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Document 32022R1358
Commission Delegated Regulation (EU) 2022/1358 of 2 June 2022 amending Regulation (EU) No 748/2012 as regards the implementation of more proportionate requirements for aircraft used for sport and recreational aviation
Commission Delegated Regulation (EU) 2022/1358 of 2 June 2022 amending Regulation (EU) No 748/2012 as regards the implementation of more proportionate requirements for aircraft used for sport and recreational aviation
Commission Delegated Regulation (EU) 2022/1358 of 2 June 2022 amending Regulation (EU) No 748/2012 as regards the implementation of more proportionate requirements for aircraft used for sport and recreational aviation
C/2022/3234
OJ L 205, 5.8.2022, p. 7–98
(BG, ES, CS, DA, DE, ET, EL, EN, FR, GA, HR, IT, LV, LT, HU, MT, NL, PL, PT, RO, SK, SL, FI, SV)
In force
5.8.2022 |
EN |
Official Journal of the European Union |
L 205/7 |
COMMISSION DELEGATED REGULATION (EU) 2022/1358
of 2 June 2022
amending Regulation (EU) No 748/2012 as regards the implementation of more proportionate requirements for aircraft used for sport and recreational aviation
THE EUROPEAN COMMISSION,
Having regard to the Treaty on the Functioning of the European Union,
Having regard to Regulation (EU) 2018/1139 of the European Parliament and of the Council of 4 July 2018 on common rules in the field of civil aviation and establishing a European Union Aviation Safety Agency, and amending Regulations (EC) No 2111/2005, (EC) No 1008/2008, (EU) No 996/2010, (EU) No 376/2014 and Directives 2014/30/EU and 2014/53/EU of the European Parliament and of the Council, and repealing Regulations (EC) No 552/2004 and (EC) No 216/2008 of the European Parliament and of the Council and Council Regulation (EEC) No 3922/91 (1), and in particular Articles 19(1) and 62(13) thereof,
Whereas:
(1) |
Commission Regulation (EU) No 748/2012 (2) lays down the requirements for the airworthiness and environmental certification of products, parts and appliances of civil aircraft, such as engines, propellers and parts to be installed therein. |
(2) |
Pursuant to Article 140(3) of Regulation (EU) 2018/1139, sport and recreational aviation is to be subject to simple and proportionate rules to avoid putting unnecessary administrative and financial burdens for the organisations involved in the design and production of such aircraft. Those rules are to be proportionate, cost-effective and flexible, while ensuring the necessary level of safety. |
(3) |
Organisations involved in the design and production of certain categories of products used in sport and recreational aviation should be provided with the possibility, as an alternative to design certification, to declare the compliance of the design of an aircraft, and if applicable of the engine and propeller, with the relevant industry standards, where it is considered that this will ensure an acceptable level of safety. |
(4) |
Organisations involved in the design and production of products used in sport and recreational aviation should also be provided with the possibility to utilise a more proportionate process for the certification of such products. |
(5) |
Organisations involved in the design and production of products used in sport and recreational aviation should be provided with the possibility, as an alternative to an organisational approval, to declare their capability to design and produce products and parts. Those organisations should be able to use existing approvals as a means to demonstrate their capability in conducting design and production activities. |
(6) |
Environmental protection requirements should be also laid down for the products the design of which is subject to a declaration of design compliance. Such environmental protection requirements should be based on requirements contained in Volumes I, II and III of Annex 16 to the Convention on International Civil Aviation (3) in order to ensure the same, uniform level of environmental protection irrespective of whether a product is subject to type certification or a declaration of design compliance. |
(7) |
Regulation (EU) No 748/2012 should therefore be amended accordingly. |
(8) |
A sufficient transitional period should be provided for organisations involved in the design and production of aircraft primarily used in sport and recreational aviation to ensure their compliance with the new rules and procedures introduced by this Regulation. |
(9) |
The measures provided for in this Regulation are in accordance with Opinion No 05/2021 (4), issued by the European Union Aviation Safety Agency in accordance with Article 76(1) of Regulation (EU) 2018/1139, |
HAS ADOPTED THIS REGULATION:
Article 1
Regulation (EU) No 748/2012 is amended as follows:
(1) |
the title is replaced by the following: ‘ COMMISSION REGULATION (EU) No 748/2012 of 3 August 2012 laying down implementing rules for the airworthiness and environmental certification or declaration of compliance of aircraft and related products, parts and appliances, as well as for the capability requirements of design and production organisations (recast) ’; |
(2) |
Article 1 is replaced by the following: ‘Article 1 Scope and definitions 1. This Regulation lays down, in accordance with Articles 19 and 62 of Regulation (EU) 2018/1139, common technical requirements and administrative procedures for the airworthiness and environmental certification of products, parts and appliances specifying:
2. For the purpose of this Regulation, the following definitions shall apply:
|
(3) |
Article 2 is replaced by the following: ‘Article 2 Certification of products, parts and appliances 1. Products, parts and appliances shall be issued certificates as specified in Annex I (Part 21). 2. By way of derogation from paragraph 1 of this Article, certificates may be alternatively issued as specified in Annex Ib (Part 21 Light) for the following products:
3. By way of derogation from paragraphs 1 and 2 of this Article, a declaration of design compliance may alternatively be made, as specified in Annex Ib (Part 21 Light), for the following products:
4. By way of derogation from paragraphs 1 to 3 of this Article, aircraft, including any installed product, part and appliance, which are not registered in a Member State shall be exempted from the provisions of Subparts H and I of Section A of Annex I (Part 21) and Subparts H and I of Section A of Annex Ib (Part 21 Light). They shall also be exempted from the provisions of Subpart P of Section A of Annex I (Part 21) and Subpart P of Section A of Annex Ib (Part 21 Light), except where aircraft identification marks are prescribed by a Member State.’; |
(4) |
the following Article 2a is inserted: ‘Article 2a Transitional arrangements for certificates previously issued under Annex I (Part 21) 1. A holder of a valid type certificate or a supplemental type certificate issued, or deemed to have been issued, by the Agency under Annex I (Part 21) may, until 25 August 2025 request to the Agency to maintain, from a given date, the type design approved under that certificate in accordance with Annex Ib (Part 21 Light), provided that the product covered by that certificate is within the scope of Article 2(2). 2. Where a request is made pursuant to paragraph 1, that type certificate or supplemental type certificate shall be governed, as of the given date referred to in paragraph 1, by the provisions of Annex Ib (Part 21 Light) regarding the type certificates or supplemental type certificates, as applicable. The Agency shall amend the type certificate data sheet or supplemental type certificate data sheet accordingly.’; |
(5) |
in Article 3, paragraphs 3 and 4 are replaced by the following: ‘3. With regard to products for which a type-certification process was proceeding through the JAA or a Member State on 28 September 2003, the following shall apply:
4. With regard to products that have a national type certificate, or equivalent, and for which the approval process of a change carried out by a Member State was not finalised at the time when the type certificate had to be approved in accordance with this Regulation, the following conditions shall apply:
|
(6) |
in Article 8, paragraphs 2 and 3 are replaced by the following: ‘2. By way of derogation from paragraph 1 of this Article, a natural or legal person responsible for the design of products whose principal place of business is in a Member State and who applies for or holds a certificate for the design of products, or changes or repairs thereto, in accordance with Article 2(2) may, alternatively, demonstrate their capability in accordance with Annex Ib (Part 21 Light). 3. Natural or legal persons involved in the design of aircraft subject to a declaration of design compliance referred to in Article 2(3) need not demonstrate their capability.’; |
(7) |
in Article 8, the following paragraph 5 is added: ‘5. By way of derogation from paragraph 1 of this Article, an organisation whose principal place of business is in a non-Member State may demonstrate its capability by holding a certificate issued by that State for the product, part and appliance for which it applies in accordance with Annex I (Part 21), provided that:
|
(8) |
in Article 9, paragraphs 2 and 3 are replaced by the following: ‘2. By way of derogation from paragraph 1 of this Article, a natural or legal person whose principal place of business is in a Member State and who is responsible for the manufacture of products and their parts and appliances in accordance with Article 2(2) may alternatively demonstrate their capability in accordance with Annex Ib (Part 21 Light). 3. The demonstration of capability pursuant to paragraphs 1 or 2 shall not be required where the production organisation or natural or legal person are involved in the following manufacturing activities:
|
(9) |
Article 10 is replaced by the following: ‘Article 10 Agency measures 1. The Agency shall develop acceptable means of compliance (“AMC”) which competent authorities, organisations and personnel may use to demonstrate compliance with the provisions of Annex I (Part 21) and Annex Ib (Part 21 Light). 2. The AMC issued by the Agency shall neither introduce new requirements nor alleviate the requirements of Annex I (Part 21) and Annex Ib (Part 21 Light).’; |
(10) |
Annex I (Part 21) is amended in accordance with Annex I to this Regulation; |
(11) |
Annex Ib (Part 21 Light) is added as set out in Annex II to this Regulation. |
Article 2
This Regulation shall enter into force on the twentieth day following that of its publication in the Official Journal of the European Union.
