Commission Regulation (EU) No 1321/2014 of 26 November 2014 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks Text with EEA relevance

Type Regulation
Publication 2014-12-17
Last updated 2026-08-07
State In force
Department European Commission
Source EUR-Lex
articles 9
Reform history JSON API
  • (c) The competent authority shall establish procedures for the participation in a mutual exchange of all necessary information and assistance with any other competent authorities concerned, whether from the same Member State or from other Member States, including on:
  • (1) all findings raised and any follow-up actions taken as a result of the oversight of persons and organisations that carry out activities in the territory of a Member State, but certified by the competent authority of another Member State or by the Agency;
  • (2) information stemming from mandatory and voluntary occurrence reporting as required by 145.A.60.
  • (d) A copy of the procedures related to the management system and their amendments shall be made available to the Agency for the purpose of standardisation.
  • (e) In addition to the requirements contained in point (a), the management system established and maintained by the competent authority shall comply with Annex I (Part-IS.AR) to Implementing Regulation (EU) 2023/203 in order to ensure the proper management of information security risks which may have an impact on aviation safety.
145.B.205   Allocation of tasks
  • (a) The competent authority may allocate tasks related to the initial certification or to the continuing oversight of organisations subject to Regulation (EU) 2018/1139 and its delegated and implementing acts, to qualified entities. When allocating tasks, the competent authority shall ensure that it has:
  • (1) put a system in place to initially and continuously assess whether the qualified entity complies with Annex VI to Regulation (EU) 2018/1139. That system and the results of the assessments shall be documented;
  • (2) established a written agreement with the qualified entity, approved by both parties at the appropriate management level, which stipulates:
  • (i) the tasks to be performed;
  • (ii) the declarations, reports and records to be provided;
  • (iii) the technical conditions to be met when performing such tasks;
  • (iv) the related liability coverage;
  • (v) the protection given to the information acquired when carrying out such tasks.
  • (b) The competent authority shall ensure that the internal audit process and safety risk management process established pursuant to point 145.B.200(a)(5) cover all the certification and continuing oversight tasks performed by the qualified entity on its behalf.
  • (c) For the certification and oversight of the organisation’s compliance with point 145.A.200A, the competent authority may allocate tasks to qualified entities in accordance with point (a), or to any relevant authority responsible for information security or cybersecurity within the Member State. When allocating tasks, the competent authority shall ensure that:
  • (1) all aspects related to aviation safety are coordinated and taken into account by the qualified entity or relevant authority;
  • (2) the results of the certification and oversight activities performed by the qualified entity or relevant authority are integrated in the overall certification and oversight files of the organisation;
  • (3) its own information security management system established in accordance with point 145.B.200(e) covers all the certification and continuing oversight tasks performed on its behalf.
145.B.210   Changes in the management system
  • (a) The competent authority shall have a system in place to identify the changes that affect its capability to perform its tasks and discharge its responsibilities as defined in Regulation (EU) 2018/1139 and its delegated and implementing acts. That system shall enable the competent authority to take action necessary to ensure that its management system remains adequate and effective.
  • (b) The competent authority shall update in a timely manner its management system to reflect any changes to Regulation (EU) 2018/1139 and its delegated and implementing acts so as to ensure its effective implementation.
  • (c) The competent authority shall notify the Agency of any changes affecting its capability to perform its tasks and discharge its responsibilities as provided for in Regulation (EU) 2018/1139 and its delegated and implementing acts.
145.B.220   Record-keeping
  • (a) The competent authority shall establish a record-keeping system that allows the adequate storage, accessibility and reliable traceability of:
  • (1) the management system’s documented policies and procedures;
  • (2) the training, qualifications and authorisations of its personnel;
  • (3) the allocation of tasks, covering the elements required by point 145.B.205, as well as the details of tasks allocated;
  • (4) certification processes and continuing oversight of certified organisations, including:
  • (i) the application for an organisation certificate;
  • (ii) the competent authority’s continuing oversight programme, including all the assessments, audits and inspection records;
  • (iii) the organisation certificate, including any changes to it;
  • (iv) a copy of the oversight programme, listing the dates when audits are due and when audits were carried out;
  • (v) copies of all formal correspondence;
  • (vi) recommendations for the issue or continuation of a certificate, details of findings and actions taken by the organisations to close those findings, including the date of closure, enforcement actions and observations;
  • (vii) any assessment, audit and inspection report issued by another competent authority pursuant to point 145.B.300(d);
  • (viii) copies of all the organisation MOEs or manuals, and of any amendments to them;
  • (ix) copies of any other documents approved by the competent authority;
  • (5) documents supporting the use of alternative means of compliance;
  • (6) safety information provided in accordance with point 145.B.125 and follow-up measures;
  • (7) the use of safeguard and flexibility provisions in accordance with Article 70, Article 71(1) and Article 76(4) of Regulation (EU) 2018/1139.
  • (b) The competent authority shall maintain a list of all the organisation certificates it has issued.
  • (c) All the records referred to in points (a) and (b) shall be kept for a minimum period of 5 years, subject to applicable data protection law.
  • (d) All the records referred to in points (a) and (b) shall be made available, upon request, to a competent authority of another Member State or to the Agency.
145.B.300   Oversight principles
  • (a) The competent authority shall verify:
  • (1) compliance with the requirements that are applicable to organisations, prior to issuing an organisation certificate;
  • (2) continued compliance with the applicable requirements of the organisations it has certified;
  • (3) the implementation of appropriate safety measures mandated by the competent authority in accordance with points 145.B.135(c) and (d).
  • (b) This verification shall:
  • (1) be supported by documentation specifically intended to provide personnel responsible for oversight with guidance to perform their functions;
  • (2) provide the organisations concerned with the results of oversight activities;
  • (3) be based on assessments, audits and inspections and, if needed, unannounced inspections;
  • (4) provide the competent authority with the evidence needed in case further action is required, including the measures provided for in point 145.B.350.
  • (c) The competent authority shall establish the scope of the oversight set out in points (a) and (b) taking into account the results of past oversight activities and the safety priorities.
  • (d) If the facilities of an organisation are located in more than one State, the competent authority, as defined in point 145.1, may agree to have the oversight tasks performed by the competent authority(ies) of the Member State(s) where the facilities are located, or by the Agency for facilities that are located outside a territory for which Member States are responsible under the Chicago Convention. Any organisation that is subject to such an agreement shall be informed of its existence and of its scope.
  • (e) For any oversight activities that are performed at facilities located in a Member State other than where the organisation has its principal place of business, the competent authority, as defined in point 145.1, shall inform the competent authority of that Member State before performing any on-site audit or inspection of the facilities.
  • (f) The competent authority shall collect and process any information deemed necessary for performing oversight activities.
  • (g) With regard to the certification and oversight of the organisation’s compliance with point 145.A.200A, in addition to complying with points (a) to (f) of this point, the competent authority shall review any approval granted under point IS.I.OR.200(e) of Annex II to Implementing Regulation (EU) 2023/203 following the applicable oversight audit cycle and whenever changes are implemented in the scope of work of the organisation.
145.B.305   Oversight programme
  • (a) The competent authority shall establish and maintain an oversight programme covering the oversight activities required by point 145.B.300.
  • (b) The oversight programme shall take into account the specific nature of the organisation, the complexity of its activities, the results of past certification or oversight activities, or both, and it shall be based on the assessment of the associated risks. It shall include, within each oversight planning cycle:
  • (1) assessments, audits and inspections, including, as appropriate:
  • (i) management system assessments and process audits;
  • (ii) product audits of a relevant sample of the maintenance carried out by the organisation;
  • (iii) sampling of the airworthiness reviews performed;
  • (iv) unannounced inspections;
  • (2) meetings convened between the accountable manager and the competent authority to ensure that both parties remain informed of all significant issues.
  • (c) The oversight planning cycle shall not exceed 24 months.
  • (d) Notwithstanding point (c), the oversight planning cycle may be extended to 36 months if the competent authority has established that during the previous 24 months:
  • (1) the organisation has demonstrated that it can effectively identify aviation safety hazards and manage the associated risks;
  • (2) the organisation has continuously demonstrated compliance with point 145.A.85 and it has full control over all changes;
  • (3) no level 1 findings have been issued;
  • (4) all corrective actions have been implemented within the time period that was accepted or extended by the competent authority as provided for in point 145.B.350. Notwithstanding point (c), the oversight planning cycle may be further extended to a maximum of 48 months if, in addition to the conditions provided in points (d)(1) to (4), the organisation has established, and the competent authority has approved, an effective continuous system for reporting to the competent authority on the safety performance and regulatory compliance of the organisation itself.
  • (e) The oversight planning cycle may be shortened if there is evidence that the safety performance of the organisation has decreased.
  • (f) The oversight programme shall include records of the dates when assessments, audits, inspections and meetings are due, and when assessments, audits, inspections and meetings have been effectively carried out.
  • (g) At the completion of each oversight planning cycle, the competent authority shall issue a recommendation report on the continuation of the approval, reflecting the results of the oversight.
145.B.310   Initial certification procedure
  • (a) Upon receiving an application from an organisation for the initial issue of a certificate, the competent authority shall verify the organisation’s compliance with the applicable requirements.
  • (b) A meeting with the accountable manager of the organisation shall be convened at least once during the investigation for initial certification to ensure that that person understands his or her role and accountability.
  • (c) The competent authority shall record all the findings issued, closure actions as well as the recommendations for the issue of the certificate.
  • (d) The competent authority shall confirm to the organisation in writing all the findings raised during the verification. For initial certification, all findings must be corrected to the satisfaction of the competent authority before the certificate can be issued.
  • (e) When satisfied that the organisation complies with the applicable requirements, the competent authority shall:
  • (1) issue the certificate as established in Appendix III ‘EASA Form 3-145’ in accordance with the class and rating system provided for in Appendix II;
  • (2) formally approve the MOE.
  • (f) The certificate reference number shall be included on the EASA Form 3-145 certificate in a manner specified by the Agency.
  • (g) The certificate shall be issued for an unlimited duration. The privileges and the scope of the activities that the organisation is approved to conduct, including any limitations as applicable, shall be specified in the terms of approval attached to the certificate.
  • (h) To enable the organisation to implement changes without prior competent authority approval in accordance with point 145.A.85(c), the competent authority shall approve the relevant MOE procedure that sets out the scope of such changes and describes how such changes will be managed and notified to the competent authority.
145.B.330   Changes – organisations
  • (a) Upon receiving an application for a change that requires prior approval, the competent authority shall verify the organisation’s compliance with the applicable requirements before issuing the approval.
  • (b) The competent authority shall establish the conditions under which the organisation may operate during the change unless the competent authority determines that the organisation’s certificate needs to be suspended.
  • (c) When it is satisfied that the organisation complies with the applicable requirements, the competent authority shall approve the change.
  • (d) Without prejudice to any additional enforcement measures, if the organisation implements changes requiring prior approval without having received the approval of the competent authority pursuant to point (c), the competent authority shall consider the need to suspend, limit or revoke the organisation’s certificate.
  • (e) For changes not requiring prior approval, the competent authority shall include the review of such changes in its continuing oversight in accordance with the principles set forth in point 145.B.300. If any non-compliance is found, the competent authority shall notify the organisation, request further changes, and act in accordance with point 145.B.350.
145.B.330A   Changes to the information security management system
  • (a) For changes managed and notified to the competent authority in accordance with the procedure set out in point IS.I.OR.255(a) of Annex II (Part-IS.I.OR) to Implementing Regulation (EU) 2023/203, the competent authority shall include the review of such changes in its continuing oversight in accordance with the principles laid down in point 145.B.300. If any non-compliance is found, the competent authority shall notify the organisation thereof, request further changes and act in accordance with point 145.B.350.
  • (b) For other changes requiring an application for approval in accordance with point IS.I.OR.255(b) of Annex II (Part-IS.I.OR) to Implementing Regulation (EU) 2023/203:
  • (1) upon receiving the application for the change, the competent authority shall check the organisation’s compliance with the applicable requirements before issuing the approval;
  • (2) the competent authority shall establish the conditions under which the organisation may operate during the implementation of the change;
  • (3) if it is satisfied that the organisation complies with the applicable requirements, the competent authority shall approve the change.
145.B.350   Findings and corrective actions; observations
  • (a) The competent authority shall have a system in place to analyse findings for their safety significance.
  • (b) A level 1 finding shall be issued by the competent authority when any significant non-compliance is detected with the applicable requirements of Regulation (EU) 2018/1139 and its delegated and implementing acts, with the organisation’s procedures and manuals, or with the organisation’s certificate including the terms of approval, which lowers safety or seriously endangers flight safety. Level 1 findings shall also include:
  • (1) any failure to grant the competent authority access to the organisation’s facilities referred to in point 145.A.140 during normal operating hours and after two written requests;
  • (2) obtaining the organisation certificate or maintaining its validity by falsification of the submitted documentary evidence;
  • (3) any evidence of malpractice or fraudulent use of the organisation certificate;
  • (4) the lack of an accountable manager.
  • (c) A level 2 finding shall be issued by the competent authority when any non-compliance is detected with the applicable requirements of Regulation (EU) 2018/1139 and its delegated and implementing acts, with the organisation’s procedures and manuals, or with the organisation’s certificate including the terms of approval, which is not classified as a level 1 finding.
  • (d) When a finding is detected during oversight or by any other means, the competent authority shall, without prejudice to any additional action required by Regulation (EU) 2018/1139 and its delegated and implementing acts, communicate in writing the finding to the organisation and request corrective action to address the non-compliance identified. If a level 1 finding directly relates to an aircraft, the competent authority shall inform the competent authority of the Member State in which the aircraft is registered.
  • (1) If there are any level 1 findings, the competent authority shall take immediate and appropriate action to prohibit or limit the activities of the organisation involved and, if appropriate, it shall take action to revoke the certificate or to limit or suspend it in whole or in part, depending on the extent of the level 1 finding, until successful corrective action has been taken by the organisation.
  • (2) If there are any level 2 findings, the competent authority shall:
  • (i) grant the organisation a corrective action implementation period that is appropriate to the nature of the finding, and that in any case shall initially not be more than 3 months. The period shall commence from the date of the written communication of the finding to the organisation requesting corrective action to address the non-compliance identified. At the end of that period, and subject to the nature of the finding, the competent authority may extend the 3-month period provided that a corrective action plan has been agreed with the competent authority;
  • (ii) assess the corrective action plan and implementation plan proposed by the organisation, and if the assessment concludes that they are sufficient to address the non-compliance, accept them.
  • (3) If the organisation fails to submit an acceptable corrective action plan, or fails to perform the corrective action within the time period accepted or extended by the competent authority, the finding shall be raised to level 1 and action shall be taken as laid down in point (d)(1).
  • (4) The competent authority shall record all the findings that it has raised or that have been communicated to it in accordance with point (e) and, where applicable, the enforcement measures it has applied, as well as all corrective actions and the dates of the action closures for all the findings.
  • (e) Without prejudice to any additional enforcement measures, when an authority performing the oversight tasks pursuant to point 145.B.300(d) identifies any non-compliance with the applicable requirements of Regulation (EU) 2018/1139 and its delegated and implementing acts by an organisation certified by the competent authority of another Member State or the Agency, it shall inform that competent authority and provide an indication of the level of the finding.
  • (f) The competent authority may issue observations for any of the following cases not requiring level 1 or level 2 findings:
  • (1) for any item whose performance has been assessed to be ineffective;
  • (2) when it has been identified that an item has the potential to cause a non-compliance under points (b) or (c);
  • (3) when suggestions or improvements are of interest for the overall safety performance of the organisation.

