CERTIFYING STAFF – PART-66Consolidated version of Part-66 of the Commission Regulation
EC No. 2042/2003, and related EASA Decisions (Acceptable Means of Compliance and Guidance Material), as amended
Revision May 2012
PART-66amended by
EU No. 1149/2011 EU No. 962/2010 EU No. 127/2010 EC No. 1056/2008 EC No. 376/2007 EC No. 707/2006
+ AMC/GM Part-66Decision 2003/19/RM amended by
Commission Regulation (EC) No. 2042/2003 of 20 November 2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisa-
tions and personnel involved in these tasks (Text with EEA relevance)
Initially published on 28/11/2003, Official Journal L 315, P. 0001 – 0165
Decision 2012/004/RDecision 2011/008/R Decision 2011/003/RDecision 2010/011/RDecision 2010/002/R Decision 2009/016/R
Decision 2009/008/R Decision 2008/003/RDecision 2007/018/RDecision 2007/009/RDecision 2007/003/R Decision 2005/07/R
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Luxembourg: Publications Office of the European Union, 2012
ISBN 978-92-9210-119-0 doi: 10.2822/33541
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Part-66 and AMC/GM rev. May 2012 Dear Reader
Dear Reader,You are finding before you the third printed Technical Publication of the Agency, the Part-66 consolidated rules. The format and layout is similar to the previous Technical Publications, Part-M and Part-145. The handbook starts with the newest amendment of Regulation (EC) No. 2042/2003, and is followed by Annex III of this regulation, Part-66. The related Acceptable Means of Compliance and Guidance Material have been included behind the respective Implementing Rules paragraphs also for this version. Again, a CD with the bookmarked and cross-referenced PDF of the handbook, as well as with the applicable Word forms, has been attached.
The next Technical Publications include updated versions of Part-M and Part-145. A probable new publication will be situated in the area of Flight Standards. It will most likely be in an electronic format. In this way, the Technical Publications service also seeks to respond to the varying needs of the different stakeholders.
Cologne, May 2012 Patrick Goudou Executive Director, EASA
Part-66 and AMC/GM rev. May 2012 Disclaimer
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Disclaimer
This Part-66 consolidated version has been prepared by the Agency in order to provide stakehold-ers with an updated and easy-to-read publication. It has been prepared by combining the officially published corresponding text of the regulation, and all amendments together with the acceptable means of compliance and guidance material adopted so far. However, this is not an official publi-cation and the Agency accepts no liability for damage of any kind resulting from the risks inherent in the use of this document.
Officially published documents, used to amalgamate all the elements into this consolidated ver-sion, may be found on the Agency’s webpage www.easa.europa.eu
The format of this publication has been adjusted in order to make it easier to read and for refer-ence purposes. Readers are invited and encouraged to report to [email protected] any perceived errors, or comments relating to this publication.
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Key to use of document
Implementing Rule (no coloured bar on the side of the page)
AMC – Acceptable Means of Compliance [pages with thick yellow bars (light grey)]
GM – Guidance Material [pages with thick green bars (dark grey)]
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GM 66.A.20(a) Privileges
1. The following definitions apply:
Electrical system means the aircraft electrical power supply source, plus the distribution system to the different components contained in the aircraft and relevant connectors. Lighting systems are also included in this definition. When working on cables and connectors which are part of these electrical systems, the following typical practices are included in the privileges:
• Continuity,insulationandbondingtechniquesandtesting;
• Crimpingandtestingofcrimpedjoints;
• Connectorpinremovalandinsertion;
• Wiringprotectiontechniques.
Avionics system means an aircraft system that transfers, processes, displays or stores analogue or digital data using data lines, data buses, coaxial cables, wireless or other data transmission medium, and includes the system’s components and connectors. Examples of avionics systems include the following:
• Autoflight;
• Communication,RadarandNavigation;
• Instruments(seeNOTEbelow);
• InFlightEntertainmentSystems;
• IntegratedModularAvionics(IMA);
• On-BoardMaintenanceSystems;
• InformationSystems;
• FlybyWireSystems(relatedtoATA27“FlightControls”);
• FibreOpticControlSystems.
NOTE: Instruments are formally includedwithin theprivilegesof theB2 licenceholders.However, maintenance on electromechanical and pitot-static components may also be releasedbyaB1licenseholder.
Simple test means a test described in approved maintenance data and meeting all the following criteria:
• Theserviceabilityofthesystemcanbeverifiedusingaircraftcontrols,switches,Built-inTestEquipment(BITE),CentralMaintenanceComputer(CMC)orexternaltestequip-ment not involving special training.
• Theoutcomeofthetestisauniquego–nogoindicationorparameter,whichcanbeasinglevalueoravaluewithinanintervaltolerance.Nointerpretationofthetestresultor interdependence of different values is allowed.
• Thetestdoesnotinvolvemorethan10actionsasdescribedintheapprovedmainte-nancedata(notincludingthoserequiredtoconfiguretheaircraftpriortothetest,i.e.jacking,flapsdown,etc,ortoreturntheaircrafttoitsinitialconfiguration).Pushingacontrol, switch or button, and reading the corresponding outcome may be considered as a single step even if the maintenance data shows them separated.
Text amended, including the regulation number amended by. [lines down side of amended text]
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66.A.15 Eligibility
An applicant for an aircraft maintenance licence shall be at least 18 years of age.