It shall apply from 25 August 2023.
This Regulation shall be binding in its entirety and directly applicable in all Member States.
Done at Brussels, 2 June 2022.
For the Commission
The President
Ursula VON DER LEYEN
(1) OJ L 212, 22.8.2018, p. 1.
(2) Commission Regulation (EU) No 748/2012 of 3 August 2012 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations (OJ L 224, 21.8.2012, p. 1).
(3) Convention on International Civil Aviation, signed at Chicago on 7 December 1944 (the ‘Chicago Convention’).
(4) Opinion 05/2021 of 22 October 2021 of the European Union Aviation Safety Agency, Part 21 Light – Certification and declaration of design compliance of aircraft used for sport and recreational aviation and related products and parts, and declaration of design and production capability of organisations, https://www.easa.europa.eu/document-library/opinions/opinion-052021
ANNEX I
Annex I (Part 21) to Regulation (EU) No 748/2012 is amended as follows:
(1) |
in Section A, Subpart G is amended as follows:
|
(2) |
in Section A, Subpart H is amended as follows:
|
(3) |
in Section A, Subpart I is amended as follows:
|
(4) |
in Section A, Subpart J is amended as follows:
|
(5) |
in Section A, in Subpart K, in point 21.A.307, the following point (b)(7) is inserted:
|
(6) |
In Appendix I, the text in title ‘Instructions for the use of EASA Form 1’ is replaced by the following: “These instructions relate only to the use of EASA Form 1 for production purposes. Attention is drawn to Appendix II to Annex I (Part-M) of Regulation (EU) No 1321/2014 which covers the use of EASA Form 1 for maintenance purposes. 1. PURPOSE AND USE
2. GENERAL FORMAT
3. COPIES
4. ERROR(S) ON A CERTIFICATE
5. COMPLETION OF THE CERTIFICATE BY THE ORIGINATOR
|
(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).
ANNEX II
The following Annex Ib (Part 21 Light) is inserted:
“Contents
21L.1 |
Scope |
21L.2 |
Competent authority |
SECTION A – |
TECHNICAL REQUIREMENTS |
SUBPART A – |
GENERAL PROVISIONS |
21L.A.1 |
Scope |
21L.A.2 |
Obligations and actions performed by a person other than the applicant for, or holder of, a certificate or the declarant of a declaration of design compliance |
21L.A.3 |
Reporting system |
21L.A.4 |
Airworthiness directives |
21L.A.5 |
Collaboration between design and production |
21L.A.6 |
Marking |
21L.A.7 |
Record-keeping |
21L.A.8 |
Manuals |
21L.A.9 |
Instructions for continued airworthiness |
21L.A.10 |
Access and investigation |
21L.A.11 |
Findings and observations |
21L.A.12 |
Means of compliance |
SUBPART B – |
TYPE CERTIFICATES |
21L.A.21 |
Scope |
21L.A.22 |
Eligibility |
21L.A.23 |
Demonstration of design capability |
21L.A.24 |
Application for a type certificate |
21L.A.25 |
Demonstration of compliance |
21L.A.26 |
Type design |
21L.A.27 |
Requirements for the issuance of a type certificate |
21L.A.28 |
Obligations of a type-certificate holder |
21L.A.29 |
Transferability of a type certificate |
21L.A.30 |
Continued validity of a type certificate |
SUBPART C – |
DECLARATIONS OF AIRCRAFT DESIGN COMPLIANCE |
21L.A.41 |
Scope |
21L.A.42 |
Eligibility |
21L.A.43 |
Declaration of design compliance |
21L.A.44 |
Compliance activities for a declaration of design compliance |
21L.A.45 |
Detailed technical specifications and environmental protection requirements that are applicable to aircraft subject to declarations of design compliance |
21L.A.46 |
Aircraft design data |
21L.A.47 |
Obligations of the declarant of a declaration of design compliance |
21L.A.48 |
Non-transferability of a declaration of aircraft design compliance |
SUBPART D – |
CHANGES TO TYPE CERTIFICATES |
21L.A.61 |
Scope |
21L.A.62 |
Standard changes |
21L.A.63 |
Classification of changes to a type certificate |
21L.A.64 |
Eligibility |
21L.A.65 |
Application for a change to a type certificate |
21L.A.66 |
Demonstration of compliance |
21L.A.67 |
Requirements for the approval of a minor change to a type certificate |
21L.A.68 |
Requirements for the approval of a major change to a type certificate |
21L.A.69 |
Approval of a change to a type certificate under a privilege |
21L.A.70 |
Obligations for minor changes to a type certificate |
SUBPART E – |
SUPPLEMENTAL TYPE CERTIFICATES |
21L.A.81 |
Scope |
21L.A.82 |
Eligibility |
21L.A.83 |
Demonstration of design capability |
21L.A.84 |
Application for a supplemental type certificate |
21L.A.85 |
Demonstration of compliance |
21L.A.86 |
Requirements for approval of a supplemental type certificate |
21L.A.87 |
Approval of a supplemental type certificate under a privilege |
21L.A.88 |
Obligations of a holder of a supplemental type certificate |
21L.A.89 |
Transferability of a supplemental type certificate |
21L.A.90 |
Continued validity of a supplemental type certificate |
21L.A.91 |
Changes to a part of a product covered by a supplemental type certificate |
SUBPART F – |
CHANGES TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED |
21L.A.101 |
Scope |
21L.A.102 |
Standard changes |
21L.A.103 |
Classification of changes to the design of an aircraft for which design compliance has been declared |
21L.A.104 |
Eligibility |
21L.A.105 |
Declaration of design compliance for minor changes |
21L.A.106 |
Obligations of the person making a declaration of compliance of the design of a minor change |
21L.A.107 |
Declaration of design compliance for a major change |
21L.A.108 |
Compliance activities for declaring compliance of a major change |
SUBPART G – |
DECLARED PRODUCTION ORGANISATIONS |
21L.A.121 |
Scope |
21L.A.122 |
Eligibility |
21L.A.123 |
Declaration of production capability |
21L.A.124 |
Management system for production |
21L.A.125 |
Resources of the declared production organisation |
21L.A.126 |
Scope of work |
21L.A.127 |
Obligations of the declared production organisation |
21L.A.128 |
Notification of changes and cessation of activities |
SUBPART H – |
CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS |
21L.A.141 |
Scope |
21L.A.142 |
Eligibility |
21L.A.143 |
Application for a certificate of airworthiness or a restricted certificate of airworthiness |
21L.A.144 |
Obligations of the applicant for a certificate of airworthiness or a restricted certificate of airworthiness |
21L.A.145 |
Transferability and re-issuance of a certificate of airworthiness and of a restricted certificate of airworthiness within Member States |
21L.A.146 |
Continued validity of a certificate of airworthiness and of a restricted certificate of airworthiness |
SUBPART I – |
NOISE CERTIFICATES AND RESTRICTED NOISE CERTIFICATES |
21L.A.161 |
Scope |
21L.A.162 |
Eligibility |
21L.A.163 |
Application |
21L.A.164 |
Transferability and re-issuance of noise certificates and restricted noise certificates within Member States |
21L.A.165 |
Continued validity of a noise certificate and of a restricted noise certificate |
SUBPART J – |
DECLARED DESIGN ORGANISATIONS |
21L.A.171 |
Scope |
21L.A.172 |
Eligibility |
21L.A.173 |
Declaration of design capability |
21L.A.174 |
Management system for design |
21L.A.175 |
Resources of the declared design organisation |
21L.A.176 |
Scope of work |
21L.A.177 |
Obligations of the declared design organisation |
21L.A.178 |
Notification of changes and cessation of activities |
SUBPART K – |
PARTS |
21L.A.191 |
Scope |
21L.A.192 |
Showing of compliance |
21L.A.193 |
Release of parts for installation |
SUBPART M – |
DESIGN OF REPAIRS TO TYPE-CERTIFIED PRODUCTS |
21L.A.201 |
Scope |
21L.A.202 |
Standard repairs |
21L.A.203 |
Classification of repair designs to a type-certified product |
21L.A.204 |
Eligibility |
21L.A.205 |
Application for the approval of a repair design to a type-certified product |
21L.A.206 |
Demonstration of compliance |
21L.A.207 |
Requirements for the approval of a minor repair design |
21L.A.208 |
Requirements for the approval of a major repair design |
21L.A.209 |
Approval of a repair design under a privilege |
21L.A.210 |
Obligations of a holder of a repair design approval |
21L.A.211 |
Unrepaired damage |
SUBPART N – |
DESIGN OF REPAIRS TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED |
21L.A.221 |
Scope |
21L.A.222 |
Standard repairs |
21L.A.223 |
