Commission Delegated Regulation (EU) 2021/699 of 21 December 2020 amending and correcting Regulation (EU) No 748/2012 as regards the instructions for continued airworthiness, the production of parts to be used during maintenance and the consideration of ageing aircraft aspects during certification

Delegated Regulation (EU) 2021/699 · Regulation · 5 articles

Data as of 2026-07-04 · Compiled from an official source version. Later amendments or repeals may not be reflected; the official text prevails. · Read the official text ↗

Article 1

Regulation (EU) No 748/2012 is amended as follows: (1) in Article 9, paragraph 1 is replaced by the following: ‘1. An organisation responsible for the manufacture of products, parts and appliances shall demonstrate its capability in accordance with the provisions of Annex I (Part 21). This demonstration of capability is not required for the parts or appliances that an organisation manufactures which, in accordance with the provisions of Annex I (Part 21), are eligible for installation in a type-certified product without the need to be accompanied by an authorised release certificate (i.e. EASA Form 1).’; (2) Annex I is amended in accordance with Annex I to this Regulation.

Article 2

Annex I to Regulation (EU) No 748/2012 is corrected in accordance with Annex II to this Regulation.

Article 3

This Regulation shall enter into force on the twentieth day following that of its publication in the Official Journal of the European Union . This Regulation shall apply from 18 May 2022, with the exception of Article 2 and point 4, point 6, point 9 and point 15 of Annex I which shall apply from 18 May 2021.