66.A.20 Privileges
(a) The following privileges shall apply:
1. A category A aircraft maintenance 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 certification authorisation referred to in point 145.A.35 of Annex II (Part-145). The certification privileges shall be restricted to work that the licence holder has personally performed in the maintenance organisation that issued the certification authorisation.
2. A category B1 aircraft maintenance licence shall permit the holder to issue certificates of release to service and to act as B1 support staff following:
- maintenance performed on aircraft structure, powerplant and mechanical and electri-cal systems,
- work on avionic systems requiring only simple tests to prove their serviceability and not requiring troubleshooting.
Category B1 includes the corresponding A subcategory.
3. A category B2 aircraft maintenance licence shall permit the holder:
(i) to issue certificates of release to service and to act as B2 support staff for following:
- maintenance performed on avionic and electrical systems, and
- electrical and avionics tasks within powerplant and mechanical systems, requiring only simple tests to prove their serviceability; and
(ii) 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 certification authorisation referred to in point 145.A.35 of Annex II (Part-145). This certification privilege shall be restricted to work that the licence holder has personally performed in the maintenance organisation which issued the certification authorisa-tion and limited to the ratings already endorsed in the B2 licence.
The category B2 licence does not include any A subcategory.
4. A category B3 aircraft maintenance licence shall permit the holder to issue certificates of release to service and to act as B3 support staff for :
- maintenance performed on aeroplane structure, powerplant and mechanical and elec-trical systems,
- work on avionic systems requiring only simple tests to prove their serviceability and not requiring troubleshooting.
5. A category C aircraft maintenance licence shall permit the holder to issue certificates of release to service following base maintenance on aircraft. The privileges apply to the air-craft in its entirety.
(b) The holder of an aircraft maintenance licence may not exercise its privileges unless:
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The 6 months maintenance experience in 2 years should be understood as consisting of two ele-ments: 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 working with the same organisation; or
- 6 months split up into different blocks, working 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 licence holder 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 licence holder hap-pens 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, con-tinuing airworthiness management or engineering activities. To avoid a too long period without experience, the working days should be spread over the intended 6-months period.
2. Nature of the experience:
Depending on the category of the aircraft maintenance licence, the following activities are con-sidered relevant for maintenance experience:
- Servicing;
- Inspection;
- Operational and functional testing;
- Troubleshooting;
- Repairing;
- Modifying;
- Changing component;
- Supervising these activities;
- Releasing aircraft to service.
For category A licence holders, the experience should include exercising the privileges, by means of performing tasks related to the authorization on at least one aircraft type for each licence subcategory. This means tasks as mentioned in AMC 145.A.30(g), including servicing, compo-nent changes and simple defect rectifications.
For category B1, B2 and B3, for every aircraft type rating included in the authorization the expe-rience should be on that particular aircraft or on a similar aircraft within the same licence (sub)category. Two aircraft can be considered as similar when they have similar technology, construc-tion and comparable systems, which means equally equipped with the following (as applicable to the licence category):
Part-66 and AMC/GM rev. May 2012 Contents
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Contents
Dear reader ............................................................................................................................................. 3Disclaimer .............................................................................................................................................. 4Key to use of document .......................................................................................................................... 5Article 1 Objective and scope ................................................................................................................. 10Article 2 Definitions ................................................................................................................................. 10Article 3 Continuing airworthiness requirements ................................................................................... 11Article 4 Maintenance organisation approvals ....................................................................................... 12Article 5 Certifying staff .......................................................................................................................... 12Article 6 Training organisation requirements ......................................................................................... 13Article 7 Entry into force ......................................................................................................................... 13Article 8 Agency measures ...................................................................................................................... 15
ANNEX III (Part-66) ....................................................................................................................... 1766.1 Competent authority ............................................................................................................ 17
AMC 66.1(a) .......................................................................................................................... 18
SECTION A TECHNICAL REQUIREMENTS .................................................................................. 19
SUBPART A AIRCRAFT MAINTENANCE LICENCE .................................................................................... 1966.A.1 Scope .................................................................................................................................... 1966.A.3 Licence categories ................................................................................................................ 20 GM 66.A.3 ............................................................................................................................. 2166.A.5 Aircraft groups ...................................................................................................................... 2266.A.10 Application ............................................................................................................................ 23 AMC 66.A.10 ......................................................................................................................... 2466.A.15 Eligibility ............................................................................................................................... 2566.A.20 Privileges............................................................................................................................... 25 GM 66.A.20(a) ...................................................................................................................... 27 AMC 66.A.20(b)2 .................................................................................................................. 29 GM 66.A.20(b)2 .................................................................................................................... 31 AMC 66.A.20(b)3 .................................................................................................................. 32 GM 66.A.20(b)4 .................................................................................................................... 3366.A.25 Basic knowledge requirements ............................................................................................ 34 AMC 66.A.25 ......................................................................................................................... 35 GM 66.A.25(a) ...................................................................................................................... 3666.A.30 Basic experience requirements ............................................................................................ 37 AMC 66.A.30(a) .................................................................................................................... 39 AMC 66.A.30(d) .................................................................................................................... 39 AMC 66.A.30(e) .................................................................................................................... 3966.A.40 Continued validity of the aircraft maintenance licence ....................................................... 40 GM 66.A.40 ........................................................................................................................... 4166.A.45 Endorsement with aircraft ratings ....................................................................................... 42 GM 66.A.45(b) ...................................................................................................................... 44 AMC 66.A.45(e) .................................................................................................................... 45 AMC 66.A.45(d), (e)3, (f)1 and (g)1 ...................................................................................... 46 GM 66.A.45 ........................................................................................................................... 4766.A.50 Limitations ............................................................................................................................ 50