Classification of repair designs to an aircraft for which design compliance has been declared |
21L.A.224 |
Eligibility |
21L.A.225 |
Declaration of design compliance for minor repair designs |
21L.A.226 |
Declaration of design compliance of major repair designs |
21L.A.227 |
Compliance activities for declaring compliance of a major repair design |
21L.A.228 |
Obligations of the declarant of a declaration of design compliance of a repair design |
21L.A.229 |
Unrepaired damage |
SUBPART O – |
EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS |
SUBPART P – |
PERMIT TO FLY |
21L.A.241 |
Permit to fly and flight conditions |
SUBPART Q – |
IDENTIFICATION OF PRODUCTS AND PARTS |
21L.A.251 |
Scope |
21L.A.252 |
Design of markings |
21L.A.253 |
Identification of products |
21L.A.254 |
Handling of identification data |
21L.A.255 |
Identification of parts |
SUBPART R – |
STATEMENT OF CONFORMITY FOR AIRCRAFT AND AUTHORISED RELEASE CERTIFICATE (EASA FORM 1) FOR ENGINES AND PROPELLERS, OR PARTS THEREOF, THAT CONFORM TO A DECLARATION OF DESIGN COMPLIANCE |
21L.A.271 |
Scope |
21L.A.272 |
Eligibility |
21L.A.273 |
Production control system |
21L.A.274 |
Issuance of a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1) |
21L.A.275 |
Obligations of a natural or legal person issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1) |
SECTION B – |
PROCEDURES FOR COMPETENT AUTHORITIES |
SUBPART A – |
GENERAL PROVISIONS |
21L.B.11 |
Oversight documentation |
21L.B.12 |
Exchange of information |
21L.B.13 |
Information to the Agency |
21L.B.14 |
Airworthiness directives received from non-Member States |
21L.B.15 |
Immediate reaction to a safety problem |
21L.B.16 |
Management system |
21L.B.17 |
Allocation of tasks to qualified entities |
21L.B.18 |
Changes in the management system |
21L.B.19 |
Resolution of disputes |
21L.B.20 |
Record-keeping |
21L.B.21 |
Findings and observations |
21L.B.22 |
Enforcement measures |
21L.B.23 |
Airworthiness directives |
21L.B.24 |
Means of compliance |
SUBPART B – |
TYPE CERTIFICATES |
21L.B.41 |
Certification specifications |
21L.B.42 |
Initial investigation |
21L.B.43 |
Type-certification basis for a type certificate |
21L.B.44 |
Special conditions |
21L.B.45 |
Designation of the applicable environmental protection requirements for a type certificate |
21L.B.46 |
Investigation |
21L.B.47 |
Issuance of a type certificate |
21L.B.48 |
Continuing airworthiness oversight of products for which a type certificate has been issued |
21L.B.49 |
Transfer of a type certificate |
SUBPART C – |
DECLARATIONS OF DESIGN COMPLIANCE |
21L.B.61 |
Detailed technical specifications and applicable environmental protection requirements for declarations of product design compliance |
21L.B.62 |
Initial oversight investigation |
21L.B.63 |
Registration of a declaration of design compliance |
21L.B.64 |
Continuing airworthiness oversight of aircraft for which design compliance has been declared |
SUBPART D – |
CHANGES TO TYPE CERTIFICATES |
21L.B.81 |
Type-certification basis and applicable environmental protection requirements for a major change to a type certificate |
21L.B.82 |
Investigation and issuance of an approval of a minor change to a type certificate |
21L.B.83 |
Investigation of a major change to a type certificate |
21L.B.84 |
Issuance of an approval of a major change to a type certificate |
21L.B.85 |
Continuing airworthiness oversight of changed products for which a type certificate has been issued |
SUBPART E – |
SUPPLEMENTAL TYPE CERTIFICATES |
21L.B.101 |
Type-certification basis and applicable environmental protection requirements for a supplemental type certificate |
21L.B.102 |
Investigation |
21L.B.103 |
Issuance of a supplemental type certificate |
21L.B.104 |
Continuing airworthiness oversight of products for which a supplemental type certificate has been issued |
SUBPART F – |
CHANGES TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED |
21L.B.121 |
Initial oversight investigation of a declaration of design compliance of a major change to the design of an aircraft for which design compliance has been declared |
21L.B.122 |
Registration of a declaration of design compliance for a major change to an aircraft design |
21L.B.123 |
Continuing airworthiness oversight of a changed aircraft for which design compliance has been declared |
SUBPART G – |
DECLARED PRODUCTION ORGANISATIONS |
21L.B.141 |
Initial oversight investigation |
21L.B.142 |
Registration of a declaration of production capability |
21L.B.143 |
Oversight |
21L.B.144 |
Oversight programme |
21L.B.145 |
Oversight activities |
21L.B.146 |
Changes to declarations |
SUBPART H – |
CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS |
21L.B.161 |
Investigation |
21L.B.162 |
Issuance or amendment of a certificate of airworthiness or a restricted certificate of airworthiness |
21L.B.163 |
Oversight |
SUBPART I – |
NOISE CERTIFICATES |
21L.B.171 |
Investigation |
21L.B.172 |
Issuance or amendment of noise certificates |
21L.B.173 |
Oversight |
SUBPART J – |
DECLARED DESIGN ORGANISATIONS |
21L.B.181 |
Initial oversight investigation |
21L.B.182 |
Registration of a declaration of design capability |
21L.B.183 |
Oversight |
21L.B.184 |
Oversight programme |
21L.B.185 |
Oversight activities |
21L.B.186 |
Changes to declarations |
SUBPART K – |
PARTS |
SUBPART M – |
DESIGN OF REPAIRS TO TYPE-CERTIFIED PRODUCTS |
21L.B.201 |
Type-certification basis and applicable environmental protection requirements for a repair design approval |
21L.B.202 |
Investigation and issuance of an approval for a minor repair design |
21L.B.203 |
Investigation of an application for the approval of a major repair design |
21L.B.204 |
Issuance of an approval of a major repair design |
21L.B.205 |
Continuing airworthiness oversight of products for which a repair design has been approved |
21L.B.206 |
Unrepaired damage |
SUBPART N – |
DESIGN OF REPAIRS TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED |
21L.B.221 |
Initial oversight investigation of a declaration of design compliance of a major repair design to an aircraft for which design compliance has been declared |
21L.B.222 |
Registration of a declaration of a major repair design to an aircraft for which design compliance has been declared |
21L.B.223 |
Continuing airworthiness oversight of a repair design for which design compliance has been declared |
SUBPART O – |
EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS |
SUBPART P – |
PERMIT TO FLY |
21L.B.241 |
Investigation prior to the issuance of a permit to fly |
21L.B.242 |
Investigation prior to issuance of the flight conditions |
SUBPART Q – |
IDENTIFICATION OF PRODUCTS AND PARTS |
SUBPART R – |
STATEMENT OF CONFORMITY FOR AIRCRAFT AND AUTHORISED RELEASE CERTIFICATES (EASA FORM 1) FOR ENGINES AND PROPELLERS, AND PARTS THEREOF, THAT CONFORM TO A DECLARATION OF DESIGN COMPLIANCE |
21L.B.251 |
Oversight |
21L.B.252 |
Oversight programme |
21L.B.253 |
Oversight activities |
Appendices to Annex Ib
21L.1 Scope
(reserved)
21L.2 Competent authority
(reserved)
SECTION A
TECHNICAL REQUIREMENTS
SUBPART A – GENERAL PROVISIONS
21L.A.1 Scope
This Section establishes general rights and obligations that are applicable to:
(a) |
the applicant for, and holder of, any certificate issued or to be issued in accordance with this Annex; |
(b) |
any declarant of design or production capability or of design compliance; and |
(c) |
any natural or legal person issuing a statement of conformity for an aircraft, or an authorised release certificate (EASA Form 1) for an engine, propeller or part produced. |
21L.A.2 Obligations and actions performed by a person other than the applicant for, or holder of, a certificate or the declarant of a declaration of design compliance
The actions and obligations required to be undertaken by the applicant for, or holder of, a certificate for a product or part or by the declarant of a declaration of design compliance under this Section may be undertaken on its behalf by any other natural or legal person, provided that the applicant’s, holder’s or declarant’s obligations are and will be properly discharged.