The observations issued under this point shall be communicated in writing to the organisation and recorded by the competent authority.

145.B.355   Suspension, limitation and revocation

The competent authority shall:

  • (a) suspend a certificate when it considers that there are reasonable grounds that such action is necessary to prevent a credible threat to aircraft safety;
  • (b) suspend, revoke or limit a certificate if such action is required pursuant to point 145.B.350;
  • (c) suspend or limit in whole or in part a certificate if unforeseeable circumstances outside the control of the competent authority prevent its inspectors from discharging their oversight responsibilities over the oversight planning cycle.

Appendix I

Authorised Release Certificate — EASA Form 1

The provisions of Appendix II to Annex I (Part-M) apply.

Appendix II

Class and rating system for the terms of approval of Part-145 maintenance organisations

  • (a) Except as stated otherwise for the smallest organisations referred to in point (m), the table referred to in point (l) provides the possible classes and ratings to be used to establish the terms of approval of the certificate of the organisation approved in accordance with Annex II (Part-145). An organisation must be granted terms of approval that range from a single class and rating with limitations to all classes and ratings with limitations.
  • (b) In addition to the table in point (l), each maintenance organisation is required to indicate its scope of work in its MOE.
  • (c) Within the approval class(es) and rating(s) established by the competent authority, the scope of work specified in the MOE defines the exact limits of its approval. It is therefore essential that the approval class(es) and rating(s) and the organisation’s scope of work match.
  • (d) A category A class rating means that the maintenance organisation may carry out maintenance on aircraft and components (including engines and/or auxiliary power units (APUs)), in accordance with the aircraft maintenance data or, if agreed by the competent authority, in accordance with the component maintenance data, only while such components are fitted to the aircraft. Nevertheless, such an A-rated maintenance organisation may temporarily remove a component for maintenance in order to improve access to that component, except when its removal generates the need for additional maintenance that the organisation is not approved to perform. Such removal of component for maintenance by A-rated maintenance organisation shall be subject to an appropriate control procedure in the MOE. The limitation column must specify the scope of such maintenance, thereby indicating the extent of the approval.
  • (e) Category A class ratings are subdivided into ‘Base’ or ‘Line’ maintenance categories. Such an organisation may be approved for either ‘Base’ or ‘Line’ maintenance, or both. It should be noted that a ‘Line’ facility located at a main base facility requires a ‘Line’ maintenance approval.
  • (f) A category B class rating means that the maintenance organisation may carry out maintenance on uninstalled engines and/or APUs and engine and/or APU components, in accordance with the engine and/or APU maintenance data or, if agreed by the competent authority, in accordance with the component maintenance data, only while such components are fitted to the engine and/or the APU. Nevertheless, such a B-rated approved maintenance organisation may temporarily remove a component for maintenance in order to improve access to that component, except when its removal generates the need for additional maintenance that the organisation is not approved to perform. The limitation column must specify the scope of such maintenance, thereby indicating the extent of the approval. A maintenance organisation that is approved with a category B class rating may also carry out maintenance on an installed engine during aircraft base and line maintenance, provided that an appropriate control procedure in the MOE has been approved by the competent authority. The scope of work in the MOE shall reflect those activities if they are permitted by the competent authority.
  • (g) A category C class rating means that the maintenance organisation may carry out maintenance on uninstalled components (excluding complete engines and APUs) that are intended to be fitted on the aircraft or the engine/APU. The limitation column must specify the scope of such maintenance, thereby indicating the extent of the approval. A maintenance organisation that is approved with a category C class rating may also carry out maintenance on an installed component (other than a complete engine/APU) during aircraft base and line maintenance, or at an engine/APU maintenance facility provided that an appropriate control procedure in the MOE has been approved by the competent authority. The scope of work in the MOE shall reflect those activities if they are permitted by the competent authority.
  • (h) A category D class rating is a self-contained class rating that is not necessarily related to a specific aircraft, engine or other component. The D1 – Non-Destructive Testing (NDT) rating is only necessary for a maintenance organisation that carries out NDT as a particular task for another organisation. A maintenance organisation that is approved with a class rating in the A, B or C category may carry out NDT on products that it maintains without the need for a D1 class rating provided that the MOE contains appropriate NDT procedures.
  • (i) The limitation column is intended to give competent authorities the flexibility to customise an approval for any particular organisation. Ratings may only be mentioned on the approval if they are appropriately limited. The table in point (l) specifies the types of limitations that are possible. It is acceptable to stress in the limitation column the maintenance task rather than the type or manufacturer of the aircraft or engine, if that is more appropriate to the organisation (an example could be avionics systems installations and the related maintenance). If that is mentioned in the limitation column, it indicates that the maintenance organisation is approved to carry out maintenance up to and including that particular type/task.
  • (j) When reference is made to the series, type and group in the limitation column of class A and B, it shall be understood as follows:
  • — ‘series’ means a specific type series such as the Airbus 300, 310 or 319, or the Boeing 737-300 series, the RB211-524 series, the Cessna 150 or Cessna 172, the Beech 55 series, the continental O-200 series, etc.,
  • — ‘type’ means a specific type or model such as the Airbus 310-240 type, the RB 211-524 B4 type, or the Cessna 172RG type. Any number of series or types may be quoted,
  • — ‘group’ means, for example, Cessna single piston engine aircraft or Lycoming non-supercharged piston engines, etc.
  • (k) By way of derogation from point 145.A.85(a)(1), when a component capability list is used that could be subject to frequent amendments, then the organisation may propose to include such amendments in the procedure referred to in point 145.A.85(c) for changes not requiring prior approval.
  • (l) Table CLASS RATING LIMITATION BASE LINE AIRCRAFT A1 Aeroplanes above 5 700 kg maximum take-off mass (MTOM) [Shall state the aeroplane manufacturer or the group or series or type and/or the maintenance tasks] Example: Airbus A320 Series [YES/NO] [^E0014] [YES/NO] [^E0014] A2 Aeroplanes of 5 700 kg MTOM and below [Shall state the aeroplane manufacturer or the group or series or type and/or the maintenance tasks] Example: DHC-6 Twin Otter Series State whether the issuing of airworthiness review certificates is authorised (only possible for aircraft covered by Annex Vb (Part-ML)) [YES/NO] [^E0014] [YES/NO] [^E0014] A3 Helicopters [Shall state the helicopter manufacturer or the group or series or type and/or the maintenance task(s)] Example: Robinson R44 State whether the issuing of airworthiness review certificates is authorised (only possible for aircraft covered by Annex Vb (Part-ML)) [YES/NO] [^E0014] [YES/NO] [^E0014] A4 Aircraft other than A1, A2 and A3 aircraft [Shall state the aircraft category (sailplane, balloon, airship, etc.) when applicable, the manufacturer or group or series or type and/or the maintenance task(s)] State whether the issuing of airworthiness review certificates is authorised (only possible for aircraft covered by Annex Vb (Part-ML)) [YES/NO] [^E0014] [YES/NO] [^E0014] ENGINES B1 Turbine [Shall state the engine series or type and/or the maintenance task(s)] Example: PT6A Series B2 Piston [Shall state the engine manufacturer or group or series or type and/or the maintenance task(s)] B3 APU [Shall state the engine manufacturer or series or type and/or the maintenance task(s)] B4 Engines other than B1, B2 and B3 [Shall state the engine manufacturer or group or series or type and/or the maintenance task(s)] COMPONENTS OTHER THAN COMPLETE ENGINES OR APUs C1 Air Cond & Press [Shall state the aircraft type or aircraft manufacturer or component manufacturer or the particular component and/or cross-refer to a capability list in the exposition and/or the maintenance task(s)] Example: PT6A Fuel Control C2 Auto Flight C3 Comms and Nav C4 Doors – Hatches C5 Electrical Power & Lights C6 Equipment C7 Engine – APU C8 Flight Controls C9 Fuel C10 Rotorcraft – Rotors C11 Rotorcraft – Trans C12 Hydraulic Power C13 Indicating – recording system C14 Landing Gear C15 Oxygen C16 Propellers C17 Pneumatic & Vacuum C18 Protection ice/rain/fire C19 Windows C20 Structural C21 Water ballast C22 Propulsion Augmentation C23 Other SPECIALISED SERVICES D1 Non-Destructive Testing [Shall state particular NDT method(s)] (1) – Delete as appropriate
  • (m) A maintenance organisation which employs only one person to both plan and carry out all its maintenance activities can only hold limited terms of approval. The maximum permissible limits are as follows: CLASS RATING LIMITATION AIRCRAFT A2 AEROPLANES of 5 700 KG MTOM OR LESS WITH PISTON ENGINE or ELECTRIC POWER PLANT WITH NO FUEL CELL AIRCRAFT A3 HELICOPTERS of 3 175 KG MTOM OR LESS WITH SINGLE-PISTON ENGINE or ELECTRIC POWER PLANT WITH NO FUEL CELL AIRCRAFT A4 SAILPLANES, BALLOONS, AIRSHIPS AND ANY AIRCRAFT of 3 175 KG MTOM OR LESS WITH SINGLE-PISTON ENGINE or ELECTRIC POWER PLANT WITH NO FUEL CELL ENGINES B2 LESS THAN 450 HP ENGINES B4 ELECTRIC ENGINE COMPONENTS OTHER THAN COMPLETE ENGINES OR APUs C1 TO C23 AS PER CAPABILITY LIST SPECIALISED SERVICES D1 NDT NDT METHOD(S) TO BE SPECIFIED

It should be noted that such an organisation may be further limited by the competent authority in the terms of approval depending on the capabilities of the particular organisation.

Appendix III

Maintenance Organisation Certificate — EASA Form 3-145

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[MEMBER STATE] (*)

A Member of the European Union (**)

MAINTENANCE ORGANISATION CERTIFICATE

Reference: [MEMBER STATE CODE (*)].145.XXXX

Pursuant to Regulation (EU) 2018/1139 of the European Parliament and of the Council and to Commission Regulation (EU) No 1321/2014 and subject to the condition specified below, the [COMPETENT AUTHORITY OF THE MEMBER STATE (*)] hereby certifies:

[COMPANY NAME AND ADDRESS]

as a maintenance organisation in compliance with Section A of Annex II (Part-145) of Regulation (EU) No 1321/2014, approved to maintain products, parts and appliances listed in the attached terms of approval and issue related certificates of release to service using the above references and, when stipulated, to issue airworthiness review certificates after an airworthiness review as specified in point ML.A.903 of Annex Vb (Part-ML) to Commission Regulation (EU) No 1321/2014 for those aircraft listed in the attached approval schedule.

CONDITIONS:

1.

This approval is limited to that specified in the scope of work section of the approved maintenance organisation exposition as referred to in Section A of Annex II (Part-145), and

2.

This approval requires compliance with the procedures specified in the approved maintenance organisation exposition, and

3.

This approval is valid whilst the approved maintenance organisation remains in compliance with Annex II (Part-145) of Regulation (EU) No 1321/2014.

4.

Subject to compliance with the foregoing conditions, this approval shall remain valid for an unlimited duration unless the approval has previously been surrendered, superseded, suspended or revoked.

Date of original issue:

Date of this revision:

Revision No:

Signed:

For the competent authority: [COMPETENT AUTHORITY OF THE MEMBER STATE(*)]

EASA Form 3-145 Issue 4

(*) Or EASA if EASA is the competent authority.

(**) Delete for non-EU Member States or EASA.

