the continuing airworthiness of aircraft, including any component for installation thereto, which are:

compliance with the essential requirements set out in Regulation (EC) No 216/2008 for continuing airworthiness of aircraft registered in a third country and components for installation thereon for which their regulatory safety oversight has not been delegated to a Member State that are dry leased-in by a licence air carrier in accordance with Regulation (EC) No 1008/2008 of the European Parliament and the Council ( 1 ).

‘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;

‘certifying staff’ means personnel responsible for the release of an aircraft or a component after maintenance;

‘component’ means any engine, propeller, part or appliance;

‘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;

‘JAA’ means ‘Joint Aviation Authorities.’;

‘JAR’ means ‘Joint Aviation Requirements’;

‘commercial air transport (CAT) operation’ means an aircraft operation to transport passengers, cargo or mail for remuneration or other valuable consideration;

‘maintenance’ means any one or combination of the following activities: overhaul, repair, inspection, replacement, modification or defect rectification of an aircraft or component, with the exception of pre-flight inspection;

‘organisation’ means a natural person, a legal person or part of a legal person. Such an organisation may be established at more than one location whether or not within the territory of the Member States;

‘pre-flight inspection’ means the inspection carried out before flight to ensure that the aircraft is fit for the intended flight;

‘ELA1 aircraft’ means the following manned European light aircraft:

‘ELA2 aircraft’ means the following manned European Light Aircraft:

‘LSA aircraft’ means a light sport aeroplane which has all of the following characteristics:

‘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;

‘critical maintenance task’ means a maintenance task that involves the assembly or any disturbance of a system or any part on an aircraft, engine or propeller that, if an error occurred during its performance, could directly endanger the flight safety;

‘commercial specialised operations’ means those operations subject to the requirements of Part-ORO, Subpart-SPO set out in Annex III to Commission Regulation (EU) No 965/2012 ( 2 );

‘limited operations’ means the operations of other-than-complex motor-powered aircraft for:

For the purpose of this Regulation, ‘limited operations’ are not considered as CAT operations or commercial specialised operations;

‘introductory flight’ means ‘introductory flight’ as defined in Article 2(9) of Regulation (EU) No 965/2012;

‘competition flight’ means ‘competition flight’ as defined in Article 2(10) of Regulation (EU) No 965/2012;

‘flying display’ means ‘flying display’ as defined in Article 2(11) of Regulation (EU) No 965/2012;

‘management systems harmonisation’ means the coordinated process by which the management systems of two or more organisations interact and share information and methods to reach common or consistent safety and compliance monitoring objectives.

for the oversight of the continuing airworthiness of individual aircraft and the issue of airworthiness review certificates the authority designated by the Member State of registry;

for the oversight of a maintenance organisation as specified in Section A, Subpart F of this Annex (Part-M):

for the approval of aircraft maintenance programmes (‘AMP’), one of the following:

for the oversight of a continuing airworthiness management organisation as specified in Section A, Subpart G of this Annex (Part-M):

The owner of the aircraft shall be responsible for the continuing airworthiness of aircraft and shall ensure that no flight takes place unless all of the following requirements are met:

When the aircraft is leased, the responsibilities of the owner are transferred to the lessee if:

When reference is made in this Part to the ‘owner’, the term owner covers the owner or the lessee, as applicable.

Any person or organisation performing maintenance shall be responsible for the tasks performed.

The pilot-in-command or, in the case of aircraft used by air carriers licensed in accordance with Regulation (EC) No 1008/2008, the operator, shall be responsible for the satisfactory accomplishment of the pre-flight inspection. That inspection shall be carried out by the pilot or another qualified person and shall not need to be carried out by an approved maintenance organisation or by certifying staff.

In the case of aircraft used by air carriers licensed in accordance with Regulation (EC) No 1008/2008 ( 7 ) the operator shall be responsible for the continuing airworthiness of the aircraft it operates and shall:

By derogation to point (e)(2), at least two operators forming part of a single air carrier business grouping may use the same CAMO to assume the responsibility for the continuing airworthiness management of all the aircraft they operate, provided that all of the following requirements are met:

By derogation to point (e)(2), when the termination or revocation of an air operator certificate results in a situation where an air carrier licensed in accordance with Regulation (EC) No 1008/2008 and forming part of an air carrier business grouping is no longer in compliance with point M.A.201(ea), that licensed air carrier shall define and implement an action plan to the satisfaction of the competent authority to comply with point M.A.201(e)(2) as soon as practicable.

For complex motor-powered aircraft used for commercial specialised operations, for CAT operations other than those performed by air carriers licensed in accordance with Regulation (EC) No 1008/2008 or by commercial Approved Training Organisations (‘ATO’) and Declared Training Organisations (‘DTO’) referred to in Article 10a of Regulation (EU) No 1178/2011 ( 8 ), the operator shall ensure that:

For complex motor-powered aircraft not included in points (e) and (f), the owner shall ensure that:

For aircraft other than complex motor-powered aircraft used for commercial specialised operations or for CAT operations other than those performed by air carriers licensed in accordance with Regulation (EC) No 1008/2008, or by commercial ATOs and commercial DTOs referred to in Article 10a of Regulation (EU) No 1178/2011, the operator shall ensure that:

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▼M8

For aircraft other than complex motor-powered aircraft not included in points (e) and (h), or used for limited operations, the owner shall ensure that flight takes place only if the conditions set out in point (a) are met. To that end, the owner shall:

The owner/operator shall ensure that any person authorised by the competent authority is granted access to any of its facilities, aircraft or documents related to its activities, including any subcontracted activities, to determine compliance with this Part.

Where an aircraft included in an air operator certificate is used for non-commercial operations or specialised operations under point ORO.GEN.310 of Annex III or point NCO.GEN.104 of Annex VII to Regulation (EU) No 965/2012, the operator shall ensure that the tasks associated with continuing airworthiness are performed by the CAMO approved in accordance with Annex Vc (Part-CAMO) or Subpart G of this Annex (Part-M) or the combined airworthiness organisation (‘CAO’) approved in accordance with Annex Vd (Part-CAO), whichever applicable, of the air operator certificate holder.

Without prejudice to the reporting requirements set out in Annex II (Part-145) and Annex Vc (Part-CAMO), any person or organisation responsible in accordance with point M.A.201 shall report any identified condition of an aircraft or component which endangers flight safety to:

The reports referred to in point (a) shall be made in a manner determined by the competent authority referred to in point (a) and shall contain all pertinent information about the condition known to the person or organisation making the report.

Where the maintenance or the airworthiness review of the aircraft is carried out on the basis of a written contract, the person or the organisation responsible for those activities shall also report any condition referred to in point (a) to the owner and the operator of the aircraft and, when different, to the CAMO or CAO concerned.

The person or organisation shall submit the reports referred to in points (a) and (c) as soon as possible, but no later than 72 hours from the moment when the person or organisation identified the condition to which the report relates, unless exceptional circumstances prevent this.

The person or organisation shall submit a follow-up report, providing details of actions which that person or organisation intends to take to prevent similar occurrences in the future, as soon as those actions have been identified. The follow-up report shall be submitted in a form and manner established by the competent authority.

the accomplishment of pre-flight inspections;

the rectification of any defect and damage affecting safe operation in accordance with data specified in points M.A.304 and M.A.401, as applicable, while taking into account the minimum equipment list (‘MEL’) and configuration deviation list, when they exist;

the accomplishment of all maintenance in accordance with the AMP referred to in point M.A.302;

the release of all maintenance in accordance with Subpart H;

for all complex motor-powered aircraft or aircraft used by air carriers licensed in accordance with Regulation (EC) No 1008/2008, the analysis of the effectiveness of the approved AMP referred to in point M.A.302;

the accomplishment of any applicable:

the accomplishment of modifications and repairs in accordance with point M.A.304;

delivering to the pilot-in-command, or to the operator in the case of air carriers licensed in accordance with Regulation (EC) No 1008/2008, the mass and balance statement reflecting the current configuration of the aircraft;

maintenance check flights, when necessary.

Maintenance of each aircraft shall be organised in accordance with an AMP.