21L.A.3 Reporting system
(a) |
Without prejudice to Regulation (EU) No 376/2014 of the European Parliament and of the Council (1) and its delegated and implementing acts, any natural or legal person who holds or has applied for a type certificate, supplemental type certificate, major repair design approval, or any other relevant certificate deemed to have been issued under this Annex, or who has declared the compliance of an aircraft design, or a design change or repair design to it under this Annex shall:
|
(b) |
Without prejudice to Regulation (EU) No 376/2014 and its delegated and implementing acts, any natural or legal person who has declared their production capability under Subpart G of this Annex, or who produces a product or part under Subpart R of this Annex, shall:
The reporting obligations of point 21.A.3A(b) of Annex I of natural and legal persons who hold or have applied for a production organisation approval shall include occurrences related to products and parts produced in conformity with design data approved or declared in accordance with this Annex, and, where the design compliance was declared, reports shall be made to the declarant of design compliance. |
(c) |
Without prejudice to Regulation (EU) No 376/2014 and its delegated and implementing acts, any natural or legal person referred to in points (a) and (b) when reporting in accordance with points (a)(3), (b)(2), (b)(3) and (b)(4), shall appropriately safeguard the confidentiality of the reporter and of the persons mentioned in the report. |
(d) |
Without prejudice to Regulation (EU) No 376/2014 and its delegated and implementing acts, any natural or legal person referred to in points (a) and (b) shall make the reports defined in points (a)(3) and (b)(3) in a form and manner established by the competent authority as soon as practicable, and in any case, dispatch the reports not later than 72 hours after the natural or legal person referred to in points (a) and (b) has identified the possible unsafe condition, unless exceptional circumstances prevent this. |
(e) |
Without prejudice to Regulation (EU) No 376/2014 and its delegated and implementing acts, if an occurrence reported under point (a)(3) or under point (b)(3) results from a deficiency in the design, or a production deficiency, the holder of the type certificate, supplemental type certificate, major repair design approval, or any other relevant certificate deemed to have been issued under this Annex, the declarant of a declaration of design compliance or the production organisation referred to in point (b) as appropriate, shall investigate the reason for the deficiency and report to the Agency and to the competent authority of the Member State responsible in accordance with point 21L.2, if any, the results of its investigation and any action it is taking or proposes to take to correct that deficiency. |
(f) |
If the competent authority finds that an action is required to correct the deficiency, the holder of the type certificate, supplemental type certificate, major repair design approval, or any other relevant certificate deemed to have been issued under this Annex, the declarant of a declaration of design compliance, or the production organisation referred to in point (b) as appropriate, shall submit the relevant data to the competent authority upon its request. |
21L.A.4 Airworthiness directives
When an airworthiness directive has to be issued by the Agency in accordance with point 21L.B.23 to correct an unsafe condition, or to require the performance of an inspection, the holder of the type certificate, supplemental type certificate, major repair design approval, or any other relevant certificate deemed to have been issued under this Annex, as well as the declarant of a declaration of design compliance, as applicable, shall:
(a) |
propose the appropriate corrective action or required inspections, or both, and submit details of these proposals to the Agency for approval; |
(b) |
following the approval by the Agency of the proposals referred to under point (a), make available to all known operators or owners of the product or part, and, on request, to any person required to comply with the airworthiness directive, appropriate descriptive data and accomplishment instructions. |
21L.A.5 Collaboration between design and production
The holder of a type certificate, supplemental type certificate, approval of a change to type certificate or approval of a repair design, the declarant of a declaration of design compliance, and the organisation or the natural or legal person producing products or parts of that specific design shall collaborate so as to ensure that the product or part are in conformity to that design and to ensure the continued airworthiness of the product or part.
21L.A.6 Marking
(a) |
The holder of a type certificate, supplemental type certificate, approval of a change to type certificate or approval of a repair design, or the declarant of a declaration of design compliance shall specify the marking for products or parts in accordance with Subpart Q of this Annex. |
(b) |
The organisation or the natural or legal person producing products or parts shall mark these products and parts in accordance with Subpart Q of this Annex. |
21L.A.7 Record-keeping
All natural or legal persons who hold or who have applied for a type certificate, supplemental type certificate, repair design approval, or permit to fly, who have declared design compliance, who have issued a declaration of design or production capability, or who produce products or parts under this Regulation shall:
(a) |
when designing a product or part or changes or repairs thereto, establish a record-keeping system that incorporates the requirements imposed on its partners and subcontractors and maintain the relevant design information/data and hold it at the disposal of the Agency in order to provide the information necessary to ensure their continued airworthiness and compliance with the applicable environmental protection requirements; |
(b) |
when producing a product or part, establish a record-keeping system and record the details of the work relevant to the conformity of the products or parts, and the requirements imposed on its partners and suppliers, and hold them at the disposal of the competent authority in order to provide the information necessary to ensure the continuing airworthiness of the product and part; |
(c) |
with regard to permits to fly, in addition to the record-keeping requirements established in point 21.A.5(c) of Annex I, record any documents produced to demonstrate compliance with the additional requirements established in point 21L.A.241(b), and hold them at the disposal of the Agency and the competent authority; |
(d) |
retain records of competence and the qualifications of personnel who are involved in design or production and in the independent function to monitor the compliance, if required by points 21L.A.125(c), 21L.A.175(b) or 21L.A.175(e). |
21L.A.8 Manuals
The holder of a type certificate or supplemental type certificate or the declarant of a declaration of design compliance shall produce, maintain and update master copies of all the manuals or variations in the manuals required by the applicable type-certification basis, the applicable detailed technical specifications and the applicable environmental protection requirements for the product or part, and provide copies, on request, to the Agency.