Supplementary provisions

ANNEX ISupplementary provisions

ANNEX I Annex I (Part 21) to Regulation (EU) No 748/2012 is amended as follows: (1) the table of contents is replaced by the following: ‘ Contents 21.1 General SECTION A – TECHNICAL REQUIREMENTS SUBPART A – GENERAL PROVISIONS 21.A.1 Scope 21.A.2 Undertaking by another person than the applicant for, or holder of, a certificate 21.A.3A Failures, malfunctions and defects 21.A.3B Airworthiness directives 21.A.4 Coordination between design and production 21.A.5 Record-keeping 21.A.6 Manuals 21.A.7 Instructions for continued airworthiness SUBPART B – TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES 21.A.11 Scope 21.A.13 Eligibility 21.A.14 Demonstration of capability 21.A.15 Application 21.A.19 Changes requiring a new type-certificate 21.A.20 Demonstration of compliance with the type-certification basis, operational suitability data certification basis and environmental protection requirements 21.A.21 Requirements for the issuance of a type-certificate or restricted type-certificate 21.A.31 Type design 21.A.33 Inspections and tests 21.A.35 Flight tests 21.A.41 Type-certificate 21.A.44 Obligations of the holder 21.A.47 Transferability 21.A.51 Duration and continued validity 21.A.62 Availability of operational suitability data 21.A.65 Continuing structural integrity for aeroplanes structures (SUBPART C – NOT APPLICABLE) SUBPART D – CHANGES TO TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES 21.A.90A Scope 21.A.90B Standard changes 21.A.90C Stand-alone changes to the Instructions for Continued Airworthiness 21.A.91 Classification of changes to a type-certificate 21.A.92 Eligibility 21.A.93 Application 21.A.95 Requirements for approval of a minor change 21.A.97 Requirements for approval of a major change 21.A.101 Type-certification basis, operational suitability data certification basis and environmental protection requirements for a major change to a type-certificate 21.A.108 Availability of operational suitability data 21.A.109 Obligations and EPA marking SUBPART E – SUPPLEMENTAL TYPE-CERTIFICATES 21.A.111 Scope 21.A.112A Eligibility 21.A.112B Demonstration of capability 21.A.113 Application for a supplemental type-certificate 21.A.115 Requirements for approval of major changes in the form of a supplemental type-certificate 21.A.116 Transferability 21.A.117 Changes to that part of a product covered by a supplemental type-certificate 21.A.118A Obligations and EPA marking 21.A.118B Duration and continued validity 21.A.120B Availability of operational suitability data SUBPART F – PRODUCTION WITHOUT PRODUCTION ORGANISATION APPROVAL 21.A.121 Scope 21.A.122 Eligibility 21.A.124 Application 21.A.125A Issue of a letter of agreement 21.A.125B Findings 21.A.125C Duration and continued validity 21.A.126 Production inspection system 21.A.127 Tests: aircraft 21.A.128 Tests: engines and propellers 21.A.129 Obligations of the manufacturer 21.A.130 Statement of conformity SUBPART G – PRODUCTION ORGANISATION APPROVAL 21.A.131 Scope 21.A.133 Eligibility 21.A.134 Application 21.A.135 Issue of production organisation approval 21.A.139 Quality System 21.A.143 Exposition 21.A.145 Approval requirements 21.A.147 Changes to the approved production organisation 21.A.148 Changes of location 21.A.149 Transferability 21.A.151 Terms of approval 21.A.153 Changes to the terms of approval 21.A.157 Investigations 21.A.158 Findings 21.A.159 Duration and continued validity 21.A.163 Privileges 21.A.165 Obligations of the holder SUBPART H – CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS 21.A.171 Scope 21.A.172 Eligibility 21.A.173 Classification 21.A.174 Application 21.A.175 Language 21.A.177 Amendment or modification 21.A.179 Transferability and reissuance within Member States 21.A.180 Inspections 21.A.181 Duration and continued validity 21.A.182 Aircraft identification SUBPART I – NOISE CERTIFICATES 21.A.201 Scope 21.A.203 Eligibility 21.A.204 Application 21.A.207 Amendment or modification 21.A.209 Transferability and reissuance within Member States 21.A.210 Inspections 21.A.211 Duration and continued validity SUBPART J – DESIGN ORGANISATION APPROVAL 21.A.231 Scope 21.A.233 Eligibility 21.A.234 Application 21.A.235 Issue of design organisation approval 21.A.239 Design assurance system 21.A.243 Data 21.A.245 Approval requirements 21.A.247 Changes in design assurance system 21.A.249 Transferability 21.A.251 Terms of approval 21.A.253 Changes to the terms of approval 21.A.257 Investigations 21.A.258 Findings 21.A.259 Duration and continued validity 21.A.263 Privileges 21.A.265 Obligations of the holder SUBPART K – PARTS AND APPLIANCES 21.A.301 Scope 21.A.303 Compliance with applicable requirements 21.A.305 Approval of parts and appliances 21.A.307 The eligibility of parts and appliances for installation (SUBPART L – NOT APPLICABLE) SUBPART M – REPAIRS 21.A.431A Scope 21.A.431B Standard repairs 21.A.432A Eligibility 21.A.432B Demonstration of capability 21.A.432C Application for a repair design approval 21.A.433 Requirements for approval of a repair design 21.A.435 Classification and approval of repair designs 21.A.439 Production of repair parts 21.A.441 Repair embodiment 21.A.443 Limitations 21.A.445 Unrepaired damage 21.A.451 Obligations and EPA marking (SUBPART N – NOT APPLICABLE) SUBPART O – EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS 21.A.601 Scope 