(1)

in Article 9, paragraph 1 is replaced by the following:

(2)

Annex I is amended in accordance with Annex I to this Regulation.

(1)

the table of contents is replaced by the following:

‘Contents

SECTION A – TECHNICAL REQUIREMENTS

SUBPART A – GENERAL PROVISIONS

SUBPART B – TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES

(SUBPART C – NOT APPLICABLE)

SUBPART D – CHANGES TO TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES

SUBPART E – SUPPLEMENTAL TYPE-CERTIFICATES

SUBPART F – PRODUCTION WITHOUT PRODUCTION ORGANISATION APPROVAL

SUBPART G – PRODUCTION ORGANISATION APPROVAL

SUBPART H – CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS

SUBPART I – NOISE CERTIFICATES

SUBPART J – DESIGN ORGANISATION APPROVAL

SUBPART K – PARTS AND APPLIANCES

(SUBPART L – NOT APPLICABLE)

SUBPART M – REPAIRS

(SUBPART N – NOT APPLICABLE)

SUBPART O – EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS

SUBPART P – PERMIT TO FLY

SUBPART Q – IDENTIFICATION OF PRODUCTS, PARTS AND APPLIANCES

SECTION B – PROCEDURES FOR COMPETENT AUTHORITIES

SUBPART A – GENERAL PROVISIONS

SUBPART B – TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES

(SUBPART C – NOT APPLICABLE)

SUBPART D – CHANGES TO TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES

SUBPART E – SUPPLEMENTAL TYPE-CERTIFICATES

SUBPART F – PRODUCTION WITHOUT PRODUCTION ORGANISATION APPROVAL

SUBPART G – PRODUCTION ORGANISATION APPROVAL

SUBPART H – CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS

SUBPART I – NOISE CERTIFICATES

SUBPART J – DESIGN ORGANISATION APPROVAL

SUBPART K – PARTS AND APPLIANCES

(SUBPART L – NOT APPLICABLE)

SUBPART M – REPAIRS

(SUBPART N – NOT APPLICABLE)

SUBPART O – EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS

SUBPART P – PERMIT TO FLY

SUBPART Q – IDENTIFICATION OF PRODUCTS, PARTS AND APPLIANCES

Appendices

Appendix I – EASA Form 1 – Authorised Release Certificate;

Appendix II – EASA Forms 15 – Airworthiness Review Certificate;

Appendix III – EASA Form 20a – Permit to Fly;

Appendix IV – EASA Form 20b – Permit to Fly (issued by approved organisations);

Appendix V – EASA Form 24 – Restricted Certificate of Airworthiness;

Appendix VI – EASA Form 25 – Certificate of Airworthiness;

Appendix VII – EASA Form 45 – Noise Certificate;

Appendix VIII – EASA Form 52 – Aircraft Statement of Conformity;

Appendix IX – EASA Form 53 – Certificate of Release to Service;

Appendix X – EASA Form 55 – Production Organisation Approval Certificate;

Appendix XI – EASA Form 65 – Letter of Agreement for production without production organisation approval;

Appendix XII – Categories of flight tests and associated flight test crew qualification 85.’;

(2)

the following points 21.A.5, 21.A.6 and 21.A.7 are inserted:

‘21.A.5   Record-keeping

All relevant design information, drawings and test reports, including inspection records for the product or article tested for the purpose of certification, shall be held by the holder of a type-certificate, restricted type-certificate, supplemental type-certificate, design change or repair design approval or of an ETSO authorisation at the disposal of the Agency and shall be retained in order to provide the information necessary to ensure the continued airworthiness, continued validity of the operational suitability data and the compliance with the applicable environmental protection requirements of the product or the article.

21.A.6   Manuals

The holder of a type-certificate, restricted type-certificate, or supplemental type-certificate shall produce, maintain and update master copies of all manuals or variations in the manuals required by the applicable type-certification basis, the applicable operational suitability data certification basis and the environmental protection requirements for the product or article, and provide copies, on request, to the Agency.