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AMC 66.A.50(b) .................................................................................................................... 5166.A.55 Evidence of qualification ...................................................................................................... 5266.A.70 Conversion provisions .......................................................................................................... 52 GM 66.A.70 ........................................................................................................................... 53 GM 66.A.70(c) ....................................................................................................................... 54 GM 66.A.70(d) ...................................................................................................................... 55
SECTION B PROCEDURES FOR COMPETENT AUTHORITIES ............................................... 56
SUBPART A GENERAL ............................................................................................................................. 5666.B.1 Scope .................................................................................................................................... 5666.B.10 Competent authority ............................................................................................................ 5666.B.20 Record-keeping ..................................................................................................................... 56 AMC 66.B.20 ......................................................................................................................... 5866.B.25 Mutual exchange of information ......................................................................................... 5966.B.30 Exemptions ........................................................................................................................... 59
SUBPART B ISSUE OF AN AIRCRAFT MAINTENANCE LICENCE ............................................................... 6066.B.100 Procedure for the issue of an aircraft maintenance licence by the competent authority... 60 AMC 66.B.100 ....................................................................................................................... 6166.B.105 Procedure for the issue of an aircraft maintenance licence via the Part-145 approved maintenance organisation... ................................................................................................. 62 AMC 66.B.105 ....................................................................................................................... 6366.B.110 Procedure for the change of an aircraft maintenance licence to include an additional basic category or subcategory... ........................................................................................... 64 AMC 66.B.110 ....................................................................................................................... 6566.B.115 Procedure for the change of an aircraft maintenance licence to include an aircraft rating or to remove limitations... .................................................................................................... 66 AMC 66.B.115 ....................................................................................................................... 67 AMC 66.B.100 to 115 ........................................................................................................... 6766.B.120 Procedure for the renewal of an aircraft maintenance licence validity .............................. 68 AMC 66.B.120 ....................................................................................................................... 6966.B.125 Procedure for the conversion of licences including group ratings ...................................... 7066.B.130 Procedure for the direct approval of aircraft type training ................................................. 71 AMC 66.B.130 ....................................................................................................................... 72
SUBPART C EXAMINATIONS ................................................................................................................... 7366.B.200 Examination by the competent authority .............................................................................. 73 GM 66.B.200 ......................................................................................................................... 74
SUBPART D CONVERSION OF CERTIFYING STAFF QUALIFICATION ....................................................... 7766.B.300 General ................................................................................................................................. 77 GM 66.B.300 ......................................................................................................................... 7866.B.305 Conversion report for national qualifications ...................................................................... 79 AMC 66.B.305(a) ................................................................................................................... 80 GM 66.B.305(b)3 .................................................................................................................. 8166.B.310 Conversion report for approved maintenance organisations authorisations .......................... 82 AMC 66.B.310(a) ................................................................................................................... 83 AMC 66.B.310(b)3 ................................................................................................................ 83
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GM 66.B.310(b)3 .................................................................................................................. 84
SUBPART E EXAMINATION CREDITS ...................................................................................................... 8566.B.400 General ................................................................................................................................. 8566.B.405 Examination credit report .................................................................................................... 8566.B.410 Examination credit validity ................................................................................................... 86 GM 66.B.410 ......................................................................................................................... 87
SUBPART F CONTINUING OVERSIGHT...................................................................................................... 8866.B.500 Revocation, suspension or limitation of the aircraft maintenance licence ........................... 88
APPENDICES TO THE IMPLEMENTING RULES .......................................................................... 89
Appendix I Basic Knowledge Requirements ......................................................................................... 90Appendix II Basic Examination Standard ............................................................................................. 152Appendix III Aircraft Type Training and Examination Standard. On-the-Job Training ......................... 156 AMC to Section 1 of Appendix III ..................................................................................... 172 AMC to Paragraph 3.1(d) of Appendix III ......................................................................... 173 AMC to Paragraphs 1(b), 3.2 and 4.2 of Appendix III ....................................................... 176 AMC to Paragraph 1(c) of Appendix III ............................................................................. 177 AMC to Section 5 of Appendix III ..................................................................................... 177 AMC to Section 6 of Appendix III ..................................................................................... 177 AMC to Appendix III.......................................................................................................... 179Appendix IV Experience requirements for extending a Part-66 Aircraft Maintenance Licence ........... 180Appendix V Application Form - EASA Form 19..................................................................................... 181Appendix VI Aircraft maintenance licence referred to in Annex III (Part-66) - EASA Form 26 ............... 184
APPENDICES TO AMCs .................................................................................................................... 188
Appendix I Aircraft Type Ratings For Part-66 Aircraft Maintenance Licence .................................... 189Appendix II Aircraft Type Practical Experience and On-the-Job Training - List of Tasks .................... 221Appendix III Evaluation of the competence: assessment and assessors ............................................. 234
Part-66 and AMC/GM rev. May 2012 Article 1 Objective and scope
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Article 1 Objective and scope
1. This Regulation establishes common technical requirements and administrative procedures for ensuring the continuing airworthiness of aircraft, including any component for installation thereto, which are:
(a) registered in a Member State; or
(b) registered in a third country and used by an operator for which a Member State ensures oversight of operations.