21.A.602A Eligibility 21.A.602B Demonstration of capability 21.A.603 Application 21.A.604 ETSO authorisation for an auxiliary power unit (APU) 21.A.605 Data requirements 21.A.606 Requirements for issuance of an ETSO authorisation 21.A.607 ETSO authorisation privileges 21.A.608 Declaration of design and performance (DDP) 21.A.609 Obligations of holders of ETSO authorisations 21.A.610 Approval for deviation 21.A.611 Design changes 21.A.615 Inspection by the Agency 21.A.619 Duration and continued validity 21.A.621 Transferability SUBPART P – PERMIT TO FLY 21.A.701 Scope 21.A.703 Eligibility 21.A.705 Competent authority 21.A.707 Application for permit to fly 21.A.708 Flight conditions 21.A.709 Application for approval of flight conditions 21.A.710 Approval of flight conditions 21.A.711 Issue of a permit to fly 21.A.713 Changes 21.A.715 Language 21.A.719 Transferability 21.A.721 Inspections 21.A.723 Duration and continued validity 21.A.725 Renewal of permit to fly 21.A.727 Obligations of the holder of a permit to fly 21.A.729 Record-keeping SUBPART Q – IDENTIFICATION OF PRODUCTS, PARTS AND APPLIANCES 21.A.801 Identification of products 21.A.803 Handling of identification data 21.A.804 Identification of parts and appliances 21.A.805 Identification of critical parts 21.A.807 Identification of ETSO articles SECTION B – PROCEDURES FOR COMPETENT AUTHORITIES SUBPART A – GENERAL PROVISIONS 21.B.5 Scope 21.B.20 Obligations of the competent authority 21.B.25 Requirements for the organisation of the competent authority 21.B.30 Documented procedures 21.B.35 Changes in organisation and procedures 21.B.40 Resolution of disputes 21.B.45 Reporting/coordination 21.B.55 Record-keeping 21.B.60 Airworthiness directives SUBPART B – TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES 21.B.70 Certification specifications 21.B.75 Special conditions 21.B.80 Type-certification basis for a type-certificate or restricted type-certificate 21.B.82 Operational suitability data certification basis for an aircraft type certificate or restricted type-certificate 21.B.85 Designation of applicable environmental protection requirements and certification specifications for a type-certificate or restricted type-certificate 21.B.100 Level of involvement 21.B.103 Issuance of a type-certificate or restricted type-certificate (SUBPART C – NOT APPLICABLE) SUBPART D – CHANGES TO TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES 21.B.105 Type-certification basis, environmental protection requirements and operational suitability data certification basis for a major change to a type-certificate 21.B.107 Issuance of an approval of a change to a type-certificate SUBPART E – SUPPLEMENTAL TYPE-CERTIFICATES 21.B.109 Type-certification basis, environmental protection requirements and operational suitability data certification basis for a supplemental type-certificate 21.B.111 Issuance of a supplemental type-certificate SUBPART F – PRODUCTION WITHOUT PRODUCTION ORGANISATION APPROVAL 21.B.120 Investigation 21.B.125 Findings 21.B.130 Issue of letter of agreement 21.B.135 Maintenance of the letter of agreement 21.B.140 Amendment of a letter of agreement 21.B.145 Limitation, suspension and revocation of a letter of agreement 21.B.150 Record-keeping SUBPART G – PRODUCTION ORGANISATION APPROVAL 21.B.220 Investigation 21.B.225 Findings 21.B.230 Issue of certificate 21.B.235 Continued surveillance 21.B.240 Amendment of a production organisation approval 21.B.245 Suspension and revocation of a production organisation approval 21.B.260 Record-keeping SUBPART H – CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS 21.B.320 Investigation 21.B.325 Issue of airworthiness certificate 21.B.326 Certificate of airworthiness 21.B.327 Restricted certificate of airworthiness 21.B.330 Suspension and revocation of certificates of airworthiness and restricted certificates of airworthiness 21.B.345 Record-keeping SUBPART I – NOISE CERTIFICATES 21.B.420 Investigation 21.B.425 Issue of noise certificates 21.B.430 Suspension and revocation of a noise certificate 21.B.445 Record-keeping SUBPART J – DESIGN ORGANISATION APPROVAL SUBPART K – PARTS AND APPLIANCES (SUBPART L – NOT APPLICABLE) SUBPART M – REPAIRS 21.B.450 Type-certification basis and environmental protection requirements for a major repair design approval 21.B.453 Issuance of a repair design approval (SUBPART N – NOT APPLICABLE) SUBPART O – EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS 21.B.480 Issuance of an ETSO authorisation SUBPART P – PERMIT TO FLY 21.B.520 Investigation 21.B.525 Issue of permits to fly 21.B.530 Revocation of permits to fly 21.B.545 Record-keeping 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 (a) The holder of a type-certificate, restricted type-certificate, supplemental type-certificate, design change or repair design approval shall develop or reference the instructions which are necessary for ensuring that the airworthiness standard related to the aircraft type and any associated part is maintained throughout the operational life of the aircraft, when demonstrating compliance with the applicable type-certification basis established and notified by the Agency in accordance with point 21.B.80. (b) At least one set of complete instructions for continued airworthiness shall be provided by the holder of: 1. a type-certificate or restricted type-certificate to each known owner of