The AMP and any subsequent amendments thereto shall be approved by the competent authority.

►M8  When the continuing airworthiness of aircraft is managed by a CAMO or CAO, or when there is a limited contract between the owner and a CAMO or CAO concluded in accordance with point M.A.201(i)(3), the AMP and its amendments may be approved through an indirect approval procedure.

In that case, the indirect approval procedure shall be established by the CAMO or CAO concerned as part of the continuing airworthiness management exposition (‘CAME’) referred to in point CAMO.A.300 of Annex Vc or point M.A.704 of this Annex, or as part of the combined airworthiness exposition (‘CAE’) referred to in point CAO.A.025 of Annex Vd and shall be approved by the competent authority responsible for that CAMO or CAO. ◄

The indirect approval procedure shall only be used when the CAMO or CAO concerned is under the oversight of the Member State of registry of aircraft, unless a written contract has been concluded in accordance with point 3 of point M.1 transferring responsibility for the approval of the aircraft maintenance programme to the competent authority responsible for the CAMO or CAO.

The AMP shall demonstrate compliance with:

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▼C1

By derogation to point (d), the owner or the organisation managing the continuing airworthiness of the aircraft may deviate from the instruction referred to in point (d)(2) and propose escalated intervals in the AMP, based on data obtained from sufficient reviews carried out in accordance with point (h). Indirect approval is not permitted for the escalation of safety-related tasks. The owner or the organisation managing the continuing airworthiness of the aircraft may also propose additional instructions in the AMP.

The AMP shall contain details of all maintenance to be carried out, including frequency and any specific tasks linked to the type and specificity of operations.

For complex motor-powered aircraft, when the AMP is based on maintenance steering group logic or on condition monitoring, the AMP shall include a reliability programme.

The AMP shall be subject to periodic reviews and be amended accordingly when necessary. Those reviews shall ensure that the AMP continues to be up to date and valid in light of the operating experience and instructions from the competent authority, while taking into account new or modified maintenance instructions issued by the type certificate and supplemental type certificate holders and any other organisation that publishes such data in accordance with Annex I (Part-21) to Regulation (EU) No 748/2012.

approved by the Agency;

approved by a design organisation complying with Annex I (Part-21) to Regulation (EU) No 748/2012;

contained in the requirements referred to in point 21.A.90B or 21.A.431B of Annex I (Part-21) to Regulation (EU) No 748/2012.

At the completion of any maintenance, aircraft certificate of release to service (‘CRS’) required by point M.A.801 or point 145.A.50, as applicable, shall be entered in the aircraft continuing airworthiness record system, as soon as practicable and no later than 30 days after the completion of any maintenance.

The aircraft continuing airworthiness record system shall contain the following:

The aircraft continuing airworthiness records shall include the current mass and balance report and the current status of:

The aircraft continuing airworthiness records shall include the current status specific to components of:

The owner or operator shall establish a system to keep the following documents and data in a form acceptable to the competent authority and for the periods specified below:

The person or organisation responsible for the management of continuing airworthiness tasks pursuant to point M.A.201 shall comply with the requirements regarding the aircraft continuing airworthiness record system and present the records to the competent authority upon request.

All entries made in the aircraft continuing airworthiness record system shall be clear and accurate. When it is necessary to correct an entry, the correction shall be made in a manner that clearly shows the original entry.

In addition to the requirements of point M.A.305, for CAT, commercial specialised operations and commercial ATO or commercial DTO operations, the operator shall use a technical log system containing the following information for each aircraft:

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The initial issue of aircraft technical log system shall be approved by the competent authority specified in point CAMO.A.105 of Annex Vc (Part-CAMO), or point M.1 of this Annex (Part-M) or point CAO.1(1) of Annex Vd (Part-CAO), as applicable. Any subsequent amendment to that system shall be managed in accordance with point CAMO.A.300(c), or points M.A.704(b) and (c), or point CAO.A.025(c).

When an aircraft is permanently transferred from one owner or operator to another, the transferring owner or operator shall ensure that the continuing airworthiness records referred to in point M.A.305 and, if applicable the technical log system referred to in point M.A.306, are also transferred.

When the owner contracts the continuing airworthiness management tasks to a CAMO or CAO, the owner shall ensure that the continuing airworthiness records referred to in point M.A.305 are transferred to that contracted organisation.

The time periods for the retention of records set out in point (e) of point M.A.305 shall continue to apply to the new owner, operator, CAMO or CAO.

The person or organisation maintaining an aircraft shall have access to and use only applicable current maintenance data in the performance of maintenance including modifications and repairs.

For the purposes of this Annex, applicable maintenance data is any of the following:

The person or organisation maintaining an aircraft shall ensure that all applicable maintenance data is current and readily available for use when required. The person or organisation shall establish a work card or worksheet system to be used and shall either transcribe accurately the maintenance data onto such work cards or worksheets or make precise reference to the particular maintenance task or tasks contained in such maintenance data.

be qualified for the tasks performed, as required by this part;

ensure that the area in which maintenance is carried out is well organised and clean in respect of dirt and contamination;

use the methods, techniques, standards and instructions specified in the M.A.401 maintenance data;

use the tools, equipment and material specified in the M.A.401 maintenance data. If necessary, tools and equipment shall be controlled and calibrated to an officially recognised standard;

ensure that maintenance is performed within any environmental limitations specified in the M.A.401 maintenance data;

ensure that proper facilities are used in case of inclement weather or lengthy maintenance;

ensure that the risk of multiple errors during maintenance and the risk of errors being repeated in identical maintenance tasks are minimised;

ensure that an error capturing method is implemented after the performance of any critical maintenance task; and

carry out a general verification after completion of maintenance to ensure the aircraft or component is clear of all tools, equipment and any extraneous parts or material, and that all access panels removed have been refitted.

Any aircraft defect that hazards seriously the flight safety shall be rectified before further flight.

Only the certifying staff referred to in point M.A.801(b)(1) or in Subpart F of this Annex or in Annex II (Part-145) or in Annex Vd (Part-CAO), or the person authorised in accordance with point M.A.801(c) of this Annex can decide, using maintenance data referred to in point M.A.401 of this Annex, whether an aircraft defect hazards seriously the flight safety and therefore decide when and which rectification action shall be taken before further flight and which defect rectification can be deferred. However, this does not apply when the MEL is used by the pilot or by the certifying staff.

Any aircraft defect that would not hazard seriously the flight safety shall be rectified as soon as practicable, after the date the aircraft defect was first identified and within any limits specified in the maintenance data or the MEL.

Any defect not rectified before flight shall be recorded in the aircraft continuing airworthiness record system referred to in point M.A.305 or, if applicable in the aircraft technical log system referred to in point M.A.306.

All components shall be classified into the following categories:

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▼M5

Components, standard parts and material shall only be installed on an aircraft or a component when they are in a satisfactory condition, belong to one of the categories listed in point (a) and the applicable maintenance data specifies the particular component, standard part or material.

The maintenance of components other than the components referred to in points (b)(2) to (b)(6) of point 21.A.307 of Annex I (Part 21) to Regulation (EU) No 748/2012 shall be performed by maintenance organisations approved in accordance with Subpart F of this Annex or with Annex II (Part-145) or with Annex Vd (Part-CAO), as applicable.

By way of derogation from point (a), where a component is fitted to the aircraft, the maintenance of such a component may be performed by an aircraft maintenance organisation approved in accordance with Subpart F of this Annex or with Annex II (Part-145) or with Annex Vd (Part-CAO) or by the certifying staff referred to in point (b)(1) of point M.A.801. Such maintenance shall be performed in accordance with the aircraft maintenance data or in accordance with the component maintenance data if agreed by the competent authority. Such aircraft maintenance organisation or the certifying staff may temporarily remove the component for maintenance if this is necessary to improve access to the component, except where additional maintenance is required due to the removal. Component maintenance performed in accordance with this point shall not be eligible for the issuance of an EASA Form 1 and shall be subject to the aircraft release requirements provided for in point M.A.801.