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MAINTENANCE ORGANISATION

TERMS OF APPROVAL

Reference: [MEMBER STATE CODE (*)].145.[XXXX]

Organisation: [COMPANY NAME AND ADDRESS]

These terms of approval are limited to those products, parts and appliances and to the activities specified in the scope of work section of the approved maintenance organisation exposition,

Maintenance Organisation Exposition reference:

Date of original issue:

Date of last revision approved: Revision No:

Signed:

For the competent authority: [COMPETENT AUTHORITY OF THE MEMBER STATE (*)]

EASA Form 3-145 Issue 4

(*) Or EASA if EASA is the competent authority.

(**) Delete as appropriate if the organisation is not approved.

(***) Complete with the appropriate rating and limitation.

() Complete with appropriate limitation and state whether the issue of airworthiness review certificates is authorised or not.

CLASS

RATING

LIMITATION

BASE

LINE

AIRCRAFT (**)

(***)

(***)

[YES/NO] (**)

[YES/NO] (**)

(***)

(***)

[YES/NO] (**)

[YES/NO] (**)

(***)

(***)

[YES/NO] (**)

[YES/NO] (**)

(***)

(***)

[YES/NO] (**)

[YES/NO] (**)

ENGINES (**)

(***)

(***)

(***)

(***)

COMPONENTS OTHER THAN COMPLETE ENGINES OR APUs (**)

(***)

(***)

(***)

(***)

(***)

(***)

(***)

(***)

(***)

(***)

(***)

(***)

SPECIALISED SERVICES (**)

(***)

(***)

(***)

(***)

Appendix IV

Conditions for the use of staff not qualified in accordance with Annex III (Part-66) referred to in points 145.A.30(j)1 and 2

    1. Certifying staff in compliance with all the following conditions are deemed to meet the intent of point 145.A.30(j)(1) and (2):
  • (a) The person shall hold a licence or a certifying staff authorisation issued under national regulations in full compliance with ICAO Annex 1.
  • (b) The scope of work of the person shall not exceed the scope of work defined by the national licence or the certifying staff authorisation, whatever is the most restrictive.
  • (c) The person shall demonstrate he/she received the training on human factors and aviation legislation referred to in modules 9 and 10 of Appendix I to Annex III (Part-66).
  • (d) The person shall demonstrate 5 years maintenance experience for line maintenance certifying staff and 8 years for base maintenance certifying staff. However, those persons whose authorised tasks do not exceed those of a Part-66 category A certifying staff, need to demonstrate 3 years maintenance experience only.
  • (e) Line maintenance certifying staff and base maintenance support staff shall demonstrate he/she received type training and passed examination at the category B1, B2 or B3 level, as applicable, referred to in Appendix III to Annex III (Part-66) for each aircraft type in the scope of work referred to in point (b). Those persons whose scope of work does not exceed those of a category A certifying staff may however receive task training in lieu of a complete type training.
  • (f) Base maintenance certifying staff shall demonstrate he/she received type training and passed examination at the category C level referred to in Appendix III to Annex III (Part-66) for each aircraft type in the scope of work referred to in point (b), except that for the first aircraft type, training and examination shall be at the category B1, B2 or B3 level of Appendix III.
    1. Protected rights
  • (a) The personnel having privileges before the entry into force of the relevant requirements of Annex III (Part-66) may continue to exercise them without the need to comply with points 1(c) to 1(f).
  • (b) However after that date any certifying staff willing to extend the scope of their authorisation to include additional privileges shall comply with point 1.
  • (c) Notwithstanding point 2(b) above, in the case of additional type training, compliance with points 1(c) and 1(d) is not required.

ANNEX III

(Part-66)

CONTENTS CONTENTS
66.1. Competent authority
SECTION A — TECHNICAL REQUIREMENTS
SUBPART A — AIRCRAFT MAINTENANCE LICENCE
66.A.1 Scope
66.A.3 Licence categories and subcategories
66.A.5 Aircraft groups
66.A.10 Application
66.A.15 Eligibility
66.A.20 Privileges
66.A.25 Basic knowledge requirements
66.A.30 Basic experience requirements
66.A.40 Continued validity of the aircraft maintenance licence
66.A.45 Endorsement with aircraft ratings
66.A.50 Limitations
66.A.55 Evidence of qualification
66.A.70 Conversion provisions
SECTION B — PROCEDURES FOR COMPETENT AUTHORITIES
SUBPART A — GENERAL
66.B.1 Scope
66.B.2 Means of compliance
66.B.10 Competent authority
66.B.15 Information security management system
66.B.20 Record-keeping
66.B.25 Mutual exchange of information
66.B.30 Exemptions
SUBPART B — ISSUE OF AN AIRCRAFT MAINTENANCE LICENCE
66.B.100 Procedure for the issue of an aircraft maintenance licence by the competent authority
66.B.105 Procedure for the issue of an aircraft maintenance licence via the Part-145 approved maintenance organisation
66.B.110 Procedure for the change of an aircraft maintenance licence to include an additional basic category or subcategory
66.B.115 Procedure for the change of an aircraft maintenance licence to include an aircraft rating or to remove limitations
66.B.120 Procedure for the renewal of an aircraft maintenance licence validity
66.B.125 Procedure for the conversion of licences including group ratings
66.B.130 Procedure for the direct approval of aircraft type training
66.B.135 Procedure for the approval of multimedia-based training (MBT) courses
SUBPART C — EXAMINATIONS
66.B.200 Examination by the competent authority
SUBPART D — CONVERSION OF CERTIFYING STAFF QUALIFICATIONS
66.B.300 General
66.B.305 Conversion report for national qualifications
66.B.310 Conversion report for approved maintenance organisations authorisations
SUBPART E — EXAMINATION CREDITS
66.B.400 General
66.B.405 Examination credit report
66.B.410 Examination credit validity
SUBPART F — CONTINUING OVERSIGHT
66.B.500 Revocation, suspension or limitation of the aircraft maintenance licence
APPENDICES
Appendix I — Basic knowledge requirements (except for category L licence)
Appendix II — Basic examination standard (except for category L licence)
Appendix III — Aircraft type training and type evaluation standard – on-the-job training (OJT)
Appendix IV — Experience and basic knowledge modules or part modules required for extending a Part-66 aircraft maintenance licence
Appendix V — Application Form — EASA Form 19
Appendix VI — Aircraft Maintenance Licence referred to in Annex III (Part-66) – EASA Form 26
Appendix VII — Basic knowledge requirements for category L aircraft maintenance licence
Appendix VIII — Basic examination standards for category L aircraft maintenance licence
Appendix IX — Assessment method for the multimedia-based training (MBT)

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 issuance of an aircraft maintenance licence; or
    1. 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:
    1. defining the list of aircraft types;
    1. defining what airframe/engine (or powerplant) combinations are included in each particular aircraft type rating;
    1. in respect of an aircraft that is not covered by any licence (sub)category in point 66.A.3, point (a), defining the applicable licence (sub)category(ies) that entitle(s) the holder of the licence to exercise the privileges of point 66.A.20 on that aircraft.