one or more products upon its delivery or upon the issuance of the first certificate of airworthiness or restricted certificate of airworthiness for the affected aircraft, whichever occurs later, 2. a supplemental type-certificate or design change approval to all known operators of the product affected by the change upon the release to service of the modified product, 3. a repair design approval to all known operators of the product affected by the repair upon the release to service of the product in which the repair design is embodied. The repaired product, part or appliance may be released into service before the related instructions for continued airworthiness have been completed, but this shall be for a limited service period, and in agreement with the Agency. Thereafter, those design approval holders shall make those instructions available on request to any other person required to comply with those instructions. (c) By way of derogation from point (b), the type-certificate holder or restricted type-certificate holder may delay the availability of a part of the instructions for continued airworthiness, dealing with long lead accomplishment instructions of a scheduled nature, until after the product or modified product has entered into service, but shall make those instructions available before the use of this data is required for the product or modified product. (d) The design approval holder, who is required to provide instructions for continued airworthiness in accordance with point (b), shall also make available changes to those instructions to all known operators of the product affected by the change and, on request, to any other person required to comply with those changes. That design approval holder shall demonstrate to the Agency, on request, the adequacy of the process of making changes to the instructions for continued airworthiness available in accordance with this point.’; (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 CO 2 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: (a) undertake the obligations laid down in points 21.A.3A, 21.A.3B, 21.A.4, 21.A.55, 21.A.57, 21.A.61, 21.A.62 and 21.A.65; and, for this purpose, shall continue to meet the qualification requirements for eligibility under point 21.A.14; and (b) specify the marking in accordance with Subpart Q.’; 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: ‘2. that follow design data included in the certification specifications issued by the Agency, containing acceptable methods, techniques and practices for carrying out and identifying standard changes, including the associated instructions for continued airworthiness; and’; (8) the following point 21.A.90C is inserted: ‘21.A.90C Stand-alone changes to the Instructions for Continued Airworthiness (a) Stand-alone changes to the instructions for continued airworthiness are changes that are not directly prepared as a result of a change to the type design or repair design. (b) Stand-alone changes to the instructions for continued airworthiness can only be made by the holder of the design approval for which those instructions have been established. (c) Points 21.A.91 to 21.A.109 shall not apply to stand-alone changes to the instructions for continued airworthiness that: 1. do not affect the airworthiness limitations section of the instructions for continued airworthiness, and 2. do not require the design approval holder to perform any additional demonstration of compliance with the certification basis. (d) Stand-alone changes to the instructions for continued airworthiness referred to in point (c) shall be approved by the design approval holder under procedures agreed with the Agency.’; (9) point 21.A.101 is amended as follows: (a) the first paragraph of point (b) is replaced by the following: ‘(b) Except as provided in point (h), by derogation from point (a), an earlier amendment to a certification specification referred to in point (a) and to any other certification specification which is directly related may be used in any of the following situations, unless the earlier amendment became applicable before the date at which the corresponding certification specifications incorporated by reference in the type-certificate became applicable:’; (b) the following point (h) is added: ‘(h) For large aeroplanes subject to point 26.300 of Annex I to Regulation (EU) 2015/640 ( *1 ) , the applicant shall comply with certification specifications that provide at least an equivalent level of safety to points 26.300, 26.320 and 26.330 of Annex I to Regulation (EU) 2015/640, except for applicants for supplemental type-certificates who are not required to take into account point 26.303. ( *1 ) Commission Regulation (EU) 2015/640 of 23 April 2015 on additional airworthines specifications for a given type of operationss and amending Regulation (EU) No 965/2012 ( OJ L 106, 24.4.2015, p. 18 )’." (10) points 21.A.105 and 21.A.107 are deleted; (11) in point 21.A.109, point (a) is replaced by the following: ‘(a) undertake the obligations laid down in points 21.A.4, 21.A.5, 21.A.7 and 21.A.108; and’; (12) in point 21.A.118A, point (a)(1) is replaced by the following: ‘1. laid down in points 21.A.3A, 21.A.3B, 21.A.4, 21.A.5, 21.A.6, 21.A.7, and 21.A.120B;’; (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 (a) A part or appliance is eligible for installation in a type-certified product