By way of derogation from point (a), where a component is fitted to the engine or the auxiliary power unit (APU), the maintenance of such component may be performed by an engine maintenance organisation approved in accordance with Subpart F of this Annex, or with Annex II (Part-145), or with Annex Vd (Part-CAO). Such maintenance shall be performed in accordance with the engine or the APU maintenance data or in accordance with the component maintenance data if agreed by the competent authority. Such B-rated organisation may temporarily remove the component for maintenance if this is necessary to improve access to the component, except where additional maintenance is required due to the removal.

The maintenance of components referred to in point (b)(2) of point 21.A.307 of Annex I (Part 21) to Regulation (EU) No 748/2012, where the component is fitted to the aircraft or is temporarily removed to improve access, shall be performed by an aircraft maintenance organisation approved in accordance with Subpart F of this Annex or with Annex II (Part-145) or with Annex Vd (Part-CAO), as applicable, by the certifying staff referred to in point (b)(1) of point M.A.801 or by the pilot-owner referred to in point (b)(2) of point M.A.801. Component maintenance performed in accordance with this point shall not be eligible for the issuance of an EASA Form 1 and shall be subject to the aircraft release requirements provided for in point M.A.801.

The maintenance of components referred to in points (b)(3) to (b)(6) of point 21.A.307 of Annex I (Part 21) to Regulation (EU) No 748/2012 shall be performed by the organisation referred to in point (a), or performed by any person or organisation and released with a ‘declaration of maintenance accomplished’ issued by the person or organisation that performed the maintenance. The ‘declaration of maintenance accomplished’ shall contain at least basic details of the maintenance carried out, the date on which the maintenance was completed, and the identification of the organisation or person that issues it. It shall be considered a maintenance record and equivalent to an EASA Form 1 in respect of the maintained component.

Installed life-limited parts and time-controlled components shall not exceed the approved limitation as specified in the AMP and ADs, except as provided for in point M.A.504(b).

When the approved limitation expires, the component shall be removed from the aircraft for maintenance, or for disposal in the case of life-limited parts.

Unserviceable and unsalvageable components shall be segregated from serviceable components, standards parts and materials.

Unsalvageable components shall not be permitted to re-enter the component supply system unless the mandatory life limitation has been extended or a repair solution has been approved in accordance with Regulation (EU) No 748/2012.

An organisation involved in activities subject to this Subpart shall not exercise its activities unless approved by the competent authority. To that aim, the competent authority shall use the template set out in Appendix V.

The scope of work subject to approval shall be specified in the maintenance organisation manual in accordance with point M.A.604. Classes and ratings to be used for the approval of maintenance organisations are set out in Appendix IV of this Part.

An approved maintenance organisation may fabricate, in conformity with maintenance data, a restricted range of parts for the use in the course of undergoing work within its own facilities, as identified in the maintenance organisation manual.

The maintenance organisation shall provide a manual containing at least the following information:

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▼B

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▼B

The maintenance organisation manual and its amendments shall be approved by the competent authority.

Notwithstanding point (b) minor amendments to the manual may be approved through a procedure (hereinafter called indirect approval).

Facilities are provided for all planned work, specialised workshops and bays are segregated as appropriate, to ensure protection from contamination and the environment.

Office accommodation is provided for the management of all planned work including in particular, the completion of maintenance records.

Secure storage facilities are provided for components, equipment, tools and material. Storage conditions shall ensure segregation of unserviceable components and material from all other components, material, equipment and tools. Storage conditions shall be in accordance with the manufacturers' instructions and access shall be restricted to authorised personnel.

The organisation shall appoint an accountable manager, who has corporate authority for ensuring that all maintenance required by the customer can be financed and carried out to the standard required by this Part.

A person or group of persons shall be nominated with the responsibility of ensuring that the organisation is always in compliance with this Subpart. Such person(s) shall be ultimately responsible to the accountable manager.

All point (b) persons shall be able to show relevant knowledge, background and appropriate experience related to aircraft and/or component maintenance.

The organisation shall have appropriate staff for the normal expected contracted work. The use of temporarily sub-contracted staff is permitted in the case of higher than normally expected contracted work and only for personnel not issuing a certificate of release to service.

The qualification of all personnel involved in maintenance and airworthiness reviews shall be demonstrated and recorded.

Personnel who carry out specialised tasks such as welding, non-destructive testing/inspection other than colour contrast shall be qualified in accordance with an officially recognised standard.

The maintenance organisation shall have sufficient certifying staff to issue certificates of release to service for aircraft and components provided for in points M.A.612 and M.A.613. The staff shall comply with the following requirements:

By derogation from point (g), the organisation may use certifying staff qualified in accordance with the following provisions when providing maintenance support to operators involved in commercial operations, subject to appropriate procedures to be approved as part of the organisation's manual:

If the organisation performs airworthiness reviews and issues the corresponding airworthiness review certificate for ELA1 aircraft not involved in commercial operations in accordance with point ML.A.903 of Annex Vb (Part-ML), it shall have airworthiness review staff qualified and authorised meeting all of the following requirements:

In addition to point M.A.606(g), certifying staff can only exercise their privileges, if the organisation has ensured:

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▼B

In the following unforeseen cases, where an aircraft is grounded at a location other than the main base where no appropriate certifying staff is available, the maintenance organisation contracted to provide maintenance support may issue a one-off certification authorisation:

►M1  All such cases must be reported to the competent authority within seven days after issuing such certification authorisation. ◄ The approved maintenance organisation issuing the one-off certification authorisation shall ensure that any such maintenance that could affect flight safety is re-checked.

The approved maintenance organisation shall record all details concerning certifying staff and airworthiness review staff and maintain a current list of all certifying staff and airworthiness review staff together with their scope of approval as part of the organisation's manual pursuant to point M.A.604(a)5.

The organisation shall:

Tools and equipment shall be controlled and calibrated to an officially recognised standard. Records of such calibrations and the standard used shall be kept by the organisation.

The organisation shall inspect, classify and appropriately segregate all incoming components, standard parts and materials.

Upon completion of all required component maintenance in accordance with this Subpart, a component CRS shall be issued in accordance with point M.A.802 of this Annex or with point ML.A.802 of Annex Vb (Part-ML), as applicable. An EASA Form 1 shall be issued, except for those components maintained in accordance with points (b) or (d) of point M.A.502, for components fabricated in accordance with point (c) of point M.A.603 of this Annex and for components in respect of which point ML.A.502 of Annex Vb (Part-ML) provides otherwise.

The component CRS document, EASA Form 1, may be generated from a computer system.

The approved maintenance organisation shall record all details of work carried out. Records necessary to prove all requirements have been met for the issue of the certificate of release to service including the subcontractor's release documents and for the issue of any airworthiness review certificate shall be retained.

The approved maintenance organisation shall provide a copy of each CRS to the aircraft owner or operator, together with a copy of any detailed maintenance records associated with the work carried out and necessary to demonstrate compliance with point M.A.305 of this Annex (Part-M) or ML.A.305 of Annex Vb (Part-ML), as applicable.

The approved maintenance organisation shall retain a copy of all maintenance records and any associated maintenance data for three years from the date the aircraft or aircraft component to which the work relates was released from the approved maintenance organisation. ►M8  In addition, it shall retain a copy of all the records related to the issue of airworthiness review certificates for three years from the date of issue and shall provide a copy of them to the owner of the aircraft. ◄

maintain any aircraft and/or component for which it is approved at the locations specified in the approval certificate and the maintenance organisation manual;

arrange for the performance of specialised services under the control of the maintenance organisation at another organisation appropriately qualified, as described in the maintenance organisation manual;

maintain any aircraft or component for which it is approved at any location, where the need of such maintenance arises either from the unserviceability of the aircraft or from the necessity of supporting occasional maintenance and subject to compliance with the conditions specified in the maintenance organisation manual;

issue certificates of release to service, upon completion of maintenance, in accordance with point M.A.612 or M.A.613 of this Annex;

if specifically approved to do so for ELA1 aircraft not involved in commercial operations, perform airworthiness reviews and issue the corresponding airworthiness review certificate in accordance with the conditions specified in point ML.A.903 of Annex Vb (Part-ML).

the name of the organisation;

the location of the organisation;

additional locations of the organisation;

the accountable manager;

any of the persons specified in point M.A.606(b);

the facilities, equipment, tools, material, procedures, work scope, certifying staff and airworthiness review staff that could affect the approval.

