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Part M, DECISION NO. 2003/19/RM, Annex I,AMC-GM

CONTINUING AIRWORTHINESS REQUIREMENTS – PART M

Consolidated version of Part M of the Commission Regulation

EC No. 2042/2003, and related EASA Decisions*

(Acceptable Means of Compliance and Guidance Material), as amended

Issue: July 2010

 

* Konsolidierte Fassung nicht amtlich

 

PART M

amended by

EU No. 127/2010

EC No. 1056/2008

EC No. 376/2007

EC No. 707/2006

 

+ AMC/GM Part M

Decision 2003/19/RM

amended by

Decision 2013/025/R

Decision 2013/005/R

Decision 2012/004/R

Decision 2011/002/R

Decision 2010/006/R

Decision 2010/002/R

Decision 2009/006/R

Decision 2008/013/R

Decision 2007/001/R

Decision 2006/14/R

Decision 2006/11/R

 

 

 

Commission Regulation (EC) No. 2042/2003

of 20 November 2003


on the continuing airworthiness of aircraft and aeronautical products, parts and appliances,

and on the approval of organisations and personnel involved in these tasks

 

(Text with EEA relevance)

 

Contents

Article 1 Objective and scope

Article 2 Definitions

Article 3 Continuing airworthiness requirements

Article 4 Maintenance organisation approvals

Article 5 Certifying staff 

Article 6 Training organisation requirements

Article 7 Entry into force 

ANNEX I (Part-M)

M.1

AMC M.1

Section A TECHNICAL REQUIREMENTS

Subpart A GENERAL

M.A.101 Scope

Subpart B ACCOUNTABILITY

M.A.201 Responsibilities

AMC M.A.201 (e)

AMC M.A.201 (h) 

 AMC M.A.201 (h)(1)

AMC M.A.201 (h)(2)

M.A.202 Occurrence reporting

AMC M.A.202 (a)

AMC M.A.202 (b)

Subpart C CONTINUING AIRWORTHINESS 

M.A.301 Continuing airworthiness tasks

AMC M.A.301-1 

AMC M.A.301-2

AMC M.A.301-3 

AMC M.A.301-4

AMC M.A.301-5

AMC M.A.301-7

M.A.302 Aircraft Maintenance Programme

AMC M.A.302

AMC M.A.302 (a)

AMC M.A.302 (d)

AMC M.A.302 (f)

M.A.303 Airworthiness directives

M.A.304 Data for modifications and repairs

AMC M.A.304

M.A.305 Aircraft continuing airworthiness record system

AMC M.A.305 (d)
AMC M.A.305 (d)(4) and AMC M.A.305 (h)
AMC M.A.305 (h)
AMC M.A.305 (h)(6)
M.A.306 Operator’s technical log system
AMC M.A.306 (a)
AMC M.A.306 (b)
M.A.307 Transfer of aircraft continuing airworthiness records
AMC M.A.307 (a)

Subpart

D MAINTENANCE STANDARDS

M.A.401

Maintenance data


AMC M.A.401 (b) Maintenance data


AMC M.A.401 (c) Maintenance data

M.A.402

Performance of maintenance


AMC M.A.402 (a)


AMC M.A.402 (b)


AMC M.A.402 (d)


AMC M.A.402 (e)

M.A.403

Aircraft defects


AMC M.A.403 (b)


AMC M.A.403 (d)

Subpart

E COMPONENTS

M.A.501

Installation


AMC M.A.501 (a)


AMC M.A.501 (b)


AMC M.A.501 (c)


AMC M.A.501 (d)

M.A.502

Component maintenance


AMC M.A.502


AMC M.A.502 (b) and (c)

M.A.503

Service life limited components

M.A.504

Control of unserviceable components


AMC M.A.504 (a)


AMC M.A.504 (b)


AMC M.A.504 (c)


AMC M.A.504 (d)(2)


AMC M.A.504 (e)