when it is in a condition for safe operation, marked in accordance with Subpart Q and accompanied by an authorised release certificate (EASA Form 1), certifying that the item was manufactured in conformity with approved design data. (b) By way of derogation from point (a) and provided that the conditions in point (c) are met, the following parts or appliances do not require an EASA Form 1 in order to be eligible for installation in a type-certified product: (1) a standard part; (2) in the case of ELA1 or ELA2, a part or appliance that is: (i) not life limited, nor part of the primary structure, nor part of the flight controls; (ii) identified for installation in the specific aircraft; (iii) to be installed in an aircraft whose owner has verified compliance with the applicable conditions in (i) and (ii), and has accepted responsibility for this compliance; (3) a part or appliance for which the consequences of a non-conformity with its approved design data has a negligible safety effect on the product and which is identified as such by the holder of the design approval in the instructions for continued airworthiness. In order to determine the safety effects of a non-conforming part or appliance, the design approval holder may establish in the instructions for continued airworthiness specific verification activities to be conducted by the installer of the part or appliance on the product; (4) in the case of the embodiment of a standard change in accordance with point 21.A.90B or a standard repair in accordance with point 21.A.431B, a part or appliance, for which the consequences of a non-conformity with its design data have a negligible safety effect on the product, and which is identified as such in the certification specifications for standard changes and standard repairs issued in accordance with point (a)(2) of point 21.A.90B and point (a)(2) of point 21.A.431B. In order to determine the safety effects of a non-conforming part or appliance, specific verification activities to be conducted by the person that installs the part or appliance on the product may be established in the certification specifications referred to above; (5) a part or appliance that is exempted from an airworthiness approval in accordance with Commission Regulation (EU) No 965/2012 ( *2 ) ; and (6) a part or appliance that is an item of a higher assembly identified in points (b)(1) to (b)(5). (c) Parts and appliances listed in point (b) are eligible for installation in a type-certified product without being accompanied by an EASA Form 1, provided that the installer holds a document issued by the person or organisation that manufactured the part or appliance, which declares the name of the part or appliance, the part number, and the conformity of the part or appliance with its design data, and which contains the issuance date. ( *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: (a) point (3) is replaced by the following: ‘3. when no feature or characteristic has been identified that may make the product unsafe for the uses for which certification is requested;’; (b) the following point (5) is added: ‘5. when, for a repair to an aeroplane subject to point 26.302 of Annex I to Regulation (EU) 2015/640, it has been demonstrated that the structural integrity of the repair and affected structure is at least equivalent to the level of structural integrity established for the baseline structure by point 26.302 of Annex I to Regulation (EU) 2015/640.’; (16) points 21.A.447 and 21.A.449 are deleted; (17) point 21.A.451 is amended as follows: (a) point (a)(1)(i) is replaced by the following: ‘(i) laid down in points 21.A.3A, 21.A.3B, 21.A.4, 21.A.5, 21.A.7, 21.A.439, 21.A.441, and 21.A.443;’; (b) point (b)(1) is replaced by the following: ‘1. undertake the obligations laid down in points 21.A.4, 21.A.5 and 21.A.7; and’; (18) in point 21.A.609, point (b) is replaced by the following: ‘(b) prepare and maintain, for each model of each article for which an ETSO authorisation has been issued, a current file of complete technical data and records in accordance with point 21.A.5;’; (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 (a) Each part or appliance which is eligible for installation in a type-certified product shall be marked permanently and legibly with: 1. a name, trademark, or symbol identifying the manufacturer in a manner identified by the applicable design data; 2. the part number, as defined in the applicable design data; and 3. the letters EPA for parts or appliances produced in accordance with approved design data not belonging to the type-certificate holder of the related product, except for ETSO articles and for parts and appliances covered under point (b) of point 21.A.307. (b) By way of derogation from point (a), if the Agency agrees that a part or appliance is too small or that it is otherwise impractical to mark a part or appliance with any of the information required by point (a), the authorised release document accompanying the part or appliance or its container shall include the information that could not be marked on the part or appliance.’; ( *1 ) Commission Regulation (EU) 2015/640 of 23 April 2015 on additional airworthines specifications for a given type of operationss and amending Regulation (EU) No 965/2012 ( OJ L 106, 24.4.2015, p. 18 )’. ( *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 ).’.’