21.A.7   Instructions for continued airworthiness

(3)

point 21.A.41 is replaced by the following:

‘21.A.41   Type-certificate

The type-certificate and restricted type-certificate shall include the type design, the operating limitations, the instructions for continued airworthiness, the type-certificate data sheet for airworthiness and emissions, the applicable type-certification basis and environmental protection requirements with which the Agency records compliance, and any other conditions or limitations prescribed for the product in the applicable certification specifications and environmental protection requirements. The aircraft type-certificate and restricted type-certificate shall include in addition the applicable operational suitability data certification basis, the operational suitability data and the type-certificate data sheet for noise. The aircraft type-certificate and restricted type-certificate data sheet shall include the record of CO2 emissions compliance and the engine type-certificate data sheet shall include the record of exhaust emissions compliance.’;

(4)

point 21.A.44 is replaced by the following:

‘21.A.44   Obligations of the holder

Each holder of a type-certificate or restricted type-certificate shall:

As from 18 May 2022, the obligation to comply with the obligations listed under point (a) shall be understood as referring to points 21.A.3A, 21.A.3B, 21.A.4, 21.A.5, 21.A.6, 21.A.7, 21.A.62 and 21.A.65; and, for this purpose, each holder of a type-certificate or restricted type-certificate shall continue to meet the qualification requirements for eligibility under point 21.A.14.

(5)

points 21.A.55, 21.A.57 and 21.A.61 are deleted;

(6)

the following point 21.A.65 is inserted:

‘21.A.65   Continuing structural integrity for aeroplanes structures

The holder of the type-certificate or restricted type-certificate for a large aeroplane shall ensure that the continuing structural integrity programme remains valid throughout the operational life of the aeroplane, taking into account service experience and current operations’;

(7)

in point 21.A.90B(a), point 2 is replaced by the following:

(8)

the following point 21.A.90C is inserted:

‘21.A.90C   Stand-alone changes to the Instructions for Continued Airworthiness

(9)

point 21.A.101 is amended as follows:

(10)

points 21.A.105 and 21.A.107 are deleted;

(11)

in point 21.A.109, point (a) is replaced by the following:

(12)

in point 21.A.118A, point (a)(1) is replaced by the following:

(13)

points 21.A.119 and 21.A.120A are deleted;

(14)

point 21.A.307 is replaced by the following:

‘21.A.307   The eligibility of parts and appliances for installation

(*2)  Commission Regulation (EU) No 379/2014 of 7 April 2014 amending Commission Regulation (EU) No 965/2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No 216/2008 of the European Parliament and of the Council (OJ L 123, 24.4.2014, p. 1).’."

(15)

in point 21.A.433, point (a) is amended as follows:

(16)

points 21.A.447 and 21.A.449 are deleted;

(17)

point 21.A.451 is amended as follows:

(18)

in point 21.A.609, point (b) is replaced by the following:

(19)

point 21.A.613 is deleted;

(20)

point 21.A.804 is replaced by the following:

‘21.A.804 Identification of parts and appliances

(1)

point 21.A.15 is corrected as follows:

(2)

point 21.A.93 is corrected as follows:

(3)

in point 21.A.174, point (ii) of point (b)(3) is replaced by the following:

(*1)  Commission Regulation (EU) No 1321/2014 of 26 November 2014 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks (OJ L 362, 17.12.2014, p. 1).’;"

(4)

in point 21.A.181, point (1) of point (a) is replaced by the following:

(5)

in point 21.A.211, point (1) of point (a) is replaced by the following:

(6)

in point 21.A.431B, point (2) of point (a) is replaced by the following:

(7)

in point 21.A.432C, the first paragraph of point (b) is replaced by the following:

(8)

in point 21.A.711, point (d) is replaced by the following:

(9)

in point 21.B.325, point (c) is replaced by the following:

(10)

in Appendix II, EASA 15c – Airworthiness review certificate is replaced by the following:

‘Airworthiness Review Certificate – EASA Form 15c

NOTE: persons and organisations performing the airworthiness review in combination with the 100-h/annual inspection may use the reverse side of this form in order to issue the CRS referred to in point ML.A.801 corresponding to the 100-h/annual inspection.

EASA Form 15c, Issue 4’.