An approval shall remain valid until 24 March 2022, subject to:

▼B

Upon surrender or revocation, the approval certificate shall be returned to the competent authority.

A level 1 finding is any finding of significant non-compliance with the requirements of this Annex and Annex Vb (Part-ML) which lowers the safety standard and seriously endangers flight safety.

A level 2 finding is any finding of non-compliance with the requirements of this Annex and Annex Vb (Part-ML) which may lower the safety standard and may endanger flight safety.

After receipt of notification of findings according to point M.B.605, the holder of the maintenance organisation approval shall define a corrective action plan and demonstrate corrective action to the satisfaction of the competent authority within a period agreed with this authority.

The approval is indicated on a certificate included in Appendix VI issued by the competent authority.

Notwithstanding point (a), for licenced air carriers in accordance with Regulation (EC) No 1008/2008, the approval shall be part of the air operator certificate issued by the competent authority, for the aircraft operated.

The scope of work deemed to constitute the approval shall be specified in the continuing airworthiness management exposition in accordance with point M.A.704.

The continuing airworthiness management organisation shall provide a continuing airworthiness management exposition containing the following information:

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▼B

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▼B

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▼B

The continuing airworthiness management exposition and its amendments shall be approved by the competent authority.

Notwithstanding point (b), minor amendments to the exposition may be approved indirectly through an indirect approval procedure. The indirect approval procedure shall define the minor amendment eligible, be established by the continuing airworthiness management organisation as part of the exposition and be approved by the competent authority responsible for that continuing airworthiness management organisation.

The organisation shall appoint an accountable manager, who has corporate authority for ensuring that all continuing airworthiness management activities can be financed and carried out in accordance with this Annex (Part-M) and Annex Vb (Part-ML), as applicable.

For licenced air carriers in accordance with Regulation (EC) No 1008/2008 the accountable manager referred to in point (a) shall be the person who also has corporate authority for ensuring that all the operations of the operator can be financed and carried out to the standard required for the issue of an air operator's certificate.

A person or group of persons shall be nominated with the responsibility of ensuring that the organisation always complies with the applicable continuing airworthiness management, airworthiness review and permit to fly requirements of this Annex (Part-M) and Annex Vb (Part-ML). Such person(s) shall be ultimately responsible to the accountable manager.

For licenced air carriers in accordance with Regulation (EC) No 1008/2008, the accountable manager shall designate a nominated post holder. This person shall be responsible for the management and supervision of continuing airworthiness activities, pursuant to point (c).

The nominated post holder referred to in point (d) shall not be employed by a Part-145 approved organisation under contract to the operator, unless specifically agreed by the competent authority.

The organisation shall have sufficient appropriately qualified staff for the expected work.

All point (c) and (d) persons shall be able to show relevant knowledge, background and appropriate experience related to aircraft continuing airworthiness.

The qualification of all personnel involved in continuing airworthiness management shall be recorded.

For organisations extending airworthiness review certificates in accordance with points M.A.711(a)(4) and M.A.901 of this Annex (Part-M) or point ML.A.901(c) of Annex Vb (Part-ML) as applicable, the organisation shall nominate persons authorised to do so, subject to approval by the competent authority.

The organisation shall define and keep updated in the continuing airworthiness management exposition the title(s) and name(s) of person(s) referred to in points M.A.706(a), M.A.706(c), M.A.706(d) and M.A.706(i).

For complex motor-powered aircraft and for aircraft used by licenced air carriers in accordance with Regulation (EC) No 1008/2008, the organisation shall establish and control the competence of personnel involved in the continuing airworthiness management, airworthiness review and/or quality audits in accordance with a procedure and to a standard agreed by the competent authority.

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To be approved to carry out airworthiness reviews and, if applicable, to issue permits to fly, an approved continuing airworthiness management organisation shall have appropriate airworthiness review staff to issue airworthiness review certificates or recommendations referred to in Section A, Subpart I of Annex I (Part-M) or in Section A, Subpart I of Annex Vb (Part-ML) and, if applicable, to issue a permit to fly in accordance with point M.A.711(c):

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Airworthiness review staff nominated by the approved continuing airworthiness organisation can only be issued an authorisation by the approved continuing airworthiness organisation when formally accepted by the competent authority after satisfactory completion of an airworthiness review under the supervision of the competent authority or under the supervision of the organisation's airworthiness review staff in accordance with a procedure approved by the competent authority.

The organisation shall ensure that aircraft airworthiness review staff can demonstrate appropriate recent continuing airworthiness management experience.

Airworthiness review staff shall be identified by listing each person in the continuing airworthiness management exposition together with their airworthiness review authorisation reference.

The organisation shall maintain a record of all airworthiness review staff, which shall include details of any appropriate qualification held together with a summary of relevant continuing airworthiness management experience and training and a copy of the authorisation. This record shall be retained until two years after the airworthiness review staff have left the organisation.

The organisation shall ensure that all continuing airworthiness management is carried out in accordance with Section A, Subpart C of this Annex (Part-M), and Section A, Subpart C of Annex Vb (Part-ML), as applicable.

For every aircraft managed, the approved continuing airworthiness management organisation shall:

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▼B

▼M8

▼B

In the case of complex motor-powered aircraft or aircraft used for CAT, or aircraft used for commercial specialised operations or commercial ATO or commercial DTO operations, when the CAMO is not appropriately approved in accordance with Annex II (Part-145) or Subpart F of this Annex (Part-M) or Annex Vd (Part-CAO), the organisation shall, in consultation with the operator, establish a written maintenance contract with an organisation approved in accordance with Annex II (Part-145) or Subpart F of this Annex (Part-M) or Annex Vd (Part-CAO) or with another operator, detailing the functions specified under points M.A.301(b), M.A.301(c), M.A.301(f) and M.A.301(g) of this Annex (Part-M), or points ML.A.301(b) to (e) of Annex Vb (Part-ML), ensuring that all maintenance is ultimately carried out by a maintenance organisation approved in accordance with Annex II (Part-145) or Subpart F of this Annex (Part-M) or Annex Vd (Part-CAO) and defining the support of the quality functions referred to in point M.A.712(b) of this Annex (Part-M).

Notwithstanding point (c), the contract may be in the form of individual work orders addressed to the maintenance organisation approved in accordance with Annex II (Part-145) or Subpart F of this Annex (Part-M) or Annex Vd (Part-CAO) in the case of:

The approved continuing airworthiness management organisation shall hold and use applicable current maintenance data in accordance with point M.A.401 of this Annex (Part-M) or point ML.A.401 of Annex Vb (Part-ML), as applicable, for the performance of continuing airworthiness tasks referred to in point M.A.708 of this Annex (Part-M). That data may be provided by the owner or the operator, subject to an appropriate contract being established with such an owner or operator. In such case, the continuing airworthiness management organisation only needs to keep such data for the duration of the contract, except when required by point M.A.714 of this Annex (Part-M).

For aircraft not used by licenced air carriers in accordance with Regulation (EC) No 1008/2008, the approved continuing airworthiness management organisation may develop ‘baseline’ or ‘generic’ maintenance programmes, or both, in order to allow for the initial approval or the extension of the scope of an approval, without having the contracts referred to in Appendix I to this Annex (Part M) or Appendix I to Annex Vb (Part-ML), as applicable. Those ‘baseline’ and ‘generic’ maintenance programmes however do not preclude the need to establish an adequate Aircraft Maintenance Programme in compliance with point M.A.302 of this Annex (Part-M) or ML.A.302 of Annex Vb (Part-ML), as applicable, in due time before exercising the privileges referred to in point M.A.711 of this Annex (Part-M).