ANNEX IISupplementary provisions

ANNEX II Annex I (Part 21) to Regulation (EU) No 748/2012 is corrected as follows: (1) point 21.A.15 is corrected as follows: (a) the first paragraph of point (b) is replaced by the following: ‘(b) An application for a type-certificate or restricted type-certificate shall include, as a minimum, preliminary descriptive data of the product, the intended use of the product and the kind of operations for which certification is requested. In addition, it shall include, or be supplemented after the initial application by, a certification programme for the demonstration of compliance in accordance with point 21.A.20, consisting of:’; (b) point (d) is replaced by the following: ‘(d) An application for a type-certificate or restricted type-certificate for an aircraft shall include, or be supplemented after the initial application by, an application supplement for approval of the operational suitability data.’; (2) point 21.A.93 is corrected as follows: (a) the first paragraph of point (b) is replaced by the following: ‘(b) An application shall include, or be supplemented after the initial application by, a certification programme for the demonstration of compliance in accordance with point 21.A.20, consisting of:’; (b) point (2) of point (c) is replaced by the following: ‘2. apply for an extension of the time period provided for in the first sentence of point (c) for the original application and propose a new date for the issuance of the approval. In that case, the applicant shall comply with the type-certification basis, operational suitability data certification basis and environmental protection requirements, as established by the Agency in accordance with point 21.A.101 and notified in accordance with point 21.B.105, for a date to be selected by the applicant. However, that date shall not precede the new date proposed by the applicant for the issuance of the approval by more than five years for an application for a change to type-certificate or restricted type-certificate for a large aeroplane or a large rotorcraft, and by more than three years for an application for a change to any other type-certificate or restricted type certificate.’; (3) in point 21.A.174, point (ii) of point (b)(3) is replaced by the following: ‘(ii) a non-member State: — a statement by the competent authority of the State where the aircraft is, or was, registered, reflecting the airworthiness status of the aircraft on its register at the time of transfer; — a weight and balance report with a loading schedule; — the flight manual when such a manual is required by the airworthiness code for the aircraft; — historical records to establish the production, modification and maintenance standard of the aircraft, including all limitations associated with a restricted certificate of airworthiness issued in accordance with point 21.B.327; — a recommendation for the issuance of a certificate of airworthiness or restricted certificate of airworthiness and for an airworthiness review certificate pursuant to an airworthiness review in accordance with Annex I (Part-M) to Regulation (EU) No 1321/2014 ( *1 ) or an airworthiness review certificate in accordance with Annex Vb (Part-ML) to Regulation (EU) No 1321/2014. — the date on which the first certificate of airworthiness was issued and, if the standards of Volume III of Annex 16 to the Chicago Convetnion apply, the CO 2 metric value data.; ( *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: ‘1. compliance with the applicable type-design and continued airworthiness requirements; and’; (5) in point 21.A.211, point (1) of point (a) is replaced by the following: ‘1. compliance with the applicable type-design, environmental protection and continued airworthiness requirements; and’; (6) in point 21.A.431B, point (2) of point (a) is replaced by the following: ‘(2) that follow design data included in certification specifications issued by the Agency, containing acceptable methods, techniques and practices for carrying out and identifying standard repairs, including the associated instructions for continued airworthiness; and’; (7) in point 21.A.432C, the first paragraph of point (b) is replaced by the following: ‘(b) An application for a major repair design approval shall include, or be supplemented after the initial application by, a certification programme containing:’; (8) in point 21.A.711, point (d) is replaced by the following: ‘(d) An approved organisation may issue a permit to fly (EASA Form 20b, see Appendix IV) under the privilege granted in accordance with point M.A.711 of Annex I (Part-M) of Regulation (EU) No 1321/2014 or point CAMO.A.125 of Annex Vc (Part-CAMO) of