approved through the organization’s MOE procedures.A. The required duration of practical training should be accepted on a case-by-case basis by the DGCA prior to the type rating endorsement. the following may be used as a guideline: (a) For a first type training course with no recent recorded maintenance experience four months practical training is required. The point being to gain sufficient experience in the environment of commercial maintenance / active approved maintenance organisation as opposed to only the training school environment with a non-operating aircraft.30 (a) Experience requirements Maintenance experience on an aircraft means the experience of being involved in maintenance tasks on aircraft which are being operated by airlines. air taxi organisations. construction and systems including engines.g. Page 173 of 175 . It is strongly recommended that the agreement on the practical training duration be reached before the training starts. (b) Some factors that may lead to a reduction in the maximum duration of 4 months practical training required are as follows: -experience on aircraft type of a similar technology. For applicants from a CAR-145 organisation. B2 and C. due to the availability of aircraft its duration may need be subsequently extended in order to fulfill the required list of supervised tasks.A. in the case of a structured OJT performed at line stations.by G T SELVAN Draft CAR-66 Dated 7th March 2011 -the quality of the practical experience. Modules marked (X) are deemed covered by virtue of licence already held by the applicant. As an example. It should be noted however that while AMC 66.A. GM 66. This includes the addition of similar type ratings on a CAR-66 licence (differences courses). Table 2 and 3 provide a list of knowledge examination modules which an applicant is required to pass for conversion of existing licence to CAR 66 licence. GM 66. 4.70 Conversion provisions Conversion tables in Appendix VII indicating various conversion provisions should be interpreted as given below: Table 1 provides synopsis of requirements for issue of CAR 66 licence in Category A. These tasks should reflect. The minimum two weeks practical training is normally required for all type training courses. However. Guidance to 66.A. B1 or B2 or C aircraft type ratings may be conducted by training organisations appropriately approved. at a minimum. Limited avionics system training should be included in the category B1 type training as the B1 privileges include the replacement of avionic line replaceable units. There may be cases where the practical differences training required is less than two weeks for example an engineer with a CAR-66 type licence in category B2 on an Airbus A330 with PW 4000 engines who takes a differences course to an Airbus A330 with Rolls Royce Trent engines. Electrical systems should be included in both type training categories.A. in either case DGCA should approve the duration of practical training for adding a type rating. B1.45(d) Type/task training and ratings CAR-66 Section A Appendix III type training levels are based upon ATA 104 (Air Transport Association) corresponding type training levels. or an organisation accepted by DGCA to conduct such examination. type Page 174 of 175 . it is the responsibility of the maintenance organisation to determine that the duration of practical training is commensurate with the candidate’s recency and experience. The type of tasks carried out. Except in those cases where the approved training organisation determines the practical training required.45(f) Type/task training and ratings The examinations in respect of category A. (X) indicates the required modules in applicable category/subcategory of the licence. 3. those tasks specified by the practical training needs matrix developed by the approved training organisation.45(d) specifies a practical training duration between 2 weeks and 4 months. 1 with type rating on Airbus A320 (IAE V2500) without any knowledge or skill examination. Knowledge Modules required to be passed to remove such limitation(s) are given in “Table 5”. the licence shall be converted to Category B1.g. For example. V2500 or CFM 56) if his Category A licence has to be converted to Category B1. till the time these requirements are met. An applicant holding a single/partial licence shall be required to pass appropriate knowledge paper module(s) as given in Table 2 and 3. However. the applicant’s licence shall be converted with Limitation(s) as given in “Table 4”.1 with type rating on Airbus A320 aircraft with limitation “Code 11” indicating that the licence holder can exercise certification privileges only on airframe. ********* Page 175 of 175 . The existing license of such applicant shall be converted to applicable category of airframe and engine combination only after he has passed the applicable module(s) and has met the experience and skill test requirements. an applicant holding “Category A” licence on Airbus A320 aircraft shall be required to pass modules 15 and 17.1 licence with type rating on Airbus A320 (IAE V2500 or CFM 56). Table 6 provides Codes for limitations of the converted licences. However. demonstrate 3 (or 4) years of practical maintenance experience and pass the skill test on the applicable Engine (e.by G T SELVAN Draft CAR-66 Dated 7th March 2011 rated licence in Category “A & C” on Airbus A320 & V2500 Engine shall be converted to Category B1.