A continuing airworthiness management organisation approved in accordance with Section A, Subpart G of this Annex (Part-M) may:

▼M2

▼B

▼M8

▼M8

▼B

An approved continuing airworthiness management organisation registered in one of the Member States may, additionally, be approved to carry out airworthiness reviews referred to in point M.A.710 and:

▼M8

▼B

A continuing airworthiness management organisation whose approval includes the privileges referred to in point M.A.711(b) may additionally be approved to issue a permit to fly in accordance with point 21.A.711(d) of Annex I (Part-21) to Regulation (EU) No 748/2012 for the particular aircraft for which the organisation is approved to issue the airworthiness review certificate, when the continuing airworthiness management organisation is attesting conformity with approved flight conditions, subject to an adequate approved procedure in the exposition referred to in point M.A.704.

To ensure that the approved continuing airworthiness management organisation continues to meet the requirements of this Subpart, it shall establish a quality system and designate a quality manager to monitor compliance with, and the adequacy of, procedures required to ensure airworthy aircraft. Compliance monitoring shall include a feedback system to the accountable manager to ensure corrective action as necessary.

The quality system shall monitor activities carried out under Section A, Subpart G of this Annex (Part M). It shall at least include the following functions:

The records of these activities shall be stored for at least two years.

Where the approved continuing airworthiness management organisation is approved in accordance with another Part, the quality system may be combined with that required by the other Part.

For licenced air carriers in accordance with Regulation (EC) No 1008/2008 the M.A. Subpart G quality system shall be an integrated part of the operator's quality system.

In the case of a small organisation not managing the continuing airworthiness of aircraft used by licenced air carriers in accordance with Regulation (EC) No 1008/2008, the quality system may be replaced by regular organisational reviews subject to the approval of the competent authority, except when the organisation issues airworthiness review certificates for aircraft above 2 730 kg MTOM other than balloons. In the case where there is no quality system, the organisation shall not contract continuing airworthiness management tasks to other parties.

the name of the organisation.

the location of the organisation.

additional locations of the organisation.

the accountable manager.

any of the persons specified in M.A.706(c).

the facilities, procedures, work scope and staff that could affect the approval.

The continuing airworthiness management organisation shall record all details of work carried out. The records required under point M.A.305 of this Annex (Part-M) or ML.A.305 of Annex Vb (Part-ML), as applicable, and if applicable point M.A.306 of this Annex (Part-M), shall be retained.

If the continuing airworthiness management organisation has the privilege referred to in point M.A.711(b), it shall retain a copy of each airworthiness review certificate and recommendation issued or, as applicable, extended, together with all supporting documents. In addition, the organisation shall retain a copy of any airworthiness review certificate that it has extended under the privilege referred to in point M.A.711(a)4.

If the continuing airworthiness management organisation has the privilege referred to in point M.A.711(c), it shall retain a copy of each permit to fly issued in accordance with the provisions of point 21A.729 of Annex I (Part-21) to Regulation (EU) No 748/2012.

The continuing airworthiness management organisation shall retain a copy of all records referred to in points (b) and (c) until two years after the aircraft has been permanently withdrawn from service.

The records shall be stored in a manner that ensures protection from damage, alteration and theft.

All computer hardware used to ensure backup shall be stored in a different location from that containing the working data in an environment that ensures they remain in good condition.

Where continuing airworthiness management of an aircraft is transferred to another organisation or person, all retained records shall be transferred to the said organisation or person. The time periods prescribed for the retention of records shall continue to apply to the said organisation or person.

Where a continuing airworthiness management organisation terminates its operation, all retained records shall be transferred to the owner of the aircraft.

▼M11

An approval shall remain valid until 24 March 2022, subject to:

▼B

Upon surrender or revocation, the approval certificate shall be returned to the competent authority.

A level 1 finding is any significant non-compliance with the requirements of this Annex (Part-M) or Annex Vb (Part-ML), as applicable, which lowers the safety standard and hazards seriously the flight safety;

A level 2 finding is any non-compliance with the requirements of this Annex (Part-M) or Annex Vb (Part-ML), as applicable, which could lower the safety standard and possibly hazard the flight safety;

After receipt of notification of findings according to point M.B.705, the holder of the continuing airworthiness management organisation approval shall define a corrective action plan and demonstrate corrective action to the satisfaction of the competent authority within a period agreed with this authority.

Except for aircraft released to service by a maintenance organisation approved in accordance with Annex II (Part-145), the CRS shall be issued in accordance with this Subpart.

No aircraft shall be released to service unless a CRS is issued when all maintenance tasks ordered have been properly carried out. The CRS shall be issued by an authorised certifying staff of the maintenance organisation approved in accordance with Subpart F of this Annex or with Annex Vd (Part-CAO), except for maintenance tasks other than complex maintenance tasks listed in Appendix VII to this Annex where the CRS is issued, alternatively by:

By derogation from point (b), in case of unforeseen situations, when an aircraft is grounded at a location where no maintenance organisation approved in accordance with this Annex, Annex II (Part-145) or Annex Vd (Part-CAO) and no independent certifying staff are available, the owner may authorise any person, with no less than 3 years of appropriate maintenance experience and holding either a valid ICAO Annex 1 compliant maintenance license for the aircraft type requiring certification or a certifying staff authorisation valid for the work requiring certification issued by an ICAO Annex 6 approved maintenance organisation to maintain the aircraft in accordance with the standards set out in Subpart D of this Annex and release it to service. In that case, the owner shall:

In case of a release to service in accordance with point (b)(1), the certifying staff may be assisted in performing the maintenance tasks by one or more persons subject to his or her direct and continuous control.

A CRS shall contain at least:

By derogation from point (b) and notwithstanding point (g), when the required maintenance cannot be completed, a CRS may be issued with the approved aircraft limitations. In that case, the certificate shall indicate that the maintenance could not be completed, as well as indicate any applicable airworthiness or operations limitations, as part of the information required by point (e)(4).

A CRS shall not be issued in the case of any known non-compliance which endangers flight safety.

Except for components released to service by a maintenance organisation that is approved in accordance with Annex II (Part-145) and for the cases covered by point (e) of point M.A.502, a CRS shall be issued at the completion of any maintenance work carried out on an aircraft component in accordance with point M.A.502.

The authorised release certificate identified as EASA Form 1 constitutes the component CRS, except when such maintenance on aircraft components has been performed in accordance with point (b) or (d) of point M.A.502 in which case the maintenance is subject to aircraft release procedures in accordance with point M.A.801.

To qualify as a Pilot-owner, the person must:

For any other than complex motor-powered aircraft of 2 730  kg MTOM and below, which are not used in CAT operations, in commercial specialised operations or in commercial operations by ATOs or DTOs, the pilot-owner may issue a CRS after having carried out limited pilot-owner maintenance as specified in Appendix VIII to this Annex.

The scope of the limited Pilot-owner maintenance shall be specified in the aircraft maintenance programme referred to in point M.A.302.

The CRS shall be entered in the aircraft continuing airworthiness record system and contain basic details of the maintenance carried out, the maintenance data used, the date on which that maintenance was completed, as well as the identity, the signature and pilot licence number of the pilot-owner issuing such a certificate.

An airworthiness review certificate is issued in accordance with Appendix III (EASA Form 15a or 15b) to this Annex upon completion of a satisfactory airworthiness review. The airworthiness review certificate shall be valid for 1 year;

An aircraft in a controlled environment is an aircraft which, during the preceding 12 months:

►M8  For all aircraft used by air carriers licensed in accordance with Regulation (EC) No 1008/2008, and for aircraft above 2 730 kg MTOM that are in a controlled environment, the organisation referred to in point (b)(1) managing the continuing airworthiness of the aircraft may in accordance with CAMO.A.125(e) of Annex Vc or point M.A.711(b) of this Annex or point CAO.A.095(c)(1) of Annex Vd, as applicable, and subject to compliance with point (j): ◄

The airworthiness review certificate shall be issued by the competent authority upon a satisfactory assessment based on a recommendation made by a CAMO or CAO, sent together with the application from the owner or operator for all aircraft used by air carriers licensed in accordance with Regulation (EC) No 1008/2008, and for aircraft above 2 730  kg MTOM that complies with the following alternative conditions:

The recommendation referred to in the first subparagraph shall be based on an airworthiness review carried out in accordance with point M.A.901.