2. Paragraph 1 shall not apply to aircraft the regulatory safety oversight of which has been transferred to a third country and which are not used by a Community operator, or to aircraft referred to in Annex II to the basic Regulation.
3. The provisions of this Regulation related to commercial air transport are applicable to licensed air carriers as defined by Community law.
Article 2 Definitions
Within the scope of the basic Regulation, the following definitions shall apply:
(a) “aircraft” means any machine that can derive support in the atmosphere from the reactions of the air other than reactions of the air against the earth’s surface;
(b) “certifying staff” means personnel responsible for the release of an aircraft or a component after maintenance;
(c) “component” means any engine, propeller, part or appliance;
(d) “continuing airworthiness” means all of the processes ensuring that, at any time in its operating life, the aircraft complies with the airworthiness requirements in force and is in a condition for safe operation;
(e) “JAA” means “Joint Aviation Authorities”;
(f) “JAR” means “Joint Aviation Requirements”;
(g) “large aircraft” means an aircraft, classified as an aeroplane with a maximum take-off mass of more than 5700 kg, or a multi-engined helicopter;
(h) “maintenance” means any one or combination of overhaul, repair, inspection, replacement, modification or defect rectification of an aircraft or component, with the exception of pre-flight inspection;
(i) “organisation” means a natural person, a legal person or part of a legal person. Such an organi-sation may be established at more than one location whether or not within the territory of the Member States;
(j) “pre-flight inspection” means the inspection carried out before flight to ensure that the aircraft is fit for the intended flight.
(k) “ELA1 aircraft” means the following European Light Aircraft:
(i) an aeroplane, sailplane or powered sailplane with a Maximum Take-off Mass (MTOM) less than 1000 kg that is not classified as complex motor-powered aircraft;
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(ii) a balloon with a maximum design lifting gas or hot air volume of not more than 3400 m3 for hot-air balloons, 1050 m3 for gas balloons, 300 m3 for tethered gas balloons;
(iii) an airship designed for not more than two occupants and a maximum design lifting gas or hot-air volume of not more than 2500 m3 for hot-air airships and 1000 m3 for gas airships;
(l) “LSA aircraft” means a light sport aeroplane which has all of the following characteristics:
(i) a Maximum Take-off Mass (MTOM) of not more than 600 kg;
(ii) a maximum stalling speed in the landing configuration (VS0) of not more than 45 knots Calibrated Airspeed (CAS) at the aircraft’s maximum certificated takeoff mass and most critical centre of gravity;
(iii) a maximum seating capacity of no more than two persons, including the pilot;
(iv) a single, non-turbine engine fitted with a propeller;
(v) a non-pressurised cabin;
(m) “principal place of business” means the head office or the registered office of the undertaking within which the principal financial functions and operational control of the activities referred to in this Regulation are exercised.
Article 3 Continuing airworthiness requirements
1. The continuing airworthiness of aircraft and components shall be ensured in accordance with the provisions of Annex I.
2. Organisations and personnel involved in the continuing airworthiness of aircraft and compo-nents, including maintenance, shall comply with the provisions of Annex I and where appropri-ate those specified in Articles 4 and 5.
3. By derogation from paragraph 1, the continuing airworthiness of aircraft holding a permit to fly shall be ensured on the basis of the specific continuing airworthiness arrangements as defined in the permit to fly issued in accordance with the Annex (Part-21) to Commission Regulation (EC) No 1702/2003.
4. For aircraft not used in commercial air transport, any airworthiness review certificate or equiva-lent document issued in accordance with the Member State requirements and valid on 28 September 2008 shall be valid until its expiration date or until 28 September 2009, whichever comes first. After the expiration of its validity, the competent authority may further re-issue or extend one time the airworthiness review certificate or equivalent document for one year, if allowed by the Member State requirements. Upon further expiration, the competent authority may further re-issue or extend one more time the airworthiness review certificate or equivalent document for one year, if allowed by the Member State requirements. No further re-issuance or extension is allowed. If the provisions of this point have been used, when transferring the registration of the aircraft within the EU, a new airworthiness review certificate shall be issued in accordance with M.A.904.
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Part-66 and AMC/GM rev. May 2012 Article 4 Maintenance organisation approvals
Article 4 Maintenance organisation approvals
1. Organisations involved in the maintenance of large aircraft or of aircraft used for commercial air transport, and components intended for fitment thereto, shall be approved in accordance with the provisions of Annex II.
2. Maintenance approvals issued or recognised by a Member State in accordance with the JAA requirements and procedures and valid before the entry into force of this Regulation shall be deemed to have been issued in accordance with this Regulation. For this purpose, by deroga-tion from the provisions of 145.B.50(2) under Annex II, level 2 findings associated with the dif-ferences between JAR 145 and Annex II may be closed within one year. Certificates of release to service and authorised release certificates issued by an organisation approved under JAA requirements during that one-year period shall be deemed to have been issued under this Regulation.
3. Personnel qualified to carry out and/or control a continued airworthiness non-destructive test of aircraft structures and/or components, on the basis of any standard recognised by a Member State prior to the entry into force of this Regulation as providing an equivalent level of qualifica-tion, may continue to carry out and/or control such tests.
4. Certificates of release to service and authorised release certificates issued before the date of entry into force of this Regulation by a maintenance organisation approved under the Member State requirements shall be deemed equivalent to those required under points M.A.801 and M.A.802 of Annex I (Part-M) respectively.