Subpart

F MAINTENANCE ORGANISATION 

M.A.601

Scope


AMC M.A.601

M.A.602

Application


AMC M.A.602

M.A.603

Extent of approval


AMC M.A.603 (a)


AMC M.A.603 (c)


M.A.604

Maintenance organisation manual


AMC M.A.604

M.A.605

Facilities


AMC M.A.605 (a)


AMC M.A.605 (b)


AMC M.A.605 (c)

M.A.606

Personnel requirements


AMC M.A.606 (a)


AMC M.A.606 (b)


AMC M.A.606 (c)


AMC M.A.606 (d)


AMC M.A.606 (e)


AMC M.A.606 (f)


AMC M.A.606 (h)(2)

M.A.607

Certifying staff


AMC M.A.607


AMC M.A.607 (c)

M.A.608

Components, equipment and tools


AMC M.A.608 (a)


AMC M.A.608 (b)

M.A.609

Maintenance data


AMC M.A.609

M.A.610

Maintenance work orders


AMC M.A.610

M.A.611

Maintenance standards

M.A.612

Aircraft certificate of release to service

M.A.613

Component certificate of release to service


AMC M.A.613 (a)

M.A.614

Maintenance records


AMC M.A.614 (a)


AMC M.A.614 (c)

M.A.615

Privileges of the organisation


AMC M.A.615 (b)

M.A.616

Organisational review


AMC M.A.616

M.A.617

Changes to the approved maintenance organisation


AMC M.A.617

M.A.618

Continued validity of approval

M.A.619

Findings

Subpart

G CONTINUING AIRWORTHINESS MANAGEMENT ORGANISATION 

M.A.701

Scope

M.A.702

Application


AMC M.A.702

M.A.703

Extent of approval

M.A.704

Continuing airworthiness management exposition


AMC M.A.704

M.A.705

Facilities


AMC M.A.705


M.A.706

Personnel requirements


AMC M.A.706


AMC M.A.706 (a)


AMC M.A.706 (e)


AMC M.A.706 (f)


AMC M.A.706 (i)


AMC M.A.706 (k)

M.A.707

Airworthiness review staff


AMC M.A.707 (a)


AMC M.A.707 (a)(1)


AMC M.A.707 (a)(2)


AMC M.A.707 (b)


AMC M.A.707 (c)


AMC M.A.707 (e)

M.A.708

Continuing airworthiness management


AMC M.A.708 (b)(3)


AMC M.A.708 (c)


AMC M.A.708 (c)(1)

M.A.709

Documentation


AMC M.A.709

M.A.710

Airworthiness review


AMC M.A.710 (a)


AMC M.A.710 (b) and (c)


AMC M.A.710 (d)


AMC M.A.710 (e)

M.A.711

Privileges of the organisation


AMC M.A.711 (b)


AMC M.A.711 (c)

M.A.712

Quality system


AMC M.A.712 (a)


AMC M.A.712 (b)


AMC M.A.712 (f)

M.A.713

Changes to the approved continuing airworthiness organisation


AMC M.A.713

M.A.714

Record-keeping


AMC M.A.714

M.A.715

Continued validity of approval

M.A.716

Findings

Subpart

H CERTIFICATE OF RELEASE TO SERVICE – CRS

M.A.801

Aircraft certificate of release to service


AMC M.A.801 (b)


AMC M.A.801 (d)


AMC M.A.801 (f)


AMC M.A.801 (g)


AMC M.A.801 (h)

M.A.802

Component certificate of release to service


AMC M.A.802

M.A.803

Pilot-owner authorisation


AMC M.A.803




Subpart I

AIRWORTHINESS REVIEW CERTIFICATE

M.A.901

Aircraft airworthiness review


AMC M.A.901


AMC M.A.901 (a)


AMC M.A.901 (b)


AMC M.A.901 (c)(2), (e)(2) and (f)


AMC M.A.901 (d) and (g)


AMC M.A.901 (g)


AMC M.A.901 (j)