For aircraft of 2 730 kg MTOM and below not used by air carriers licensed in accordance with Regulation (EC) No 1008/2008, any CAMO or CAO chosen by the owner or operator may in accordance with CAMO.A.125(e) of Annex Vc or point M.A.711(b) of this Annex or CAO.A.095(c) of Annex Vd, as applicable, and subject to compliance with point (j):

▼C1

By derogation from points (c)(2) and (e)(2) of point M.A.901, for aircraft that are in a controlled environment, the organisation referred to in point (b)(1) managing the continuing airworthiness of the aircraft, may, subject to compliance with point (j), extend at most twice the validity of an airworthiness review certificate that the competent authority or another CAMO or CAO has issued, for a period of 1 year each time.

Whenever circumstances reveal the existence of a potential risk to aviation safety, the competent authority shall carry out the airworthiness review and issue the airworthiness review certificate itself.

Without prejudice to point (g), the competent authority may carry out the airworthiness review and issue the airworthiness review certificate itself in the following cases:

Where the competent authority issues the airworthiness review certificate itself in accordance with points (g) or (h) or after assessing the recommendation in accordance with point M.B.901, the owner or operator of the aircraft shall, where necessary for those purposes, provide the competent authority with:

An airworthiness review certificate shall not be issued, nor extended if there is evidence or indications that the aircraft is not airworthy.

The airworthiness review of the aircraft shall include a full documented review of the aircraft records establishing that the following requirements have been met:

The airworthiness review of the aircraft shall include a physical survey of the aircraft. For that survey, airworthiness review staff not appropriately qualified in accordance with Annex III (Part-66) shall be assisted by such qualified staff.

Through the physical survey of the aircraft, the airworthiness review staff shall ensure that:

By derogation from point (a), the airworthiness review may be anticipated by a maximum period of 90 days without loss of continuity of the airworthiness review pattern, so as to allow for the physical review to take place during a maintenance check.

The airworthiness review certificate (EASA Form 15b) or the recommendation for the issue of the airworthiness review certificate (EASA Form 15a) referred to in Appendix III to this Annex can only be issued:

A copy of any airworthiness review certificate issued or extended for an aircraft shall be sent to the Member State of registry of the aircraft concerned within 10 days.

Airworthiness review tasks shall not be subcontracted.

Should the outcome of the airworthiness review be inconclusive, the organisation having carried out the review shall inform the competent authority as soon as possible and in any case within 72 hours from the moment the organisation identifies the reason for which the airworthiness review is inconclusive.

The airworthiness review certificate shall not be issued until all findings have been closed.

An airworthiness review certificate becomes invalid if:

An aircraft must not fly if the airworthiness certificate is invalid or if:

▼M6

▼B

Upon surrender or revocation, the airworthiness review certificate shall be returned to the competent authority

When transferring an aircraft registration within the EU, the applicant shall:

Notwithstanding point M.A.902(a)(3), the former airworthiness review certificate shall remain valid until its expiry date.

When importing an aircraft onto a Member State register from a third country or from a regulatory system where Regulation (EU) 2018/1139 does not apply, the applicant shall:

When satisfied that the aircraft is in compliance with the relevant requirements, the organisation performing the airworthiness review, shall send a documented recommendation for the issuance of an airworthiness review certificate to the competent authority of the Member State of registry.

The owner of the aircraft shall allow access to the aircraft for inspection by the competent authority of the Member State of registry.

The competent authority of the Member State of registry shall issue an airworthiness certificate when it is satisfied that the aircraft complies with the requirements of Annex I (Part-21) to Regulation (EU) No 748/2012.

That competent authority of the Member State shall also issue the airworthiness review certificate. The certificate shall be valid for 1 year, unless the competent authority decides to reduce the period of validity for reasons of aviation safety.

A level 1 finding is any finding of significant non-compliance with the requirements of this Annex, which lowers the safety standard and seriously endangers flight safety.

A level 2 finding is any finding of non-compliance with the requirements of this Annex, which may lower the safety standard and may endanger the flight safety.

After receipt of notification of findings according to point M.B.903, the person or organisation accountable referred to in point M.A.201 shall define a corrective action plan and demonstrate corrective action to the satisfaction of the competent authority within a period agreed with this authority including appropriate corrective action to prevent reoccurrence of the finding and its root cause.

The competent authorities shall establish a system of record-keeping that allows adequate traceability of the process to issue, continue, change, suspend or revoke each certificate.

The records for the oversight of organisations approved in accordance with this Annex shall include as a minimum:

The retention period for the point (b) records shall be at least 5 years.

The minimum records for the oversight of each aircraft shall include, at least, a copy of:

▼M8

▼C1

The records specified in point (d) shall be retained until 2 years after the aircraft has been permanently withdrawn from service.

All records shall be made available upon request by another Member State or the Agency.

In order to contribute to the improvement of air safety, the competent authorities shall participate in a mutual exchange of all necessary information in accordance with Article 72 of Regulation (EU) 2018/1139.

Without prejudice to the competencies of the Member States, in the case of a potential safety threat involving several Member States, the concerned competent authorities shall assist each other in carrying out the necessary oversight action.

The competent authority shall without undue delay notify the Agency in case of any significant problems with the implementation of Regulation (EU) 2018/1139.

The competent authority shall provide the Agency with safety-significant information stemming from the occurrence reports it has received pursuant to point M.A.202.

The competent authority shall verify that the AMP is in compliance with point M.A.302.

Unless stated otherwise in point (c) of point M.A.302, the AMP and its amendments shall be approved directly by the competent authority. The competent authority shall have access to all the data required by points (d), (e) and (f) of point M.A.302.

In the case of indirect approval as provided for in point M.A.302(c), the competent authority shall approve the AMP approval procedure of the CAO or CAMO through that organisation’s exposition referred to in point CAO.A.025 of Annex Vd, point M.A.704 of this Annex, or point CAMO.A.300 of Annex Vc, as applicable.

The competent authority shall develop a survey programme on a risk-based approach to monitor the airworthiness status of the fleet of aircraft on its register.

The survey programme shall include sample product surveys of aircraft and shall cover all aspects of airworthiness key risk elements.

The product survey shall sample the airworthiness standards achieved, on the basis of the applicable requirements, and identify any findings.

Any findings identified shall be categorised against the requirements of this Part and confirmed in writing to the person or organisation accountable according to M.A.201. The competent authority shall have a process in place to analyse findings for their safety significance.

The competent authority shall record all findings and closure actions.

If during aircraft surveys evidence is found showing non-compliance with this Part or with any other Part, the finding shall be dealt with as prescribed by the relevant Part.

If so required to ensure appropriate enforcement action, the competent authority shall exchange information on non-compliances identified in accordance with point (f) with other competent authorities.

suspend an airworthiness review certificate on reasonable grounds in the case of potential safety threat, or;

suspend or revoke an airworthiness review certificate pursuant to M.B.903(1).

The competent authority shall approve the initial aircraft technical log system required by point M.A.306.

To enable the organisation to implement changes to the aircraft technical log system without prior competent authority approval, the competent authority shall approve the relevant procedure referred to in point CAMO.A.300(c) of Annex Vc, or point M.A.704(c) of this Annex or point CAO.A.025(c) of Annex Vd.

Provided the requirements of points M.A.606(a) and (b) are complied with, the competent authority shall formally indicate its acceptance of the M.A.606(a) and (b) personnel to the applicant in writing.

The competent authority shall establish that the procedures specified in the maintenance organisation manual comply with Subpart F of this Annex, and shall ensure that the accountable manager signs the commitment statement.

The competent authority shall verify that the organisation is in compliance with the requirements laid down in Subpart F of this Annex.

A meeting with the accountable manager shall be convened at least once during the investigation for approval to ensure that he/she fully understands the significance of the approval and the reason for signing the commitment of the organisation to compliance with the procedures specified in the manual.

All findings shall be confirmed in writing to the applicant organisation.

The competent authority shall record all findings, closure actions (actions required to close a finding) and recommendations.