Article 5 Certifying staff
1. Certifying staff shall be qualified in accordance with the provisions of Annex III, except as pro-vided for in points M.A.606(h), M.A.607(b), M.A.801(d) and M.A.803 of Annex I and in point 145.A.30(j) of Annex II (Part 145) and Appendix IV to Annex II (Part 145).
2. Any aircraft maintenance licence and if any, the technical limitations associated with that licence, issued or recognised by a Member State in accordance with the JAA requirements and procedures and valid at the time of entry into force of this Regulation, shall be deemed to have been issued in accordance with this Regulation.
3. Certifying staff holding a licence issued in accordance with Annex III (Part-66) in a given catego-ry/sub-category are deemed to have the privileges described in point 66.A.20(a) of this Annex corresponding to such a category/sub-category. The basic knowledge requirements correspond-ing to these new privileges shall be deemed as met for the purpose of extending such licence to a new category/sub-category.
4. Certifying staff holding a licence including aircraft which do not require an individual type rating may continue to exercise his/her privileges until the first renewal or change, where the licence shall be converted following the procedure described in point 66.B.125 of Annex III (Part-66) to the ratings defined in point 66.A.45 of this Annex.
5. Conversion reports and Examination credit reports complying with the requirements applicable before this Regulation applies shall be deemed to be in compliance with this Regulation.
6. Until such time as this Regulation specifies requirements for certifying staff:
(i) for aircraft other than aeroplanes and helicopters,
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(ii) for components;
the requirements in force in the relevant Member State shall continue to apply, except for maintenance organisations located outside the European Union where the requirements shall be approved by the Agency.
Article 6 Training organisation requirements
1. Organisations involved in the training of personnel referred to in Article 5 shall be approved in accordance with Annex IV to be entitled:
(a) to conduct recognised basic training courses; and/or (b) to conduct recognised type training courses; and (c) to conduct examinations; and (d) to issue training certificates.
2. Any maintenance training organisation approval issued or recognised by a Member State in accordance with the JAA requirements and procedures and valid at the time of entry into force of this Regulation shall be deemed to have been issued in accordance with this Regulation. For this purpose, by derogation from the provisions of 147.B.130(b) under Annex IV, level 2 findings associated with the differences between JAR 147 and Annex IV may be closed within one year.
3. Basic training courses complying with the requirements applicable before this Regulation applies may be started until one year after the date by which this Regulation applies. Basic knowledge examinations conducted as part of these courses may comply with the requirements applicable before this Regulation applies.
4. Basic knowledge examinations complying with the requirements applicable before this Regulation applies and conducted by the competent authority or conducted by a maintenance training organisation approved in accordance with Annex IV (Part-147) while not being part of a basic training course, may be conducted until one year after the date by which this Regulation applies.
5. Type training courses and type examinations complying with the requirements applicable before this Regulation applies shall be started and finished not later than one year after the date by which this Regulation applies.
Article 7 Entry into force
1. This Regulation shall enter into force on the day following that of its publication in the Official Journal of the European Union.
2. By way of derogation from paragraph 1:
(a) the provisions of Annex I, except for points M.A.201(h)(2) and M.A.708(c), shall apply from 28 September 2005;
(b) point M.A.201(f) of Annex I shall apply to aircraft not involved in commercial air transport operated by third country carriers as from 28 September 2009.
3. By way of derogation from paragraph 1 and 2, Member States may elect not to apply:
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(a) the provisions of Annex I to aircraft not involved in commercial air transport, until 28 September 2009;
(b) the provisions of Annex I(I) to aircraft involved in commercial air transport, until 28 September 2008;
(c) the following provisions of Annex II, until 28 September 2006:
- 145.A.30(e), human factors elements,- 145.A.30(g) as applicable to large aircraft with a maximum take-off mass of more than
5700 kg,- 145.A.30(h)(1) as applicable to aircraft with a maximum take-off mass of more than 5700
kg,- 145.A.30(j)(1), Appendix IV,- 145.A.30(j)(2), Appendix IV;
(d) the following provisions of Annex II, until 28 September 2008:
- 145.A.30(g) as applicable to aircraft with a maximum take-off mass of 5700 kg or below,- 145.A.30(h)(1) as applicable to aircraft with a maximum take-off mass of 5700 kg or
below,- 145.A.30(h)(2);
(e) the provisions of Annex III, as applicable to aircraft with a maximum take-off mass above 5700 kg until 28 September 2005;
(f) the provisions of Annex III, as applicable to aircraft with a maximum take-off mass of 5700 kg or below until 28 September 2006.
(g) for aircraft not involved in commercial air transport other than large aircraft, the need to comply with Annex III (Part 66) in the following provisions, until 28 September 2011:
- M.A.606(g) and M.A.801(b)2 of Annex I (Part-M),- 145.A.30(g) and (h) of Annex II (Part-145).
(h)(1) for the maintenance of piston-engine non pressurized aeroplanes of 2000 Kg MTOM and below not involved in commercial air transport:
(i) until 28 September 2012, the requirement for the competent authority to issue aircraft maintenance licences in accordance with Annex III (Part-66), as new or as converted pursuant to point 66.A.70 of this Annex.
(ii) until 28 September 2014, the requirement to have certifying staff qualified in accord-ance with Annex III (Part-66) contained in the following provisions:
- M.A.606(g) and M.A.801(b)2 of Annex I (Part-M)- 145.A.30(g) and (h) of Annex II (Part-145).