M.A.902

Validity of the airworthiness review certificate

M.A.903

Transfer of aircraft registration within the EU


AMC M.A.903 (a)(1)


AMC M.A.903 (b)

M.A.904

Airworthiness review of aircraft imported into the EU


AMC M.A.904 (a)(1)


AMC M.A.904 (a)(2)


AMC M.A.904 (b)

M.A.905

Findings

 

Section B PROCEDURE FOR COMPETENT AUTHORITIES 

 

Subpart A GENERAL

M.B.101

Scope

M.B.102

Competent authority


AMC M.B.102 (a)


AMC M.B.102 (c)


AMC M.B.102 (d)

M.B.103

Acceptable means of compliance

M.B.104

Record-keeping


AMC M.B.104 (a)


AMC M.B.104 (f)

M.B.105

Mutual exchange of information


AMC M.B.105 (a)

Subpart

B ACCOUNTABILITY

M.B.201

Responsibilities

Subpart

C CONTINUING AIRWORTHINESS

M.B.301

Maintenance programme


AMC M.B.301 (a)


AMC M.B.301 (b)


AMC M.B.301 (c)


AMC M.B.301 (d)

M.B.302

Exemptions

M.B.303

Aircraft continuing airworthiness monitoring


AMC M.B.303


AMC M.B.303 (b)


AMC M.B.303 (c)


AMC M.B.303 (d)

M.B.304

Revocation, suspension and limitation

Subpart

D MAINTENANCE STANDARDS


Subpart E

COMPONENTS 

Subpart F

MAINTENANCE ORGANISATION 

M.B.601

Application

M.B.602

Initial Approval


AMC M.B.602 (a)


AMC M.B.602 (b)


AMC M.B.602 (c)


AMC M.B.602 (e)


AMC M.B.602 (f)


AMC M.B.602 (g)

M.B.603

Issue of approval


AMC M.B.603 (a)


AMC M.B.603 (c)

M.B.604

Continuing oversight


AMC M.B.604 (b)

M.B.605

Findings


AMC M.B.605 (b)(1)

M.B.606

Changes


AMC M.B.606

M.B.607

Revocation, suspension and limitation of an approval

Subpart

G CONTINUING AIRWORTHINESS MANAGEMENT ORGANISATION .......

M.B.701

Application


AMC M.B.701 (a)

M.B.702

Initial approval


AMC M.B.702 (a)


AMC M.B.702 (b)


AMC M.B.702 (c)


AMC M.B.702 (e)


AMC M.B.702 (f)


AMC M.B.702 (g)

M.B.703

Issue of approval


AMC M.B.703


AMC M.B.703 (a)


AMC M.B.703 (c)

M.B.704

Continuing oversight


AMC M.B.704 (b)

M.B.705

Findings


AMC M.B.705 (a)(1)

M.B.706

Changes


AMC M.B.706

M.B.707

Revocation, suspension and limitation of an approval

Subpart

H CERTIFICATE OF RELEASE TO SERVICE – CRS

Subpart

I AIRWORTHINESS REVIEW CERTIFICATE

M.B.901

Assessment of recommendations


AMC M.B.901

M.B.902

Airworthiness review by the competent authority


AMC M.B.902 (b)

AMC M.B.902 (b)(1)
AMC M.B.902 (b)(2)
AMC M.B.902 (c)
M.B.903 Findings

APPENDICES

TO THE IMPLEMENTING RULES

Appendix I

Continuing Airworthiness Arrangement

Appendix II

EASA Form 1: Authorised Release Certificate EASA Form 1
AMC to Appendix II to Part-M: Use of the EASA Form 1 for maintenance
GM to Appendix II to Part-M: Use of the EASA Form 1 for maintenance

Appendix III

Airworthiness Review Certificate – EASA Form 15

Appendix IV

Approval Ratings

Appendix V

Maintenance Organisation Approval … EASA Form 3
AMC to Appendix V

Appendix VI

Continuing Airworthiness Management Organisation … EASA Form 14
AMC to Appendix VI
Approval Certificate referred to in Annex I (Part-M) Subpart G