21L.A.9 Instructions for continued airworthiness
(a) |
The holder of a type certificate, supplemental type certificate, design change or repair design approval or the declarant of a declaration of design compliance shall establish the information which is necessary for ensuring that the airworthiness of the aircraft type and any associated part, conforming to that design, is maintained throughout the operational life. |
(b) |
The holder of a type certificate, supplemental type certificate, design change or repair design approval or the declarant of a declaration of design compliance shall provide the information established in (a) before that design is released to service. |
(c) |
The instructions for continued airworthiness shall be provided by:
Thereafter, these certificate holders or declarants shall make this information available on request to any other person required to comply with those instructions for continued airworthiness. |
(d) |
By way of derogation from point (b), the type-certificate holder or declarant of a declaration of design compliance 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. |
(e) |
The design approval holder or declarant of a declaration of design compliance who is required to provide instructions for continued airworthiness in accordance with point (b) shall also make available all the changes to those instructions to all the known operators of the product affected by the change, and, on request, to any other person required to comply with those changes. |
21L.A.10 Access and investigation
All natural or legal persons who hold or who have applied for a type certificate, supplemental type certificate, major repair design approval, permit to fly, certificate of airworthiness, restricted certificate of airworthiness, noise certificate or restricted noise certificate, who have declared design compliance, who have declared their design or production capability or who produce aircraft, engines, propellers or parts under Subpart R of this Annex, shall:
(a) |
grant the competent authority access to any facility, product, part, document, record, data, processes, procedures or any other material, and permit the review of any report and make any inspection and perform or witness any test that is necessary to verify the compliance and the continued compliance with the applicable requirements of this Section; |
(b) |
if the natural or legal person uses partners, suppliers or subcontractors, make arrangements with them to ensure that the competent authority has access and can investigate as described in point (a). |
21L.A.11 Findings and observations
(a) |
After the receipt of the notification of findings, the natural or legal person who holds or who has applied for a type certificate, supplemental type certificate, major repair design approval, permit to fly, certificate of airworthiness, restricted certificate of airworthiness, noise certificate or restricted noise certificate, who has declared design compliance, who has declared their design or production capability or who produces aircraft, engines, propellers or parts under Subpart R of this Annex, shall take the following steps within the time period determined by the competent authority in accordance with point (d) or (e) of point 21L.B.21:
|
(b) |
An observation notified by the competent authority in accordance with point (f) of point 21L.B.21 shall be given due consideration. The natural or legal person shall record the decision taken in respect of those observations. |
21L.A.12 Means of compliance
(a) |
A legal or natural person may use any alternative means of compliance to the acceptable means of compliance (AMC) to establish compliance with this Regulation. |
(b) |
If a natural or legal person wishes to use an alternative means of compliance, they shall, prior to using it, provide the competent authority with a full description. The description shall include any revisions to manuals or procedures that may be relevant, as well as an explanation indicating how compliance with this Regulation is achieved. |
(c) |
The natural or legal person may use those alternative means of compliance subject to prior approval from the competent authority. |
SUBPART B – TYPE CERTIFICATES
21L.A.21 Scope
This Subpart establishes the procedure for applying for type certificates, and establishes the rights and obligations of the applicants for, and holders of, those certificates for products, when the product is one of the following:
(a) |
an aeroplane with a maximum take-off mass (MTOM) of 2 000 kg or less with a seating configuration of maximum four persons; |
(b) |
a sailplane or powered sailplane with an MTOM of 2 000 kg or less; |
(c) |
a balloon; |
(d) |
a hot air airship; |
(e) |
a passenger gas airship designed for not more than four persons; |
(f) |
a rotorcraft with an MTOM of 1 200 kg or less with a seating configuration of maximum four persons; |
(g) |
a piston engine and fixed pitch propeller that are intended to be installed on an aircraft referred to in points (a) to (f). In such cases, the type certificate data sheet shall be appropriately annotated to only permit installation of the engine or propeller on such aircraft; |
(h) |
gyroplanes. |
21L.A.22 Eligibility
Any natural or legal person who has demonstrated, or is in the process of demonstrating, their design capability in accordance with point 21L.A.23, may apply for a type certificate under the conditions laid down in this Subpart.
21L.A.23 Demonstration of design capability
An applicant for a type certificate shall demonstrate their design capability by:
(a) |
holding a design organisation approval with terms of approval that cover the respective category of the product, issued by the Agency in accordance with Subpart J of Section A of Annex I (Part 21); or |
(b) |
declaring their design capability for the type of design work and the category of the product in accordance with Subpart J of this Annex. |
21L.A.24 Application for a type certificate
(a) |
An application for a type certificate shall be made in a form and manner established by the Agency. |
(b) |
An application for a type certificate shall include as a minimum:
|
(c) |
An application for a type certificate shall remain valid for 3 years. In case a type certificate has not been issued within this period, a new application shall be made in accordance with points (a) and (b). |
21L.A.25 Demonstration of compliance
(a) |
The applicant for a type certificate shall, following the acceptance of the compliance demonstration plan by the Agency and in accordance with its contents, then:
|
(b) |
The applicant for a type certificate shall provide the Agency with a recorded justification of the means of compliance within compliance documents according to the compliance demonstration plan. |
(c) |
When carrying out testing and inspections to demonstrate compliance in accordance with point (a), the applicant shall have verified and documented this verification prior to carrying out any test:
|
(d) |
The flight testing for the purpose of obtaining a type certificate shall be conducted in accordance with the methods for such flight testing specified by the Agency. The applicant for a type certificate shall make all the flight tests necessary to determine compliance with the applicable type-certification basis. The flight tests shall include a period of operation in a final configuration of a sufficient duration to ensure that there will be no safety issues when the aircraft first enters service. |
(e) |
An applicant for a type certificate shall allow the Agency to:
|
(f) |
Upon the completion of the compliance demonstration, the applicant shall declare to the Agency that:
|
21L.A.26 Type design
The applicant for a type certificate shall define the product type design to enable its unique and unambiguous identification, consisting of:
(a) |
drawings and specifications and a listing of those drawings and specifications that are necessary to define the configuration and the design features of the product; |
(b) |
information on the materials and processes used; |
(c) |
information on the methods of manufacture and assembly; |
(d) |
any airworthiness limitations; |
(e) |
the environmental compatibility requirements; and |
(f) |
any other data allowing by comparison the determination of the airworthiness, and, if relevant, the environmental compatibility of later products of the same type. |
21L.A.27 Requirements for the issuance of a type certificate
In order to be issued with a type certificate, the applicant shall:
(a) |
demonstrate their design capability in accordance with point 21L.A.23; |
(b) |
demonstrate the compliance of the design in accordance with point 21L.A.25; |
(c) |
demonstrate, for aircraft type certificates, that the engine or propeller, or both, if installed on the aircraft, have either:
|
(d) |
demonstrate that there are no unresolved issues from the physical inspection of the first article of that product in the final configuration or any other investigation carried out by the Agency in accordance with points (c) and (d) of point 21L.B.46. |
21L.A.28 Obligations of a type-certificate holder
The holder of a type certificate shall undertake the obligations of a type-certificate holder set forth in Subpart A of this Annex and shall continue to comply with the eligibility requirement under point 21L.A.22.
21L.A.29 Transferability of a type certificate
A type certificate may be transferred to a new holder, provided that the Agency has verified, in accordance with point 21L.B.49, that the natural or legal person to whom the type certificate is intended to be transferred is eligible in accordance with point 21L.A.22 to hold a type certificate and is able to undertake the obligations of a type-certificate holder under point 21L.A.28. The holder of the type certificate or the natural or legal person who wishes to adopt the certificate shall apply to the Agency to verify whether these conditions are complied with, in a form and manner established by the Agency.
21L.A.30 Continued validity of a type certificate
(a) |
A type certificate shall remain valid as long as:
|
(b) |
Upon surrender or revocation, the type certificate shall be returned to the Agency. |
SUBPART C – DECLARATIONS OF AIRCRAFT DESIGN COMPLIANCE
21L.A.41 Scope
(a) |
This Subpart establishes the procedure for declaring the design compliance of aircraft, and establishes the rights and obligations of the persons making such declarations. |
(b) |
This Subpart applies to the following categories of aircraft, provided that the design of the aircraft does not include novel or unusual design features:
|
(c) |
For the purpose of this Subpart, a design feature shall be considered to be novel or unusual if at the time that the declaration of design compliance is made, that design feature is not covered by the detailed technical specifications established and made available by the Agency in accordance with point 21L.B.61. |
21L.A.42 Eligibility
Any natural or legal person may declare the compliance of an aircraft design under the conditions laid down in this Subpart.