For initial approval all findings shall be corrected by the organisation and closed by the competent authority before the approval can be issued.

The competent authority shall issue to the applicant an EASA Form 3 approval certificate (Appendix V to this Annex), which includes the extent of the approval, when the maintenance organisation is in compliance with the applicable points of this Annex.

The competent authority shall indicate the conditions attached to the approval on the EASA Form 3 approval certificate.

The reference number shall be included on the EASA Form 3 approval certificate in a manner specified by the Agency.

The competent authority shall keep and update a programme listing, for each maintenance organisation approved in accordance with Subpart F of Section B of this Annex under its supervision, the dates when audit visits are due and when such visits were carried out.

Each organisation shall be completely audited at periods not exceeding 24 months.

All findings shall be confirmed in writing to the applicant organisation.

The competent authority shall record all findings, closure actions (actions required to close a finding) and recommendations.

A meeting with the accountable manager shall be convened at least once every 24 months to ensure he/she remains informed of significant issues arising during audits.

When during audits or by other means evidence is found showing non-compliance with a requirement laid down in this Annex or Annex Vb (Part-ML), the competent authority shall take the following actions:

▼B

Action shall be taken by the competent authority to suspend in whole or part the approval in case of failure to comply within the timescale granted by the competent authority.

The competent authority shall comply with the applicable elements of the initial approval for any change to the organisation notified in accordance with point M.A.617.

The competent authority may prescribe the conditions under which the approved maintenance organisation may operate during such changes, unless it determines that the approval should be suspended due to the nature or the extent of the changes.

For any change to the maintenance organisation manual:

suspend an approval on reasonable grounds in the case of potential safety threat, or;

suspend, revoke or limit an approval pursuant to point M.B.605.

For licenced air carriers in accordance with Regulation (EC) No 1008/2008 the competent authority shall receive for approval with the initial application for the air operator's certificate and where applicable any variation applied for and for each aircraft type to be operated:

Where facilities are located in more than one Member State the investigation and continued oversight of the approval shall be carried out in conjunction with the competent authorities designated by the Member States in whose territory the other facilities are located.

Provided the requirements of points M.A.706(a), (c), (d) and M.A.707 are complied with, the competent authority shall formally indicate its acceptance of the M.A.706(a), (c), (d) and M.A.707 personnel to the applicant in writing.

The competent authority shall establish that the procedures specified in the continuing airworthiness management exposition comply with Section A, Subpart G of this Annex (Part-M) and ensure the accountable manager signs the commitment statement.

The competent authority shall verify the organisation's compliance with requirements laid down in Section A, Subpart G of this Annex (Part-M).

A meeting with the accountable manager shall be convened at least once during the investigation for approval to ensure that he/she fully understands the significance of the approval and the reason for signing the exposition commitment of the organisation to compliance with the procedures specified in the continuing airworthiness management exposition.

All findings shall be confirmed in writing to the applicant organisation.

The competent authority shall record all findings, closure actions (actions required to close a finding) and recommendations.

For initial approval all findings shall be corrected by the organisation and closed by the competent authority before the approval can be issued.

The competent authority shall issue to the applicant an EASA Form 14-MG approval certificate (Appendix VI to this Annex) which includes the extent of approval, when the continuing airworthiness management organisation is in compliance with Section A, Subpart G of this Annex (Part-M).

The competent authority shall indicate the validity of the approval on the EASA Form 14 MG approval certificate.

The reference number shall be included on the Form 14 MG approval certificate in a manner specified by the Agency.

In the case of licenced air carriers in accordance with Regulation (EC) No 1008/2008, the information contained on an EASA Form 14 MG will be included on the air operator's certificate.

The competent authority shall keep and update a program listing, for each continuing airworthiness organisation approved under Section A, Subpart G of this Annex (Part-M) under its supervision, the dates when audit visits are due and when such visits were carried out.

Each organisation shall be completely audited at periods not exceeding 24 months.

A relevant sample of the aircraft managed by the organisation approved under Section B, Subpart G of this Annex (Part-M) shall be surveyed in every 24 month period. The size of the sample will be decided by the competent authority based on the result of prior audits and earlier product surveys.

All findings shall be confirmed in writing to the applicant organisation.

The competent authority shall record all findings, closure actions (actions required to close a finding) and recommendations.

A meeting with the accountable manager shall be convened at least once every 24 months to ensure he/she remains informed of significant issues arising during audits.

▼M8

When during audits or by other means, evidence is found showing non-compliance to a requirement laid down in this Annex (Part-M) or Annex Vb (Part-ML), as applicable, the competent authority shall take the following actions:

▼B

Action shall be taken by the competent authority to suspend in whole or part the approval in case of failure to comply within the timescale granted by the competent authority.

The competent authority shall comply with the applicable elements of the initial approval for any change to the organisation notified in accordance with point M.A.713.

The competent authority may prescribe the conditions under which the approved continuing airworthiness management organisation may operate during such changes unless it determines that the approval should be suspended due to the nature or the extent of the changes.

For any change to the continuing airworthiness management exposition:

suspend an approval on reasonable grounds in the case of potential safety threat, or;

suspend, revoke or limit an approval pursuant to point M.B.705.

Appropriately qualified personnel of the competent authority shall verify that the compliance statement contained in the recommendation demonstrates that a complete airworthiness review in accordance with point M.A.901 has been carried out.

The competent authority shall investigate and may request further information to support the assessment of the recommendation.

When the competent authority carries out the airworthiness review and issues the airworthiness review certificate (Appendix III (EASA Form 15a) to this Annex), the competent authority shall carry out an airworthiness review in accordance with point M.A.901.

The competent authority shall have appropriate airworthiness review staff to carry out the airworthiness reviews.

The competent authority shall maintain a record of all airworthiness review staff, which shall include details of any appropriate qualification held together with a summary of relevant continuing airworthiness management experience and training.

The competent authority shall have access to the applicable data as specified in points M.A.305, M.A.306 and M.A.401 in the performance of the airworthiness review.

The staff that carries out the airworthiness review shall issue a Form 15a after satisfactory completion of the airworthiness review.

for level 1 findings, the competent authority shall require appropriate corrective action to be taken before further flight and immediate action shall be taken by the competent authority to revoke or suspend the airworthiness review certificate.

for level 2 findings, the corrective action required by the competent authority shall be appropriate to the nature of the finding.

Maintenance data used, including the revision status and reference.

Compliance with airworthiness directives or service bulletins.

Repairs carried out.

Modifications carried out.

Replacement parts installed.

Life limited parts status.

Deviations from the customer work order.

Release statements to satisfy a foreign Civil Aviation Authority maintenance requirement.

Information needed to support shipment with shortages or re-assembly after delivery.

For maintenance organisations approved in accordance with Subpart F of Annex I (Part-M) or Annex Vd (Part-CAO), the component CRS statement referred to in point M.A.613 and CAO.A.070, as applicable:

‘Certifies that, unless otherwise specified in this block, the work identified in block 11 and described in this block was accomplished in accordance with the requirements of Section A, Subpart F of Annex I (Part-M) or Annex Vd (Part-CAO) to Regulation (EU) No 1321/2014, and in respect to that work the item is considered ready for release to service. THIS IS NOT A RELEASE UNDER ANNEX II (PART-145) TO REGULATION (EU) No 1321/2014.’

If printing the data from an electronic EASA Form 1, any appropriate data not fit for other blocks should be entered in this block.

where maintenance could not be completed;

where maintenance deviated from the standard required by Annex I (Part-M) or Annex Vd (Part-CAO);

where maintenance was carried out in accordance with a requirement other than that specified in Annex I (Part-M) or Annex Vd (Part-CAO); in this case, block 12 shall specify the particular national regulation.

where maintenance could not be completed;

where maintenance deviated from the standard required by Annex II (Part-145);

where maintenance was carried out in accordance with a requirement other than that specified in Annex II (Part-145); in this case, block 12 shall specify the particular national regulation.

Except as stated otherwise for the smallest organisations in point 12, the table referred to in point 13 provides the standard system for the approval of maintenance organisation under Subpart F of Annex I (Part-M) and Annex II (Part-145). An organisation must be granted an approval ranging from a single class and rating with limitations to all classes and ratings with limitations.