Appendix VII

Complex Maintenance Tasks

 

AMC to Appendix VII

Appendix VIII

Limited Pilot-Owner Maintenance
AMC to Appendix VIII

APPENDICES 

TO AMCs

Appendix I 

to AMC M.A.302 and AMC M.B.301 (b): Content of the maintenance programme

Appendix II

to M.A. 201 (h)(1): Sub-contracting of continuing airworthiness management tasks

Appendix III

to AMC M.B.303 (d)

Appendix IV

to AMC M.A.604 Maintenance Organisation Manual

Appendix V

to AMC M.A.704 Continuing airworthiness management organisation exposition

Appendix VI

to AMC M.B.602 (f) EASA Form 6F

Appendix VII

to AMC M.B.702 (f) EASA Form 13

Appendix VIII

to AMC M.A.616

Appendix IX

to AMC M.A.602 and AMC M.A.702 EASA Form 2

Appendix X

to AMC M.B.602 (a) and AMC M.B.702 (a) EASA Form 4

Appendix XI

to AMC to M.A.708 (c)

Appendix XII

to AMC to M.A.706 (f) and M.B.102 (c)

Appendix XIII

to AMC M.A.712 (f)


Article 1

Objective and scope

1.    This Regulation establishes common technical requirements and administrative procedures for ensuring the continuing airworthiness of aircraft, including any component for installation thereto, which are:

(a) registered in a Member State; or

(b) registered in a third country and used by an operator for which a Member State ensures oversight of operations.

2.    Paragraph 1 shall not apply to aircraft the regulatory safety oversight of which has been transferred to a third country and which are not used by a Community operator, or to aircraft referred to in Annex II to the basic Regulation.

3.    The provisions of this Regulation related to commercial air transport are applicable to licensed air carriers as defined by Community law.

Article 2

Definitions

Within the scope of the basic Regulation, the following definitions shall apply:

(a)   “aircraft” means any machine that can derive support in the atmosphere from the reactions of the air other than reactions of the air against the earth’s surface;

(b)   “certifying staff” means personnel responsible for the release of an aircraft or a component after maintenance;

(c) “component” means any engine, propeller, part or appliance;

(d) “continuing airworthiness” means all of the processes ensuring that, at any time in its operating life, the aircraft complies with the airworthiness requirements in force and is in a condition for safe operation;

(e)   “JAA” means “Joint Aviation Authorities”;

(f)   “JAR” means “Joint Aviation Requirements”;

(g)   “large aircraft” means an aircraft, classified as an aeroplane with a maximum take-off mass of more than 5700 kg, or a multi-engined helicopter;

(h)   “maintenance” means any one or combination of overhaul, repair, inspection, replacement, modification or defect rectification of an aircraft or component, with the exception of pre-flight inspection;

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

(j)    “pre-flight inspection” means the inspection carried out before flight to ensure that the aircraft is fit for the intended flight.

(k) “ELA1 aircraft” means the following European Light Aircraft:

(i) an aeroplane, sailplane or powered sailplane with a Maximum Take-off Mass (MTOM) less than 1000 kg that is not classified as complex motor-powered aircraft;

(ii) a balloon with a maximum design lifting gas or hot air volume of not more than 3400 m3 for hot-air balloons, 1050 m3 for gas balloons, 300 m3 for tethered gas balloons;

(iii) an airship designed for not more than two occupants and a maximum design lifting gas or hot-air volume of not more than 2500 m3 for hot-air airships and 1000 m3 for gas airships;

(l)    “LSA aircraft” means a light sport aeroplane which has all of the following characteristics:

(i) a Maximum Take-off Mass (MTOM) of not more than 600 kg;

(ii) a maximum stalling speed in the landing configuration (VS0) of not more than 45 knots Calibrated Airspeed (CAS) at the aircraft’s maximum certificated takeoff mass and most critical centre of gravity;

(iii) a maximum seating capacity of no more than two persons, including the pilot;

(iv) a single, non-turbine engine fitted with a propeller;

(v) a non-pressurised cabin;

(m) “principal place of business” means the head office or the registered office of the undertaking within which the principal financial functions and operational control of the activities referred to in this Regulation are exercised.