21L.A.43 Declaration of design compliance
(a) |
Prior to producing an aircraft or agreeing with a production organisation to produce an aircraft, a natural or legal person who designs that aircraft shall declare that its design complies with the applicable detailed technical specifications and the applicable environmental protection requirements referred to in point 21L.A.45. |
(b) |
The declaration shall be made in a form and manner established by the Agency and shall contain at least the following information:
|
(c) |
The declarant shall submit the declaration of design compliance referred to in point (b) to the Agency. Together with this declaration, the declarant shall provide to the Agency:
|
21L.A.44 Compliance activities for a declaration of design compliance
Prior to making a declaration of design compliance in accordance with point 21L.A.43, the declarant responsible for design of that aircraft shall, for that specific aircraft design:
(a) |
establish a compliance demonstration plan detailing the means for compliance demonstration that shall be followed during the compliance demonstration. This document shall be updated as necessary; |
(b) |
record the justification of compliance within compliance documents according to the compliance demonstration plan; |
(c) |
perform testing and inspections as necessary in accordance with the compliance demonstration plan; |
(d) |
ensure and record the conformity of the test articles and equipment and ensure that the test specimen conforms to the specifications, drawings, manufacturing processes, construction and assembly means in the design; |
(e) |
ensure that the test and measuring equipment to be used for testing are adequate for testing and appropriately calibrated; |
(f) |
allow the Agency to conduct or participate in any inspections or tests of aircraft in the final or suitably mature design and production configuration that are necessary to determine that the product has no feature or characteristic that makes the aircraft unsafe or environmentally incompatible for the intended use; |
(g) |
carry out flight testing, in accordance with the methods for such flight testing specified by the Agency, to determine whether the aircraft complies with the applicable detailed technical specifications and the applicable environmental protection requirements. The flight testing shall include a period of operation in the final configuration of a sufficient duration to ensure that there will be no safety issues when the aircraft first enters service. |
21L.A.45 Detailed technical specifications and environmental protection requirements that are applicable to aircraft subject to declarations of design compliance
The declarant shall demonstrate the compliance of the aircraft design with the detailed technical specifications and the applicable environmental protection requirements referred to in point 21L.B.61, which are applicable to that aircraft and which are effective on the date on which the declaration of design compliance is made to the Agency.
21L.A.46 Aircraft design data
(a) |
The declarant shall clearly define the aircraft design to enable its unique and unambiguous identification. |
(b) |
The aircraft design data that is used by the declarant to uniquely define the aircraft design shall include:
|
21L.A.47 Obligations of the declarant of a declaration of design compliance
The declarant who made a declaration of aircraft design compliance to the Agency in accordance with point 21L.A.43 shall:
(a) |
upon submission of the declaration, arrange for the Agency to conduct a physical inspection and flight tests of the first article of that aircraft in the final or a suitably mature configuration to ensure that the aircraft can achieve an acceptable level of safety and is environmentally compatible; |
(b) |
retain all the supporting documents for the declaration of design compliance, and make them available to the Agency upon request; |
(c) |
comply with all other obligations applicable to a declarant of a declaration of design compliance set forth in Subpart A of this Annex. |
21L.A.48 Non-transferability of a declaration of aircraft design compliance
(a) |
A declaration of aircraft design compliance cannot be transferred. |
(b) |
A natural or legal person who is taking over the design of an aircraft for which compliance of the design has been previously declared shall:
|
SUBPART D – CHANGES TO TYPE CERTIFICATES
21L.A.61 Scope
This Subpart establishes:
(a) |
the procedure for applying for the approval of changes to type certificates for products certified in accordance with this Annex, provided that the changed product is still within the scope of point 21L.A.21; |
(b) |
the rights and obligations of the applicants for, and holders of, those approvals referred to in point (a); |
(c) |
provisions regarding the standard changes that do not require an approval. |
21L.A.62 Standard changes
(a) |
Standard changes are those changes to a type certificate of a product approved in accordance with Subpart B of Section B of this Annex:
|
(b) |
Points 21L.A.63 to 21L.A.70 are not applicable to standard changes. |
21L.A.63 Classification of changes to a type certificate
(a) |
Changes to a type certificate shall be classified as minor or major. |
(b) |
A ‘minor change’ is a change that has no appreciable effect on the mass, balance, structural strength, reliability, certified noise or emissions levels, operational characteristics, or other characteristics affecting the airworthiness or the environmental compatibility of the product. |
(c) |
All other changes are ‘major changes’, unless the change in design, power, thrust, or mass is so extensive that a substantially complete investigation of compliance with the applicable type-certification basis or with the applicable environmental protection requirements or with the applicable detailed technical specifications is required, in which case the design shall be certified in accordance with Subpart B of this Annex. |
(d) |
The requirements for the approval of minor changes are those established in point 21L.A.67. |
(e) |
The requirements for the approval of major changes are those established in point 21L.A.68. |
21L.A.64 Eligibility
(a) |
Only the type-certificate holder may apply for the approval of a major change to a type certificate under this Subpart; all other applicants for a major change to a type certificate shall apply under Subpart E of this Annex. |
(b) |
Any natural or legal person may apply for the approval of a minor change to a type certificate under this Subpart. |
21L.A.65 Application for a change to a type certificate
(a) |
An application for the approval of a change to a type certificate shall be made in a form and manner established by the Agency. |
(b) |
For a major change to a type certificate, the applicant shall include in the application a compliance demonstration plan for the demonstration of compliance in accordance with point 21L.A.66, along with a proposal for the type-certification basis and the applicable environmental protection requirements, prepared in accordance with the requirements and options specified in point 21L.B.81. |
21L.A.66 Demonstration of compliance
(a) |
The applicant for a major change to a type certificate shall demonstrate compliance with the applicable type-certification basis and the applicable environmental protection requirements as established and notified to the applicant by the Agency in accordance with point 21L.B.81, and shall provide the Agency with the means by which such compliance has been demonstrated. |
(b) |
The applicant for a major change to a type certificate shall provide the Agency with a recorded justification of the means of compliance according to the compliance demonstration plan. |
(c) |
When carrying out testing and inspections to demonstrate compliance in accordance with point (a), the applicant shall have verified and documented this verification prior to carrying out any test:
|
(d) |
The flight testing for the purpose of obtaining an approval of a major change to a type certificate shall be conducted in accordance with the methods for such flight testing specified by the Agency. The applicant for a major change to a type certificate shall make all the flight tests necessary to determine compliance with the applicable type-certification basis and the applicable environmental protection requirements. |
(e) |
An applicant for a major change to a type certificate shall allow the Agency to:
|
(f) |
Upon completion of the compliance demonstration, the applicant shall declare to the Agency that:
|
21L.A.67 Requirements for the approval of a minor change to a type certificate
In order to be issued with an approval of a minor change to a type certificate, the applicant shall:
(a) |
demonstrate that the change and the areas affected by the change comply:
|
(b) |
declare compliance with the type-certification basis and the applicable environmental protection requirements that apply in accordance with point (a)(1), or with the certification specifications chosen in accordance with point (a)(2), record the justifications of compliance in the compliance documents, and record that no feature or characteristic has been identified that may make the changed product unsafe for the uses for which certification is requested; |
(c) |
submit to the Agency the justification of compliance for the change and the declaration of compliance. |
21L.A.68 Requirements for the approval of a major change to a type certificate
In order to be issued with an approval of a major change to a type certificate, the applicant shall:
(a) |
demonstrate that the change and the areas affected by the change comply with the type-certification basis and the applicable environmental protection requirements, as established and notified to the applicant by the Agency in accordance with point 21L.B.81; |
(b) |
demonstrate compliance in accordance with point 21L.A.66; |
(c) |
demonstrate that there are no unresolved issues from the physical inspection of the first article of that product in the final changed configuration carried out by the Agency in accordance with point 21L.A.66(e)(3). |
21L.A.69 Approval of a change to a type certificate under a privilege
(a) |
The approval of a change to a type certificate that it has designed may be issued by an approved design organisation without an application according to point 21L.A.65 in accordance with the scope of its privileges provided for in points (2) and (8) of point 21.A.263(c) of Annex I (Part 21) instead of the Agency, as recorded in the terms of approval. |
(b) |
When issuing an approval of a change to type certificate in accordance with point (a), the design organisation shall:
|
21L.A.70 Obligations for minor changes to a type certificate
The holder of an approval of a minor change to a type certificate shall ensure that the obligations for holders of minor change approvals of Subpart A of this Annex are undertaken.
SUBPART E – SUPPLEMENTAL TYPE CERTIFICATES
21L.A.81 Scope
This Subpart establishes the procedure for natural or legal persons other than the holder of that type certificate for applying for the approval of major changes to type certificates, issued under Annex I (Part 21) or this Annex, of products within the scope of point 21L.A.21, provided that the changed product is still within the scope of that point, and establishes the rights and obligations of the applicants for, and holders of, those certificates.