(i)(1) for the maintenance of ELA1 aeroplanes not involved in commercial air transport, until 28 September 2015:
(i) the requirement for the competent authority to issue aircraft maintenance licences in accordance with Annex III (Part-66), as new or as converted pursuant to point 66.A.70 of this Annex.
(ii) the requirement to have certifying staff qualified in accordance with Annex III (Part-66) contained in the following provisions:
- M.A.606(g) and M.A.801(b)2 of Annex I (Part-M)- 145.A.30(g) and (h) of Annex II (Part-145).
(1) NOTE: Applicable from 17 November 2011 (Art.2, EU No. 1149/2011)
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4. Member States may issue approvals with regard to Annex II and Annex IV of a limited duration until 28 September 2007.
5. When a Member State makes use of the provisions of paragraphs 3 or 4 it shall notify the Commission and the Agency.
6. The Agency shall make an evaluation of the implication of the provisions of Annex I to this Regulation with a view to submitting an opinion to the Commission, including possible amend-ments to it, before 28 March 2005.
7. By way of derogation from paragraph 1:
(a) the provisions of point M.A.706(k) of Annex I (Part-M) shall apply as from 28 September 2010;
(b) the provisions of point 7.7 of Appendix I to Annex III (Part-66) shall apply as from 28 September 2010;
(c) maintenance organisations approved in accordance with Section A of subpart F of Annex I (Part-M) or Section A of Annex II (Part-145) may continue to issue Authorised Release Certificates by using the EASA Form 1 original issue, as laid down in Appendix II to the Annex I (Part-M) as well as Appendix I to the Annex II (Part 145), until 28 September 2010;
(d) competent authorities may continue to issue certificates, previous issue, as laid down in Appendices III, V and VI to Annex I (Part-M), Appendix III to Annex II (Part-145), Appendix V to Annex III (Part-66) or Appendix II to Annex IV (Part-147) to Regulation (EC) No 2042/2003 in force prior to the entry into force of this regulation, until 28 September 2010;
8.(2) For the purpose of time limits contained in points 66.A.25, 66.A.30 and Appendix III of Annex III (Part-66) related to basic knowledge examinations, basic experience, theoretical type training and examinations, practical training and assessment, type examinations and On-the-Job train-ing completed before this regulation applies, the origin of time shall be the date by which this Regulation applies.
9.(2) The Agency shall submit an opinion to the Commission including proposals for a simple and proportionate system for the licensing of certifying staff involved in the maintenance of ELA1 aeroplanes as well as aircraft other than aeroplanes and helicopters.
Article 8(2) Agency Measures
1. The Agency shall develop acceptable means of compliance (hereinafter called "AMC") that com-petent authorities, organisations and personnel may use to demonstrate compliance with the provisions of the Annexes to this Regulation.
2. The AMC issued by the Agency shall neither introduce new requirements nor alleviate the requirements of the Annexes to this Regulation.
3. Without prejudice to Articles 54 and 55 of Regulation (EC) No 216/2008, when the acceptable means of compliance issued by the Agency are used, the related requirements of the Annexes to this Regulation shall be considered as met without further demonstration.
(2) NOTE: Applicable from 1 August 2012 (Art. 2, EU No. 1149/2011)
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Part-66 and AMC/GM rev. May 2012
This Regulation shall be binding in its entirety and directly applicable in all Member States.
Done at Brussels, 20 November 2003
For the Commission Loyola DE PALACIO Vice-President
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Part-66 and AMC/GM rev. May 2012 66.1 Competent authority
ANNEX III (Part-66)
66.1 Competent authority
(a) For the purpose of this Annex (Part-66), the competent authority shall be:
1. the authority designated by the Member State to whom a person first applies for the issu-ance of an aircraft maintenance licence, or
2. the authority designated by another Member State, in case it would be different, subject to agreement with the authority referred to in point 1. In that case, the licence referred to in point 1 shall be revoked, all the records mentioned in point 66.B.20 shall be transferred and a new licence shall be issued on the basis of these records.
(b) The Agency shall be responsible for defining:
1. the list of aircraft types; and
2. what airframe/engine combinations are included in each particular aircraft type rating.
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Part-66 and AMC/GM rev. May 2012 AMC 66.1(a)
AMC 66.1(a)
A competent authority may be a ministry, a national aviation authority, or any aviation body desig-nated by the Member State and located within that Member State. A Member State may designate more than one competent authority to cover different areas of responsibility, as long as the designa-tion decision contains a list of the competencies of each authority and there is only one competent authority responsible for each given area of responsibility.
The purpose of 66.1(a)2 is to allow the possibility for a person who already holds a Part-66 licence issued by one Member State (i.e. Member State X) to replace it by a Part-66 licence issued by anoth-er Member State (i.e. Member State Y). This may be useful, for example, in cases where a person holding a licence from “Member State X” is developing his/her career in a maintenance organisa-tion located in “Member State Y”. In this case, this person may need to endorse new type ratings based on courses directly approved by the competent authority of “Member State Y” or may need to endorse new licence (sub)categories based on basic examinations performed by the competent authority of “Member State Y”.
Part-66 and AMC/GM rev. May 2012 66.A.1 Scope
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SECTION A TECHNICAL REQUIREMENTS
SUBPART A AIRCRAFT MAINTENANCE LICENCE
66.A.1 Scope
This section defines the aircraft maintenance licence and establishes the requirements for applica-tion, issue and continuation of its validity.