Article 3

Continuing airworthiness requirements

1.    The continuing airworthiness of aircraft and components shall be ensured in accordance with the provisions of Annex I.

2.    Organisations and personnel involved in the continuing airworthiness of aircraft and components, including maintenance, shall comply with the provisions of Annex I and where appropriate those specified in Articles 4 and 5.

3.    By derogation from paragraph 1, the continuing airworthiness of aircraft holding a permit to fly shall be ensured on the basis of the specific continuing airworthiness arrangements as defined in the permit to fly issued in accordance with the Annex (Part-21) to Commission Regulation (EC) N°1702/2003.

4.    For aircraft not used in commercial air transport, any airworthiness review certificate or equivalent document issued in accordance with the Member State requirements and valid on 28 September 2008 shall be valid until its expiration date or until 28 September 2009, whichever comes first. After the expiration of its validity, the competent authority may further re-issue or extend one time the airworthiness review certificate or equivalent document for one year, if allowed by the Member State requirements. Upon further expiration, the competent authority may further re-issue or extend one more time the airworthiness review certificate or equivalent document for one year, if allowed by the Member State requirements. No further re-issuance or extension is allowed. If the provisions of this point have been used, when transferring the registration of the aircraft within the EU, a new airworthiness review certificate shall be issued in accordance with M.A.904.

Article 4

Maintenance organisation approvals

1.    Organisations involved in the maintenance of large aircraft or of aircraft used for commercial air transport, and components intended for fitment thereto, shall be approved in accordance with the provisions of Annex II.

2.    Maintenance approvals issued or recognised by a Member State in accordance with the JAA requirements and procedures and valid before the entry into force of this Regulation shall be deemed to have been issued in accordance with this Regulation. For this purpose, by derogation from the provisions of 145.B.50(2) under Annex II, level 2 findings associated with the differences between JAR 145 and Annex II may be closed within one year. Certificates of release to service and authorised release certificates issued by an organisation approved under JAA requirements during that one-year period shall be deemed to have been issued under this Regulation.

3.    Personnel qualified to carry out and/or control a continued airworthiness nondestructive test of aircraft structures and/or components, on the basis of any standard recognised by a Member State prior to the entry into force of this Regulation as providing an equivalent level of qualification, may continue to carry out and/or control such tests.

4.    Certificates of release to service and authorised release certificates issued before the date of entry into force of this Regulation by a maintenance organisation approved under the Member State requirements shall be deemed equivalent to those required under points M.A.801 and M.A.802 of Annex I (Part-M) respectively.

Article 5

Certifying staff

1.    Certifying staff shall be qualified in accordance with the provisions of Annex III, except as provided for in points M.A.606(h), M.A.607(b), M.A.801(d) and M.A.803 of Annex I and in point 145.A.30(j) of Annex II (Part 145) and Appendix IV to Annex II (Part 145).

2.    Any aircraft maintenance licence and if any, the technical limitations associated with that licence, issued or recognised by a Member State in accordance with the JAA requirements and procedures and valid at the time of entry into force of this Regulation, shall be deemed to have been issued in accordance with this Regulation.

Article 6

Training organisation requirements

1.    Organisations involved in the training of personnel referred to in Article 5 shall be approved in accordance with Annex IV to be entitled:

(a) to conduct recognised basic training courses; and/or

(b) to conduct recognised type training courses; and

(c) to conduct examinations; and

(d) to issue training certificates.

2.    Any maintenance training organisation approval issued or recognised by a Member State in accordance with the JAA requirements and procedures and valid at the time of entry into force of this Regulation shall be deemed to have been issued in accordance with this Regulation. For this purpose, by derogation from the provisions of 147.B.130(b) under Annex IV, level 2 findings associated with the differences between JAR 147 and Annex IV may be closed within one year.