Regulation (EU) No 1321/2014 or point CAO.A.095 of Annex Vd (Part-CAO) of Regulation (EU) No 1321/2014, when the flight conditions referred to in point 21.A.708 of this Annex have been approved in accordance with point 21.A.710 of this Annex;’; (9) in point 21.B.325, point (c) is replaced by the following: ‘(c) For aircraft originating from a non-member State, in addition to the appropriate airworthiness certificate referred to in point (a) or (b), the competent authority of the Member State of registry shall issue: 1. for new or used aircraft subject to Annex I (Part-M) to Commission Regulation (EU) No 1321/2014, an initial airworthiness review certificate (EASA Form 15a, Appendix II); 2. for new aircraft subject to Annex Vb (Part-ML) to Commission Regulation (EU) No 1321/2014, an initial airworthiness review certificate (EASA Form 15c, Appendix II); 3. for used aircraft subject to Annex Vb (Part-ML) to Commission Regulation (EU) No 1321/2014, an initial airworthiness review certificate (EASA Form 15c, Appendix II), when the competent authority has performed the airworthiness review.’ (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. AIRWORTHINESS REVIEW CERTIFICATE (ARC) (for aircraft complying with Part-ML) ARC reference: ……….. Pursuant to Regulation (EU) 2018/1139 of the European Parliament and of the Council: [NAME OF THE COMPETENT AUTHORITY] (**) hereby certifies that: ☐…..it has performed an airworthiness review in accordance with Regulation (EU) No 1321/2014 on the following aircraft: [or] ☐.….the following new aircraft: Aircraft manufacturer:………………………………….Manufacturer’s designation:…………………………… Aircraft registration:……………………………………Aircraft serial number:…………………………………. (and that this aircraft) is considered airworthy at the time of the review. Date of issue: ..................................................................Date of expiry: ………………………………………….. Airframe flight hours (FH) at date of review (*): ……………………………………………………………….. Signed: ............................................................................Authorisation No (if applicable): ………………………. [OR] [NAME OF APPROVED ORGANISATION, ADDRESS and APPROVAL REFERENCE] (**) [or] [FULL NAME OF THE CERTIFYING STAFF AND PART-66 LICENCE NUMBER (OR NATIONAL EQUIVALENT)] (**) hereby certifies that it has performed an airworthiness review in accordance with Regulation (EU) No 1321/2014 on the following aircraft: Aircraft manufacturer:………………………………….Manufacturer’s designation:…………………………… Aircraft registration:……………………………………Aircraft serial number:…………………………………. and that this aircraft is considered airworthy at the time of the review. Date of issue: ..................................................................Date of expiry: ………………………………………….. Airframe flight hours (FH) at date of review (*): ……………………………………………………………….. Signed: ............................................................................Authorisation No (if applicable): ………………………. =================================================================================== 1st extension: The aircraft complies with the conditions of ML.A.901(c) of Annex Vb (Part-ML) Date of issue: ..................................................................Date of expiry: ………………………………………….. Airframe flight hours (FH) at date of issue (*): …………………………………………………… ……………… Signed: ............................................................................Authorisation No: ……………………… Company name: .............................................................Approval reference: ……………………………………... =================================================================================== 2nd extension: The aircraft complies with the conditions of ML.A.901(c) of Annex Vb (Part-ML) Date of issue: ..................................................................Date of expiry: ………………………………………….. Airframe flight hours (FH) at date of issue (*): …………………………………………………… ……………… Signed: ............................................................................Authorisation No: ……………………… Company name: .............................................................Approval reference: ……………………………………... (*) Except for balloons and airships (**) The issuer of the Form can tailor it to his need by deleting the name, the certifying statement, the reference to the subject aircraft and the issuance details that are not relevant for his use. EASA Form 15c, Issue 4’. ( *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 ).’;’

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Source: EUR-Lex (Publications Office of the EU), © European Union, reuse permitted under Commission Decision 2011/833/EU.

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