21L.A.82 Eligibility
Any natural or legal person who has demonstrated, or is in the process of demonstrating, or have declared, their design capability in accordance with point 21L.A.83 may apply for a supplemental type certificate under the conditions laid down in this Subpart.
21L.A.83 Demonstration of design capability
An applicant for a supplemental type certificate shall demonstrate their design capability by:
(a) |
holding a design organisation approval with terms of approval that cover the respective category of product, issued by the Agency in accordance with Subpart J of Section A of Annex I (Part 21); or |
(b) |
declaring their design capability for the scope of the product in accordance with Subpart J of this Annex. |
21L.A.84 Application for a supplemental type certificate
(a) |
An application for a supplemental type certificate shall be made in a form and manner established by the Agency. |
(b) |
When applying for a supplemental type certificate, the applicant shall:
|
21L.A.85 Demonstration of compliance
(a) |
The applicant for a supplemental type certificate shall demonstrate compliance with the applicable type-certification basis and the applicable environmental protection requirements as established and notified to the applicant by the Agency in accordance with point 21L.B.101 and shall provide the Agency with the means by which such compliance has been demonstrated. |
(b) |
The applicant for a supplemental type certificate shall provide the Agency with a recorded justification of the means of compliance within compliance documents according to the compliance demonstration plan. |
(c) |
When carrying out testing and inspections to demonstrate compliance in accordance with point (a), the applicant shall have verified and documented this verification prior to carrying out any test:
|
(d) |
The flight testing for the purpose of obtaining a supplemental type certificate shall be conducted in accordance with the methods for such flight testing specified by the Agency. The applicant for a supplemental type certificate shall make all the flight tests necessary to determine compliance with the applicable type-certification basis. |
(e) |
An applicant for a supplemental type certificate shall allow the Agency to:
|
(f) |
Upon completion of the compliance demonstration, the applicant for a supplemental type certificate shall declare to the Agency that:
|
21L.A.86 Requirements for approval of a supplemental type certificate
(a) |
In order to be issued with a supplemental type certificate, the applicant shall:
|
(b) |
A supplemental type certificate shall be limited to the specific configuration(s) in the type certificate to which the related major change relates. |
21L.A.87 Approval of a supplemental type certificate under a privilege
(a) |
The approval of a supplemental type certificate for a major change it has designed may be issued by an approved design organisation without an application according to point 21L.A.84 in accordance with the scope of its privileges provided for in point (9) of point 21.A.263(c) of Annex I (Part 21) instead of the Agency, as recorded in the terms of approval. |
(b) |
When issuing a supplemental type certificate in accordance with point (a), the design organisation shall:
|
21L.A.88 Obligations of a holder of a supplemental type certificate
Each holder of a supplemental type certificate shall undertake the obligations of a supplemental type-certificate holder set forth in Subpart A of this Annex and shall continue to comply with the eligibility requirement under point 21L.A.82.
21L.A.89 Transferability of a supplemental type certificate
A supplemental type certificate may be transferred to a new holder, provided that the Agency has verified that the natural or legal person to whom the certificate is intended to be transferred is eligible in accordance with point 21L.A.83 to hold a supplemental type certificate and is able to undertake the obligations of a supplemental type-certificate holder under point 21L.A.88.
21L.A.90 Continued validity of a supplemental type certificate
(a) |
A supplemental type certificate shall remain valid as long as:
|
(b) |
Upon surrender or revocation, the type certificate shall be returned to the Agency. |
21L.A.91 Changes to a part of a product covered by a supplemental type certificate
(a) |
A minor change to a part of a product covered by a supplemental type certificate shall be approved in accordance with Subpart D of this Annex. |
(b) |
A major change to that part of a product covered by a supplemental type certificate shall be approved as a separate supplemental type certificate in accordance with this Subpart. |
(c) |
By way of derogation from point (b), a major change to that part of a product covered by a supplemental type certificate submitted by the supplemental type-certificate holder may be approved as a change to the existing supplemental type certificate in accordance with points 21L.A.63 to 21L.A.69. |
SUBPART F – CHANGES TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED
21L.A.101 Scope
This Subpart establishes:
(a) |
the procedure for declaring the compliance of a change to the design of an aircraft which was subject to a declaration made in accordance with Subpart C of this Annex; |
(b) |
the rights and obligations of the declarant making a declaration of compliance of the change referred to in point (a); and |
(c) |
provisions regarding the standard changes that do not require a declaration of design compliance. |
21L.A.102 Standard changes
(a) |
Standard changes are changes to the design of an aircraft which was subject to a declaration made in accordance with Subpart C of this Annex and which:
|
(b) |
Points 21L.A.103 to 21L.A.108 are not applicable to standard changes. |
21L.A.103 Classification of changes to the design of an aircraft for which design compliance has been declared
(a) |
Changes to the design of an aircraft which was subject to a declaration made in accordance with Subpart C of this Annex shall be classified as minor or major, using the criteria laid down in points 21L.A.63 (b) and (c). |
(b) |
The design compliance of a minor change shall be declared in accordance with point 21L.A.105. |
(c) |
The design compliance of a major change shall be declared in accordance with point 21L.A.107. |
21L.A.104 Eligibility
(a) |
A declarant who made a declaration of aircraft design compliance in accordance with Subpart C of this Annex may declare compliance of a minor change to the design of that aircraft under the conditions laid down in this Subpart. In addition, such a declaration of compliance may also be made, under the conditions laid down in this Subpart, by a design organisation approved in accordance with point (c)(3) of point 21.A.263 of Annex I (Part 21). |
(b) |
Only the declarant who made a declaration of aircraft design compliance in accordance with Subpart C of this Annex may declare the compliance of a major change to the design of an aircraft for which design compliance has been declared in accordance with Subpart C of this Annex, under the conditions laid down in this Subpart. |
(c) |
By derogation from point (b) of point 21.L.A.104, if the declarant who made a declaration of aircraft design compliance in accordance with Subpart C of this Annex is no longer active or is unresponsive to requests for design changes, the compliance of a changed aircraft design may also be declared in accordance with Subpart C of this Annex by a design organisation approved in accordance with point (c)(4) of point 21.A.263 of Annex I (Part 21) within the scope of their terms of approval, or by any other natural or legal person who is able to undertake the obligations laid down in point 21L.A.47 with respect to that changed aircraft. |
21L.A.105 Declaration of design compliance for minor changes
(a) |
Prior to installing or incorporating or agreeing with a production organisation to install or incorporate a minor change to the design of an aircraft for which design compliance has been declared in accordance with Subpart C of this Annex the organisation that has designed that minor change shall declare that the design of that minor change complies with:
|
(b) |
The declaration of design compliance shall be made in a form and manner established by the Agency. |
(c) |
The declarant or the organisation that has designed the minor change shall maintain a register of minor changes to the design of aircraft for which design compliance has been declared, and make any declaration made in accordance with point (a) available to the Agency upon request. |
21L.A.106 Obligations of the person making a declaration of compliance of the design of a minor change
Any person that has made a declaration of compliance of a minor change to an aircraft design in accordance with point 21L.A.105 shall:
(a) |
maintain a register of those declarations and shall make those declarations available to the Agency upon request; |
(b) |
retain all supporting documents for a declaration of design compliance, and make them available to the Agency upon request; |
(c) |
undertake all other obligations of a declarant of a declaration of design compliance set forth in Subpart A of this Annex. |
21L.A.107 Declaration of design compliance for a major change
(a) |
Prior to installing or incorporating or agreeing with a production organisation to install or incorporate a major change to the design of an aircraft for which design compliance has been declared in accordance with Subpart C of this Annex, the organisation that has designed that major change shall declare that the design of that major change and the areas affected by that change comply with:
|
(b) |
The declaration of design compliance shall be made in a form and manner established by the Agency. |
(c) |
The declaration shall contain at least the following information:
|
(d) |
The declarant that designs a major change shall submit the declaration referred to in point (c) to the Agency. Together with this declaration, the declarant shall provide to the Agency:
|
(e) |
The declaration of a major change to a declaration of design compliance shall be limited to the specific configuration(s) in the declaration of design compliance to which the change relates. |
21L.A.108 Compliance activities for declaring compliance of a major change
Prior to making a declaration of compliance in accordance with point 21L.A.107, the declarant shall, for that specific design:
(a) |
establish a compliance demonstration plan detailing the means for compliance demonstration that shall be followed during the compliance demonstration. This document shall be updated as necessary; |
(b) |
record the justification of compliance within compliance documents according to the compliance demonstration plan; |
(c) |
perform testing and inspections as necessary in accordance with the compliance demonstration plan; |