Article 7

Entry into force

1.    This Regulation shall enter into force on the day following that of its publication in the Official Journal of the European Union.

2.    By way of derogation from paragraph 1:

(a) the provisions of Annex I, except for points M.A.201(h)(2) and M.A.708(c), shall apply from 28 September 2005;

(b) point M.A.201(f) of Annex I shall apply to aircraft not involved in commercial air transport operated by third country carriers as from 28 September 2009.

3.    By way of derogation from paragraph 1 and 2, Member States may elect not to apply:

(a) the provisions of Annex I to aircraft not involved in commercial air transport, until 28 September 2009;

(b) the provisions of Annex I (I) to aircraft involved in commercial air transport, until 28 September 2008;

(c) the following provisions of Annex II, until 28 September 2006:

- 145.A.30(e), human factors elements,

- 145.A.30(g) as applicable to large aircraft with a maximum take-off mass of more than 5700 kg,

- 145.A.30(h)(1) as applicable to aircraft with a maximum take-off mass of more than 5700 kg,

- 145.A.30(j)(1), Appendix IV,

- 145.A.30(j)(2), Appendix IV;

(d) the following provisions of Annex II, until 28 September 2008:

- 145.A.30(g) as applicable to aircraft with a maximum take-off mass of 5700 kg or below,

- 145.A.30(h)(1) as applicable to aircraft with a maximum take-off mass of 5700 kg or below,

- 145.A.30(h)(2);

(e)   the provisions of Annex III, as applicable to aircraft with a maximum take-off mass above 5700 kg until 28 September 2005;

(f)   the provisions of Annex III, as applicable to aircraft with a maximum take-off mass of 5700 kg or below until 28 September 2006.

(g) for aircraft not involved in commercial air transport other than large aircraft, the need to comply with Annex III (Part 66) in the following provisions, until 28 September 2011:

— M.A.606(g) and M.A.801(b)2 of Annex I (Part-M),

— 145.A.30(g) and (h) of Annex II (Part-145).

4.    Member States may issue approvals with regard to Annex II and Annex IV of a limited duration until 28 September 2007.

5.    When a Member State makes use of the provisions of paragraphs 3 or 4 it shall notify the Commission and the Agency.

6.    The Agency shall make an evaluation of the implication of the provisions of Annex I to this Regulation with a view to submitting an opinion to the Commission, including possible amendments to it, before 28 March 2005.

7.   By way of derogation from paragraph 1:

(a)     the provisions of point M.A.706(k) of Annex I (Part-M) shall apply as from 28 September 2010;

(b)    the provisions of point 7.7 of Appendix I to Annex III (Part-66) shall apply as from 28 September 2010;

(c)     maintenance organisations approved in accordance with Section A of subpart F of Annex I (Part-M) or Section A of Annex II (Part-145) may continue to issue Authorised Release Certificates by using the EASA Form 1 original issue, as laid down in Appendix II to the Annex I (Part-M) as well as Appendix I to the Annex II (Part 145), until 28 September 2010;

(d)    competent authorities may continue to issue certificates, previous issue, as laid down in Appendices III, V and VI to Annex I (Part-M), Appendix III to Annex II (Part-145), Appendix V to Annex III (Part-66) or Appendix II to Annex IV (Part-147) to Regulation (EC) No 2042/2003 in force prior to the entry into force of this regulation, until 28 September 2010;

(e) certificates issued in accordance with Annex I (Part-M), Annex II (Part-145), Annex III (Part-66) or Annex IV (Part-147) prior to the entry into force of this regulation remain valid until they are changed or revoked.

This Regulation shall be binding in its entirety and directly applicable in all Member States.

Done at Brussels, 20 November 2003

For the Commission

Loyola de PALACIO

Vice-President


ANNEX I (Part-M)

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