In addition to the table referred to in point 13, the approved maintenance organisation is required to indicate its scope of work in its maintenance organisation manual/exposition. See also point 11.

Within the approval class(es) and rating(s) granted by the competent authority, the scope of work specified in the maintenance organisation exposition defines the exact limits of approval. It is therefore essential that the approval class(es) and rating(s) and the organisations scope of work are matching.

A category A class rating means that the approved maintenance organisation may carry out maintenance on the aircraft and any component (including engines and/or Auxiliary Power Units (APUs), in accordance with aircraft maintenance data or, if agreed by the competent authority, in accordance with component maintenance data, only whilst such components are fitted to the aircraft. Nevertheless, such A-rated approved maintenance organisation may temporarily remove a component for maintenance, in order to improve access to that component, except when such removal generates the need for additional maintenance not eligible for the provisions of this point. This will be subject to a control procedure in the maintenance organisation exposition to be approved by the competent authority. The limitation section will specify the scope of such maintenance thereby indicating the extent of approval.

A category B class rating means that the approved maintenance organisation may carry out maintenance on the uninstalled engine and/or APU and engine and/or APU components, in accordance with engine and/or APU maintenance data or, if agreed by the competent authority, in accordance with component maintenance data, only whilst such components are fitted to the engine and/or APU. Nevertheless, such B-rated approved maintenance organisation may temporarily remove a component for maintenance, in order to improve access to that component, except when such removal generates the need for additional maintenance not eligible for the provisions of this point. The limitation section will specify the scope of such maintenance thereby indicating the extent of approval. A maintenance organisation approved with a category B class rating may also carry out maintenance on an installed engine during ‘base’ and ‘line’ maintenance subject to a control procedure in the maintenance organisation exposition to be approved by the competent authority. The maintenance organisation exposition scope of work shall reflect such activity where permitted by the competent authority.

A category C class rating means that the approved maintenance organisation may carry out maintenance on uninstalled components (excluding engines and APUs) intended for fitment to the aircraft or engine/APU. The limitation section will specify the scope of such maintenance thereby indicating the extent of approval. A maintenance organisation approved with a category C class rating may also carry out maintenance on an installed component during base and line maintenance or at an engine/APU maintenance facility subject to a control procedure in the maintenance organisation exposition to be approved by the competent authority. The maintenance organisation exposition scope of work shall reflect such activity where permitted by the competent authority.

A category D class rating is a self contained class rating not necessarily related to a specific aircraft, engine or other component. The D1 — Non Destructive Testing (NDT) rating is only necessary for an approved maintenance organisation that carries out NDT as a particular task for another organisation. A maintenance organisation approved with a class rating in A or B or C category may carry out NDT on products it is maintaining subject to the maintenance organisation exposition containing NDT procedures, without the need for a D1 class rating.

In the case of maintenance organisations approved in accordance with Annex II (Part-145), category A class ratings are subdivided into ‘Base’ or ‘Line’ maintenance. 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.

The limitation section is intended to give the competent authorities the flexibility to customise the approval to any particular organisation. Ratings shall be mentioned on the approval only when appropriately limited. The table referred to in point 13 specifies the types of limitation possible. Whilst maintenance is listed last in each class rating it is acceptable to stress the maintenance task rather than the aircraft or engine type or manufacturer, if this is more appropriate to the organisation (an example could be avionic systems installations and related maintenance). Such mention in the limitation section indicates that the maintenance organisation is approved to carry out maintenance up to and including this particular type/task.

When reference is made to series, type and group in the limitation section of class A and B, series means a specific type series such as Airbus 300 or 310 or 319 or Boeing 737-300 series or RB211-524 series or Cessna 150 or Cessna 172 or Beech 55 series or continental O-200 series etc; type means a specific type or model such as Airbus 310-240 type or RB 211-524 B4 type or 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.

When a lengthy capability list is used which could be subject to frequent amendment, then such amendment may be in accordance with the indirect approval procedure referred to in points M.A.604(c) and M.B.606(c) or 145.A.70(c) and 145.B.40, as applicable.

A maintenance organisation which employs only one person to both plan and carry out all maintenance can only hold a limited scope of approval rating. The maximum permissible limits are:

It should be noted that such an organisation may be further limited by the competent authority in the scope of approval dependent upon the capability of the particular organisation.

Table

This certificate is limited to what is specified in the scope of work section of the approved maintenance organisation manual as referred to in Section A, Subpart F of Annex I (Part-M) to Commission Regulation (EU) No 1321/2014; and

This certificate requires compliance with the procedures specified in the approved maintenance organisation manual; and

This certificate is valid whilst the approved maintenance organisation remains in compliance with Annex I (Part-M) and Annex Vb (Part-ML) to Commission Regulation (EU) No 1321/2014.

Subject to compliance with the foregoing conditions, this certificate shall remain valid until 24 March 2022 unless the certificate has been surrendered, superseded, suspended or revoked before that date.

This certificate is limited to that specified in the scope of work section of the approved continuing airworthiness management exposition as referred to in Section A, Subpart G of Annex I (Part-M) to Regulation (EU) No 1321/2014.

This certificate requires compliance with the procedures specified in the continuing airworthiness management exposition approved in accordance with Subpart G of Annex I (Part-M) to Regulation (EU) No 1321/2014.

This certificate is valid whilst the approved continuing airworthiness management organisation remains in compliance with Annex I (Part-M) and, if applicable, Annex Vb (Part-ML) to Regulation (EU) No 1321/2014.

Where the continuing airworthiness management organisation contracts under its Quality System the service of an organisation or several organisations, this certificate remains valid subject to such organisation(s) fulfilling applicable contractual obligations.

Subject to compliance with the conditions 1 to 4 above, this certificate shall remain valid until 24 March 2022, unless the certificate has previously been surrendered, superseded, suspended or revoked.

If this form is also used for licenced air carriers in accordance with Regulation (EC) No 1008/2008, the Air Operator Certificate (AOC) number shall be added to the reference, in addition to the standard number, and the condition 5 shall be replaced by the following extra conditions 6, 7 and 8:

This certificate does not constitute an authorisation to operate the types of aircraft referred in condition 1. The authorisation to operate the aircraft is the AOC.

Termination, suspension or revocation of the AOC automatically invalidates this certificate in relation to the aircraft registrations specified in the AOC, unless otherwise explicitly stated by the competent authority.

Subject to compliance with conditions 1 to 4, 6 and 7, this certificate shall remain valid until 24 March 2022, unless the certificate has previously been surrendered, superseded, suspended or revoked.

The modification, repair or replacement by riveting, bonding, laminating, or welding of any of the following airframe parts:

The modification or repair of any of the following parts:

The performance of the following maintenance on a piston engine:

The balancing of a propeller, except:

Any additional task that requires:

Competence and responsibility

▼M8

▼B

Tasks

The Pilot-owner may carry out simple visual inspections or operations to check for general condition and obvious damage and normal operation of the airframe, engines, systems and components.

Maintenance tasks shall not be carried out by the Pilot-owner when the task:

▼M2

▼B

▼M6 —————

▼M1

The criteria 1 to 9 cannot be overridden by less restrictive instructions issued in accordance with ‘M.A.302(d) Maintenance Programme’.

▼B

Any task described in the aircraft flight manual as preparing the aircraft for flight (Example: assembling the glider wings or pre-flight), is considered to be a pilot task and is not considered a Pilot-owner maintenance task and therefore does not require a Certificate of Release to Service.

Performance of the maintenance Pilot-owner tasks and records

The maintenance data as specified in point M.A.401 must be always available during the conduct of Pilot-owner maintenance and must be complied with. Details of the data referred to in the conduct of Pilot-owner maintenance must be included in the Certificate of Release to Service in accordance with point M.A.803(d).

The Pilot-owner must inform the approved continuing airworthiness management organisation responsible for the continuing airworthiness of the aircraft (if applicable) not later than 30 days after completion of the Pilot-owner maintenance task in accordance with point M.A.305(a).