Part-66 and AMC/GM rev. May 2012 66.A.3 Licence categories
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66.A.3 Licence categories
(a) Aircraft maintenance licences include the following categories:
- Category A
- Category B1
- Category B2
- Category B3
- Category C
(b) Categories A and B1 are subdivided into subcategories relative to combinations of aeroplanes, helicopters, turbine and piston engines. These subcategories are:
- A1 and B1.1 Aeroplanes Turbine
- A2 and B1.2 Aeroplanes Piston
- A3 and B1.3 Helicopters Turbine
- A4 and B1.4 Helicopters Piston
(c) Category B3 is applicable to piston-engine non-pressurized aeroplanes of 2000 Kg MTOM and below.
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GM 66.A.3 Licence categories
Individual aircraft maintenance licence holders need not be restricted to a single category. Provided that each qualification requirement is satisfied, any combination of categories may be granted.
Part-66 and AMC/GM rev. May 2012 66.A.5 Aircraft groups
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66.A.5 Aircraft groups
For the purpose of ratings on aircraft maintenance licences, aircraft shall be classified in the follow-ing groups:
1. Group 1: complex motor-powered aircraft as well as multiple engine helicopters, aeroplanes with maximum certified operating altitude exceeding FL290, aircraft equipped with fly-by-wire systems and other aircraft requiring an aircraft type rating when defined so by the Agency.
2. Group 2: aircraft other than those in Group 1 belonging to the following subgroups:
- sub-group 2a: single turbo-propeller engine aeroplanes
- sub-group 2b: single turbine engine helicopters
- sub-group 2c: single piston engine helicopters
3. Group 3: piston engine aeroplanes other than those in Group 1.
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66.A.10 Application
(a) An application for an aircraft maintenance licence or change to such licence shall be made on an EASA Form 19 (see Appendix V) in a manner established by the competent authority and submitted thereto.
(b) An application for the change to an aircraft maintenance licence shall be made to the competent authority of the Member State that issued the aircraft maintenance licence.
(c) In addition to the documents required in points 66.A.10(a), 66.A.10(b) and 66.B.105, as appro-priate, the applicant for additional basic categories or subcategories to an aircraft maintenance licence shall submit his/her current original aircraft maintenance licence to the competent authority together with the EASA Form 19.
(d) Where the applicant for change of the basic categories qualifies for such change via the proce-dure referred to in point 66.B.100 in a Member State other than the Member State which issued the license, the application shall be sent to the competent authority referred to in point 66.1.
(e) Where the applicant for change of the basic categories qualifies for such change via the proce-dure referred to in point 66.B.105 in a Member State other than the Member State which issued the license, the maintenance organisation approved in accordance with Annex II (Part-145) shall send the aircraft maintenance licence together with the EASA Form 19 to the competent author-ity referred to in point 66.1 for stamp and signature of the change or reissue of the licence, as appropriate.
(f) Each application shall be supported by documentation to demonstrate compliance with the applicable theoretical knowledge, practical training and experience requirements at the time of application.
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Part-66 and AMC/GM rev. May 2012 AMC 66.A.10 Application
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1. Maintenance experience should be written up 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 bland statement “X years maintenance experience completed” is not acceptable. A log book of maintenance experience is desirable and some competent authorities may require such log book to be kept. It is acceptable to cross-refer in the EASA Form 19 to other documents containing information on maintenance.
2. Applicants claiming the maximum reduction in 66.A.30(a) total experience based upon success-ful completion of 147.A.200 approved basic training should include the Part-147 certificate of recognition for approved basic training.
3. Applicants claiming reduction in 66.A.30(a) total experience based upon successful completion of technical training in an organisation or institute recognised by the competent authority as a competent organisation or institute should include the relevant certificate of successful comple-tion of training.
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66.A.15 Eligibility
An applicant for an aircraft maintenance licence shall be at least 18 years of age.
66.A.20 Privileges
(a) The following privileges shall apply:
1. A category A aircraft maintenance 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 certification authorisation referred to in point 145.A.35 of Annex II (Part-145). The certification privileges shall be restricted to work that the licence holder has personally performed in the maintenance organisation that issued the certification authorisation.
2. A category B1 aircraft maintenance licence shall permit the holder to issue certificates of release to service and to act as B1 support staff following:
- maintenance performed on aircraft structure, powerplant and mechanical and electri-cal systems,
- work on avionic systems requiring only simple tests to prove their serviceability and not requiring troubleshooting.
Category B1 includes the corresponding A subcategory.
3. A category B2 aircraft maintenance licence shall permit the holder:
(i) to issue certificates of release to service and to act as B2 support staff for following:
- maintenance performed on avionic and electrical systems, and
- electrical and avionics tasks within powerplant and mechanical systems, requiring only simple tests to prove their serviceability; and
(ii) 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 certification authorisation referred to in point 145.A.35 of Annex II (Part-145). This certification privilege shall be restricted to work that the licence holder has personally performed in the maintenance organisation which issued the certification authorisa-tion and limited to the ratings already endorsed in the B2 licence.
The category B2 licence does not include any A subcategory.
4. A category B3 aircraft maintenance licence shall permit the holder to issue certificates of release to service and to act as B3 support staff for :
- maintenance performed on aeroplane structure, powerplant and mechanical and elec-trical systems,
- work on avionic systems requiring only simple tests to prove their serviceability and not requiring troubleshooting.
5. A category C aircraft maintenance licence shall permit the holder to issue certificates of release to service following base maintenance on aircraft. The privileges apply to the air-craft in its entirety.