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 application, issue and continuation of its validity.

66.A.3   Licence categories and subcategories
  • (a) Aircraft maintenance licences include the following categories and, where applicable, subcategories and system ratings:
  • (1) Category A:
  • (i) Category A, is divided into the following subcategories:
  • — A1 Aeroplanes Turbine,
  • — A2 Aeroplanes Piston,
  • — A3 Helicopters Turbine,
  • — A4 Helicopters Piston.
  • (ii) Subcategories A1 and A3 may also be used for aircraft not covered by any A subcategory.
  • (2) Category B1, is divided into the following subcategories:
  • — B1.1 Aeroplanes Turbine,
  • — B1.2 Aeroplanes Piston,
  • — B1.E Aeroplanes with electric power plant and MTOM below 5 700 kg,
  • — B1.3 Helicopters Turbine,
  • — B1.4 Helicopters Piston.
  • (3) Category B2 The B2 licence is applicable to all aircraft.
  • (4) Category B2L The B2L licence is applicable to all aircraft other than those in Group 1 as set out in Point 66.A.5(1) and is divided into the following ‘system ratings’:
  • — communication/navigation (com/nav),
  • — instruments,
  • — autoflight,
  • — surveillance,
  • — airframe systems. A B2L licence shall contain, as a minimum, one system rating.
  • (5) Category B3 The B3 licence is applicable to piston-engine non-pressurised aeroplanes of 2 000 kg MTOM and below.
  • (6) Category L, divided into the following subcategories:
  • — L1C: composite sailplanes,
  • — L1: sailplanes,
  • — L2C: composite powered sailplanes and composite ELA1 aeroplanes,
  • — L2: powered sailplanes and ELA1 aeroplanes,
  • — L3H: hot-air balloons,
  • — L3G: gas balloons,
  • — L4H: hot-air airships,
  • — L4G: ELA2 gas airships,
  • — L5: gas airships other than ELA2.
  • (7) Category C The C licence is applicable to aeroplanes and helicopters.
  • (8) When an aircraft can be considered as included in more than one of the above (sub)categories, the Agency, based on the aircraft characteristics, shall establish the (sub)category(ies) of the licence applicable for the aircraft in its type certificate data sheet.
  • (b) Additionally, for aircraft and combinations of aircraft and power plant not referred to in point (a), the applicable licence (sub)category(ies) shall be the one(s) identified by the Agency. The Agency shall identify such licence (sub)category(ies) in the operational suitability data established in accordance with Regulation (EU) No 748/2012, taking into consideration a report from the applicant for, or holder of, the aircraft type certificate which assesses the architecture and systems of the aircraft (and power plant) against the syllabus of the basic knowledge modules and knowledge levels, as relevant to the designated licence (sub)category, and the privileges established in 66.A.20.
66.A.5   Aircraft groups

For the purpose of ratings on aircraft maintenance licences, aircraft shall be classified into the following groups:

  • (1) Group 1 is composed of:
  • (i) aeroplanes certified for a MTOM exceeding 5 700 kg; aeroplanes certified for a maximum passenger seating configuration of more than 19; aeroplanes certified for operation with a minimum crew of at least two pilots; aeroplanes equipped with (one) turbojet engine(s) or more than one turboprop engine; aeroplanes with maximum certified operating altitude exceeding FL290 powered with a power plant other than piston; aeroplanes with a power plant not being piston, turbine or electric;
  • (ii) helicopters certified for a MTOM exceeding 3 175 kg; helicopters certified for a maximum passenger seating configuration of more than nine; helicopters certified for operation with a minimum crew of at least two pilots; helicopters equipped with multiple engines; helicopters equipped with a power plant not being piston, turbine or electric;
  • (iii) gas airships other than ELA2;
  • (iv) non-conventional aircraft; and
  • (v) aircraft equipped with fly-by-wire systems. Notwithstanding the first paragraph, the Agency may decide to classify into a subgroup of Group 2, Group 3 or Group 4, as appropriate, an aircraft which meets the conditions set out in the first paragraph, if it considers that the lower complexity of the particular aircraft justifies so.
  • (2) Group 2: aircraft other than those in Group 1 belonging to the following subgroups:
  • (i) subgroup 2a: single turboprop engine aeroplanes;
  • (ii) subgroup 2b: single turbine engine helicopters;
  • (iii) subgroup 2c: single piston engine helicopters;
  • (iv) subgroup 2E: aeroplanes with electric power plant.
  • (3) Group 3: piston engine aeroplanes other than those in Group 1.
  • (4) Group 4: sailplanes, powered sailplanes, balloons and airships, other than those in Group 1.
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 appropriate, 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 procedure 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 procedure 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) or Annex Vd (Part-CAO) shall send the aircraft maintenance licence together with the EASA Form 19 to the competent authority 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.
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.
    1. 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 electrical systems,
  • — work on avionic systems requiring only simple tests to prove their serviceability and not requiring troubleshooting. Category B1 includes the corresponding A subcategory.
    1. 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 authorisation and limited to the ratings already endorsed in the B2 licence. The category B2 licence does not include any A subcategory.
    1. A category B2L aircraft maintenance licence shall permit the holder to issue certificates of release to service and to act as B2L support staff for the following:
  • — maintenance performed on electrical systems;
  • — maintenance performed on avionics systems within the limits of the system ratings specifically endorsed on the licence, and
  • — when holding the ‘airframe system’ rating, performance of electrical and avionics tasks within power plant and mechanical systems, requiring only simple tests to prove their serviceability.
    1. 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 the following:
  • — maintenance performed on aeroplane structure, power plant and mechanical and electrical systems; and
  • — work on avionics systems requiring only simple tests to prove their serviceability and not requiring troubleshooting.
    1. A category L aircraft maintenance licence shall permit the holder to issue certificates of release to service and to act as L support staff for the following:
  • — maintenance performed on aircraft structure, power plant and mechanical and electrical systems;
  • — work on radio, Emergency Locator Transmitters (ELT) and transponder systems; and
  • — work on other avionics systems requiring simple tests to prove their serviceability. Subcategory L2 includes subcategory L1. Any limitation to subcategory L2 in accordance with point 66.A.45(h) becomes also applicable to subcategory L1. Subcategory L2C includes subcategory L1C.
    1. A category C aircraft maintenance licence shall permit the holder to issue certificates of release to service following base maintenance of the aircraft. The privileges apply to the aircraft in its entirety. A Category C aircraft maintenance licence issued with respect to complex motor-powered aircraft shall include the privileges of category C aircraft maintenance licence also with respect to other than complex motor-powered aircraft.
    1. In addition, the privileges in point 1 to 7 are also extended to aircraft referred to in point (b) of point 66.A.3 for the corresponding licence (sub)category(ies) identified as applicable in the operational suitability data established in accordance with Regulation (EU) No 748/2012 of these aircraft.
  • (b) The holder of an aircraft maintenance licence may not exercise its privileges unless:
    1. in compliance with the applicable requirements of Annex I (Part-M), Annex II (Part-145), Annex Vb (Part-ML) and Annex Vd (Part-CAO); and
    1. in the preceding 2-year period he/she has, either had 6 months of maintenance experience in accordance with the privileges granted by the aircraft maintenance licence or, met the provision for the issue of the appropriate privileges; and
    1. he/she has the adequate competence to certify maintenance on the corresponding aircraft; and
    1. 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.
66.A.25   Basic knowledge requirements
  • (a) The applicant for an aircraft maintenance licence shall demonstrate by examination a level of knowledge of the related subject modules in accordance with Appendix I (applicable to category A, B1, B2, B2L, B3 and C licences) or Appendix VII (applicable to category L licences).
  • (b) The basic knowledge examinations shall comply with the standard set out in Appendix II (applicable to category A, B1, B2, B2L, B3 and C licences) or Appendix VIII (applicable to category L licences) to this Annex and shall be conducted by either of the following:
  • (1) a training organisation approved in accordance with Annex IV (Part-147);
  • (2) the competent authority;
  • (3) for category L licences, another organisation as agreed by the competent authority.
  • (c) The basic knowledge examinations shall have been passed within 10 years prior to the application for an aircraft maintenance licence or the addition of a category or subcategory to such a licence. If the basic knowledge examinations have not been passed within that 10-year period, credits for basic knowledge examinations may be alternatively obtained by the applicant in accordance with point (d). The 10 years’ validity requirement applies to each individual module examination, except for those module examinations which were already passed as part of another licence category and the licence has already been issued.
  • (d) The applicant may apply to the competent authority for full or partial credits for the basic knowledge requirements for:
  • (1) basic knowledge examinations which were passed more than 10 years before the application for an aircraft maintenance licence was submitted (see point (c));
  • (2) any other national technical training and examination considered by the competent authority as equivalent to the corresponding basic knowledge requirements of this Annex. The applicant shall provide evidence of the granted credits by referring to an examination credit report approved by the competent authority in accordance with Section B, Subpart E, of this Annex III (Part-66).
  • (e) A basic training course without Modules 1 and 2 of Appendix I to this Annex is considered a full basic training course approved in accordance with Annex IV (Part-147) only when knowledge of those Modules is subsequently demonstrated by the applicant by examination and is credited by the competent authority.
  • (f) The holder of an aircraft maintenance licence applying for the addition of a different category or subcategory shall complement by examination the level of knowledge that is appropriate to the related subject modules in accordance with Appendix I (for category A, B1, B2, B2L, B3 and C licences) or Appendix VII (for category L licences). Appendix IV details the modules of Appendix I (for category B1, B2, B2L, B3 and C licences) or Appendix VII (for category L licences) required for the addition of a new category or subcategory to an existing licence issued in accordance with this AnnexA.
66.A.30   Basic experience requirements
  • (a) An applicant for an aircraft maintenance licence shall have acquired:
    1. for category A, subcategories B1.2, B1.E and B1.4 and category B3:
  • (i) 3 years of practical maintenance experience on operating aircraft, if the applicant has no previous relevant technical training; or
  • (ii) 2 years of practical maintenance experience on operating aircraft and completion of training considered relevant by the competent authority as a skilled worker, in a technical trade; or
  • (iii) 1 year of practical maintenance experience on operating aircraft and completion of a basic training course approved in accordance with Annex IV (Part-147);
    1. for category B2 and subcategories B1.1 and B1.3:
  • (i) 5 years of practical maintenance experience on operating aircraft if the applicant has no previous relevant technical training; or
  • (ii) 3 years of practical maintenance experience on operating aircraft and completion of training considered relevant by the competent authority as a skilled worker, in a technical trade; or
  • (iii) 2 years of practical maintenance experience on operating aircraft and completion of a basic training course approved in accordance with Annex IV (Part-147);
  • 2a. for category B2L:
  • (i) 3 years of practical maintenance experience in operating aircraft, covering the corresponding system rating(s), if the applicant has no previous relevant technical training; or
  • (ii) 2 years of practical maintenance experience in operating aircraft, covering the corresponding system rating(s), and completion of training, considered relevant by the competent authority, as a skilled worker in a technical trade; or
  • (iii) 1 year of practical maintenance experience in operating aircraft, covering the corresponding system rating(s), and completion of a Part-147 approved basic training course. For the addition of (a) new system rating(s) to an existing B2L licence, 3 months of practical maintenance experience relevant to the new system rating(s) shall be required for each system rating added.
  • 2b. for category L:
  • (i) 2 years of practical maintenance experience in operating aircraft covering a representative cross section of maintenance activities in the corresponding subcategory;
  • (ii) as a derogation from point (i), 1 year of practical maintenance experience in operating aircraft covering a representative cross section of maintenance activities in the corresponding subcategory, subject to the introduction of the limitation provided for in point 66.A.45(h)(ii)(3). —————
    1. for category C with respect to complex motor-powered aircraft (CMPA):
  • (i) 3 years of experience in exercising category B1.1, B1.3 or B2 privileges as support staff, or both support staff and certifying staff, in accordance with point 145.A.35 of Annex II (Part-145), at a maintenance organisation working on CMPA, including 12 months of experience as base maintenance support staff; or
  • (ii) 5 years of experience in exercising category B1.2, B1.E, B1.4 or L5 privileges as support staff, or both support staff and certifying staff, in accordance with point 145.A.35 of Annex II (Part-145), at a maintenance organisation working on CMPA, including 12 months of experience as base maintenance support staff; or
  • (iii) for applicants holding an academic degree, 3 years of experience in working at an aircraft maintenance environment, on a representative selection of tasks that are directly associated with aircraft maintenance, including 6 months of participation in the performance of base maintenance tasks in operating CMPA;
  • (iv) to extend the endorsed category C with respect to other than CMPA to CMPA:
  • (a) 2 years of experience in exercising category B1.1, B1.2, B1.E, B1.3, B1.4, B2 or L5 privileges as support staff, or both support staff and certifying staff, in accordance with point 145.A.35 of Annex II (Part-145), at a maintenance organisation working on CMPA, including 6 months of experience as base maintenance support staff; or
  • (b) when holding a category C licence based on an academic degree, 2 years of experience in working at an aircraft maintenance environment on a representative selection of tasks that are directly associated with aircraft maintenance, including 3 months of participation in the performance of base maintenance tasks in operating CMPA;
    1. for category C with respect to other than CMPA:
  • (i) 3 years of experience in exercising category B1, B2, B2L, B3 or L privileges as support staff, or both support staff and certifying staff, in accordance with point 145.A.35 of Annex II (Part-145), at a maintenance organisation in operating other than CMPA, including 6 months of experience as base maintenance support staff; or
  • (ii) for holders of an academic degree, 3 years of experience in working at an aircraft maintenance environment, on a representative selection of tasks that are directly associated with aircraft maintenance, including 6 months of participation in the performance of base maintenance tasks in operating other than CMPA;
    1. the academic degree shall be in a relevant technical discipline, issued by a university or any other higher educational institution recognised by the competent authority.
  • (b) An applicant for an extension to an aircraft maintenance licence shall have a minimum civil aircraft maintenance experience requirement appropriate to the additional category or subcategory of licence applied for as defined in Appendix IV to this Annex (Part-66).
  • (c) The experience shall be practical and involve a representative cross section of maintenance tasks on aircraft.
  • (d) At least 1 year of the required experience shall be recent maintenance experience on aircraft of the category/subcategory for which the initial aircraft maintenance licence is sought. For subsequent category/subcategory additions to an existing aircraft maintenance licence, the additional recent maintenance experience required may be less than 1 year, but shall be at least 3 months. The required experience shall be dependent upon the difference between the licence category/subcategory held and applied for. Such additional experience shall be typical of the new licence category/subcategory sought.
  • (da) Notwithstanding points (a), (b) and (d), practical maintenance experience and recent maintenance experience gained in aircraft referred to in point (b) of point 66.A.3 shall account for a maximum of 50 % of the practical maintenance experience and recent maintenance experience required in points (a), (b) or (d) in respect of the licence (sub)category(ies) on which these aircraft can be endorsed.
  • (e) Notwithstanding point (a), experience in aircraft maintenance gained in organisations not approved in accordance with Annexes II (Part-145) or Vd (Part-CAO) may be recognised when such maintenance is equivalent to that required by this Annex as established by the competent authority. However, demonstration of additional experience in organisations approved in accordance with Annexes II or Vd or under the supervision of independent certifying staff, shall be required.
  • (f) Experience shall have been acquired within the 10 years preceding the application for an aircraft maintenance licence or the addition of a category or subcategory to such a licence.
66.A.40   Continued validity of the aircraft maintenance licence
  • (a) The aircraft maintenance licence becomes invalid 5 years after its last issue or change, unless the holder submits his/her aircraft maintenance licence to the competent authority that issued it, in order to verify that the information contained in the licence is the same as that contained in the competent authority records, pursuant to point 66.B.120.
  • (b) The holder of an aircraft maintenance licence shall complete the relevant parts of EASA Form 19 (see Appendix V) and submit it with the holder’s copy of the licence to the competent authority that issued the original aircraft maintenance licence, unless the holder works in a maintenance organisation approved in accordance with Annex II (Part-145) or Annex Vd (Part-CAO) that has a procedure in its exposition whereby such organisation may submit the necessary documentation on behalf of the aircraft maintenance licence holder.
  • (c) Any certification privilege based upon a aircraft maintenance licence becomes invalid as soon as the aircraft maintenance licence is invalid.
  • (d) The aircraft maintenance licence is only valid (i) when issued and/or changed by the competent authority and (ii) when the holder has signed the document.
66.A.45   Endorsement with aircraft ratings
  • (a) In order to be entitled to exercise certification privileges on a specific aircraft type, the holder of an aircraft maintenance licence needs to have their licence endorsed with the relevant aircraft ratings:
  • — For category B1, B2 or C, the relevant aircraft ratings are the following: (i) for Group 1 aircraft, the appropriate aircraft type rating; (ii) for Group 2 aircraft, the appropriate aircraft type rating, manufacturer subgroup rating or full subgroup rating; (iii) for Group 3 aircraft, the appropriate aircraft type rating or full group rating; (iv) for Group 4 aircraft, for the category B2 licence, the full group rating.
  • — For category B2L, the relevant aircraft ratings are the following: (i) for Group 2 aircraft, the appropriate manufacturer subgroup rating or full subgroup rating; (ii) for Group 3 aircraft, the full group rating; (iii) for Group 4 aircraft, the full group rating.
  • — For category B3, the relevant rating is ‘piston-engine non-pressurised aeroplanes of 2 000 kg MTOM and below’.
  • — For category L, the relevant aircraft ratings are the following: (i) for subcategory L1C, the rating ‘composite sailplanes’; (ii) for subcategory L1, the rating ‘sailplanes’; (iii) for subcategory L2C, the rating ‘composite powered sailplanes and composite ELA1 aeroplanes’; (iv) for subcategory L2, the rating ‘powered sailplanes and ELA1 aeroplanes’; (v) for subcategory L3H, the rating ‘hot-air balloons’; (vi) for subcategory L3G, the rating ‘gas balloons’; (vii) for subcategory L4H, the rating ‘hot-air airships’; (viii) for subcategory L4G, the rating ‘ELA2 gas airships’; (ix) for subcategory L5, the appropriate airship type rating.
  • — For category A, no rating is required, subject to compliance with the requirements of point 145.A.35 of Annex II (Part-145).
  • (b) The endorsement of aircraft type ratings requires the satisfactory completion of one of the following:
  • — the relevant category B1, B2 or C aircraft type training in accordance with Appendix III to Annex III (Part-66);
  • — in the case of gas airship type ratings on a B2 or L5 licence, a type training approved by the competent authority in accordance with point 66.B.130.
  • (c) For other than category C licences, in addition to the requirements of point (b), the endorsement of the first aircraft type rating within a given category/subcategory requires satisfactory completion of the corresponding on-the-job training. This on-the-job training shall comply with Appendix III to Annex III (Part-66), except in the case of gas airships, where it shall be directly approved by the competent authority. The on-the-job training on an aircraft referred to in point (b) of point 66.A.3 may only be considered for the purpose of endorsement of the licence as the first aircraft type rating within a given (sub)category, as described in the previous paragraph, when so established in the aircraft operational suitability data. Otherwise, an aircraft referred to in point (b) of point 66.A.3 may be endorsed as a first aircraft type rating within a given (sub)category after satisfactory completion of the corresponding on-the-job training, but in such case, additional on-the-job training will be required for the endorsement on the licence within that (sub)category of the first aircraft type rating belonging to the categories referred in point (a) of point 66.A.3.
  • (d) By derogation from points (b) and (c), for Group 2 and 3 aircraft, aircraft type ratings may also be endorsed on a licence after completing the following steps:
  • — satisfactory completion of the relevant category B1, B2 or C aircraft type evaluation in accordance with Appendix III to this Annex (Part-66);
  • — in the case of B1 and B2 category, demonstration of practical experience in the aircraft type. In that case, the practical experience shall include a representative cross section of maintenance activities relevant to the licence category. In the case of a category C rating, for a person qualified through the academic route as referred to in point (a)(5) of point 66.A.30, the first relevant aircraft type evaluation shall be at the category B1 or B2 level.

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