(b) The holder of an aircraft maintenance licence may not exercise its privileges unless:
Part-66 and AMC/GM rev. May 2012 66.A.20 Privileges
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1. in compliance with the applicable requirements of Annex I (Part-M) and Annex II (Part-145); and
2. in the preceding two-year period he/she has, either had six months of maintenance experi-ence in accordance with the privileges granted by the aircraft maintenance licence or, met the provision for the issue of the appropriate privileges; and
3. he/she has the adequate competence to certify maintenance on the corresponding aircraft; and
4. he/she is able to read, write and communicate to an understandable level in the language(s) in which the technical documentation and procedures necessary to support the issue of the certificate of release to service are written.
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1. The following definitions apply:
Electrical system means the aircraft electrical power supply source, plus the distribution system to the different components contained in the aircraft and relevant connectors. Lighting systems are also included in this definition. When working on cables and connectors which are part of these electrical systems, the following typical practices are included in the privileges:
• Continuity, insulation and bonding techniques and testing;
• Crimping and testing of crimped joints;
• Connector pin removal and insertion;
• Wiring protection techniques.
Avionics system means an aircraft system that transfers, processes, displays or stores analogue or digital data using data lines, data buses, coaxial cables, wireless or other data transmission medium, and includes the system’s components and connectors. Examples of avionics systems include the following:
• Autoflight;
• Communication, Radar and Navigation;
• Instruments (see NOTE below);
• In Flight Entertainment Systems;
• Integrated Modular Avionics (IMA);
• On-Board Maintenance Systems;
• Information Systems;
• Fly by Wire Systems (related to ATA27 “Flight Controls”);
• Fibre Optic Control Systems.
NOTE: Instruments are formally included within the privileges of the B2 licence holders. However, maintenance on electromechanical and pitot-static components may also be released by a B1 license holder.
Simple test means a test described in approved maintenance data and meeting all the following criteria:
• The serviceability of the system can be verified using aircraft controls, switches, Built-in Test Equipment (BITE), Central Maintenance Computer (CMC) or external test equip-ment not involving special training.
• The outcome of the test is a unique go – no go indication or parameter, which can be a single value or a value within an interval tolerance. No interpretation of the test result or interdependence of different values is allowed.
• The test does not involve more than 10 actions as described in the approved mainte-nance data (not including those required to configure the aircraft prior to the test, i.e. jacking, flaps down, etc, or to return the aircraft to its initial configuration). Pushing a control, switch or button, and reading the corresponding outcome may be considered as a single step even if the maintenance data shows them separated.
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Troubleshooting means the procedures and actions necessary, using approved maintenance data, in order to identify the root cause of a defect or malfunction. It may include the use of BITE or external test equipment.
Line maintenance means any maintenance that is carried out before flight to ensure that the aircraft is fit for the intended flight. It may include:
• 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 powerplant 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 performed by a line maintenance organisation provided all requirements are fulfilled. The Member State will prescribe the conditions under which these tasks may be performed.
Base Maintenance means any task falling outside the criteria that are given above for Line Maintenance.
NOTE:
Aircraft maintained in accordance with "progressive" type programmes need to be indi-vidually assessed in relation to this paragraph. In principle, the decision to allow some "progressive" checks to be carried out is determined by the assessment that all tasks within the particular check can be carried out safely to the required standards at the designated line maintenance station.
2. The category B3 licence does not include any A subcategory. Nevertheless, this does not pre-vent the B3 licence holder from releasing maintenance tasks typical of the A1.2 subcategory for piston-engine non-pressurized aeroplanes of 2000 Kg MTOM and below, within the limitations contained in the B3 licence.
3. The category C licence 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. The basis for this certification is that the maintenance has been carried out by competent mechanics and category B1, B2 and B3 support staff, as appropriate, have signed for the maintenance tasks under their respective specialisation. The principal function of the cat-egory C certifying staff is to ensure that all required maintenance has been called up and signed off by the category B1, B2 and B3 support staff, as appropriate, before issue of the certificate of release to service. Only category C personnel who also hold category B1, B2 or B3 qualifications may perform both roles in base maintenance.
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Part-66 and AMC/GM rev. May 2012 AMC 66.A.20(b)2 Privileges
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The 6 months maintenance experience in 2 years should be understood as consisting of two ele-ments: 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 working with the same organisation; or
- 6 months split up into different blocks, working 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 licence holder 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 licence holder hap-pens 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, con-tinuing airworthiness management or engineering activities. To avoid a too long period without experience, the working days should be spread over the intended 6-months period.
2. Nature of the experience:
Depending on the category of the aircraft maintenance licence, the following activities are con-sidered relevant for maintenance experience:
- Servicing;
- Inspection;
- Operational and functional testing;
- Troubleshooting;
- Repairing;
- Modifying;
- Changing component;
- Supervising these activities;
- Releasing aircraft to service.
For category A licence holders, the experience should include exercising the privileges, by means of performing tasks related to the authorization on at least one aircraft type for each licence subcategory. This means tasks as mentioned in AMC 145.A.30(g), including servicing, compo-nent changes and simple defect rectifications.
For category B1, B2 and B3, for every aircraft type rating included in the authorization the expe-rience should be on that particular aircraft or on a similar aircraft within the same licence (sub)category. Two aircraft can be considered as similar when they have similar technology, construc-tion and comparable systems, which means equally equipped with the following (as applicable to the licence category):