(d) |
ensure and record the conformity of the test articles and equipment and ensure that the test specimen conforms to the specifications, drawings, manufacturing processes, construction and assembly means in the design; |
(e) |
ensure that the test and measuring equipment to be used for testing are adequate for testing and appropriately calibrated; |
(f) |
allow the Agency to conduct or participate in any inspections or tests of aircraft in the final or suitably mature design and production configuration that are necessary to determine that the changed product has no feature or characteristic that makes the aircraft unsafe or environmentally incompatible for the intended use; |
(g) |
carry out flight testing, in accordance with the methods for such flight testing specified by the Agency, as necessary to determine that the aircraft complies with the applicable detailed technical specifications and the applicable environmental protection requirements. |
SUBPART G – DECLARED PRODUCTION ORGANISATIONS
21L.A.121 Scope
(a) |
This Subpart establishes:
|
(b) |
The following categories of products and parts may be produced by organisations which have made a declaration of production capability in accordance with this Subpart:
|
21L.A.122 Eligibility
Any natural or legal person (‘organisation’) may declare their production capability under this Subpart, if that person:
(a) |
has applied or intends to apply for the approval of the design of the product or part in accordance with this Annex; or |
(b) |
has declared or intends to declare the compliance of an aircraft design in accordance with this Annex; or |
(c) |
is collaborating with the applicant for, or holder of, an approval of the design of the product to be issued or issued in accordance with this Annex, or with the organisation that has declared or intends to declare the compliance of that aircraft design in accordance with this Annex, in order to ensure that the manufactured product or part is in conformity to that design, and to ensure the continued airworthiness of the product or part. |
21L.A.123 Declaration of production capability
(a) |
Prior to producing any products or parts, an organisation intending to show the conformity of those products or parts with the applicable design data shall declare its production capability. |
(b) |
The declaration, and any subsequent changes thereto, shall be made in a form and manner established by the competent authority. |
(c) |
The declaration shall include the information necessary for the competent authority to become familiar with the organisation and the intended scope of work, and shall include at least the following:
|
(d) |
The declaration of production capability shall be submitted to the competent authority. |
21L.A.124 Management system for production
(a) |
The declared production organisation shall establish, implement, and maintain a management system for production with clear accountability and lines of responsibility throughout the organisation that:
|
(b) |
The management system for production shall include a means to manage quality by maintaining a quality system that shall:
|
(c) |
The declared production organisation shall establish, as part of their management system for production, an independent function to monitor the compliance of the organisation with the relevant requirements, and compliance with, and the adequacy of, the production management system. This monitoring shall include a system to provide feedback to the person or group of persons referred to in points (c)(1) and (2) of point 21L.A.125 to ensure, as necessary, corrective action. |
(d) |
The declared production organisation shall establish, maintain and keep updated, as part of their management system for production, processes and procedures that ensure the compliance of products that are produced with the applicable design data. The declared production organisation shall make documentary evidence of these processes and procedures available to the competent authority upon request. |
(e) |
The declared production organisation shall have procedures in place to ensure that newly manufactured aircraft are maintained in accordance with the applicable maintenance instructions and are kept in an airworthy condition and, if applicable, that a certificate of release to service is issued for any maintenance that has been completed. |
(f) |
If the declared production organisation holds (an)other organisation certificate(s) issued on the basis of Regulation (EU) 2018/1139 and the delegated and implementing acts adopted on the basis thereof, the production organisation may integrate the production management system with the management system that is required for the issuance of the other certificate(s). |
21L.A.125 Resources of the declared production organisation
The declared production organisation shall ensure that:
(a) |
the facilities, working conditions, equipment and tools, processes and associated materials, the number and competence of staff, and the general organisation are adequate to discharge its obligations under point 21L.A.127; |
(b) |
with regard to all necessary airworthiness and environmental protection data:
|
(c) |
with regard to management and staff:
|
(d) |
with regard to certifying staff, authorised by the declared production organisation to sign the documents issued under point 21L.A.126 within the scope of declared production activities:
|
21L.A.126 Scope of work
(a) |
A declared production organisation is entitled to show the conformity of the products and parts that are within the scope of this Section and that it has produced within the declared scope of work, with the applicable design data. |
(b) |
A declared production organisation is entitled, for a complete aircraft, after presentation of an aircraft statement of conformity (EASA Form 52B), to apply:
|
(c) |
A declared production organisation is entitled to issue authorised release certificates (EASA Form 1) for engines, propellers and parts that either conform to:
|
(d) |
A declared production organisation is entitled to recommend the conditions for an aircraft that it has produced and for which it has attested conformity with the applicable design data, under which a permit to fly can be issued by the competent authority under Subpart P of Annex I (Part 21). |
(e) |
A declared production organisation is entitled to maintain a new aircraft that it has produced, as necessary to keep it in an airworthy condition, unless Regulation (EU) No 1321/2014 requires the maintenance to be performed under such rules, and to issue a certificate of release to service (EASA Form 53B) in respect of that maintenance. |
21L.A.127 Obligations of the declared production organisation
(a) |
The declared production organisation shall work in accordance with clearly defined procedures, practices and processes. |
(b) |
If the declared production organisation intends to conduct flight tests, then it shall prepare, maintain and keep updated an operations manual that includes a description of the organisation’s policies and processes for flight testing. The declared production organisation shall make this manual available to the competent authority upon request. |
(c) |
For completed aircraft, prior to submitting an aircraft statement of conformity (EASA Form 52B) to the competent authority, the declared production organisation shall ensure that the aircraft is in a condition for safe operation and conforms to:
|
(d) |
For products (other than complete aircraft) and parts, the declared production organisation shall ensure prior to issuing an authorised release certificate (EASA Form 1) that the product or part is in a condition for safe operation and conforms to the approved type design of a type-certified product issued in accordance with Subpart B, D, E or M of Section B of this Annex or conforms to the design data of an aircraft for which design compliance has been declared in accordance with Subpart C, F or M of this Annex. |
(e) |
For engines, the declared production organisation shall ensure that the completed engine is in compliance with the applicable engine exhaust emissions requirements applicable on the date of production of the engine. |
(f) |
The declared production organisation shall include, in any authorised release certificates (EASA Form 1) that are issued by it, the reference number issued by the competent authority in accordance with point 21L.B.142 for this declared production organisation. |
(g) |
The declared production organisation shall ensure that the organisation records the details of any work that is completed. |
(h) |
The declared production organisation shall provide, to the design holder or the declarant of a declaration of design compliance, continuing airworthiness support for any products or parts that they have produced. |
(i) |
The declared production organisation shall have an archiving system that records the requirements that have been placed on other organisations, such as suppliers and subcontractors. The declared production organisation shall make the archived data available to the competent authority for continuing airworthiness purposes. |
(j) |
For the production of new aircraft, the declared production organisation shall ensure that the aircraft is kept in an airworthy condition and that maintenance is performed, including any necessary repairs in accordance with the applicable design data, prior to the issuance of an aircraft statement of conformity (EASA Form 52B). |
(k) |
Where the declared production organisation issues a certificate of release to service after such maintenance, it shall determine that each completed aircraft has been subjected to the necessary maintenance and is in a condition for safe operation, prior to issuing that certificate. |
(l) |
The declared production organisation shall comply with the requirements in Subpart A of this Annex applicable to a declared production organisation. |
21L.A.128 Notification of changes and cessation of activities
The declared production organisation shall notify the competent authority without undue delay of the following:
(a) |
any changes to the information that has been declared in accordance with point (c) of point 21L.A.123; |
(b) |
any changes to the management system for production that are significant to the showing of conformity or to the airworthiness and environmental compatibility characteristics of the product or part; |
(c) |
the cessation of some of or all the activities covered by the declaration. |
SUBPART H – CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS
21L.A.141 Scope
This Subpart establishes the procedure for applying for a certificate of airworthiness or a restricted certificate of airworthiness for an aircraft whose design has been certified or declared in accordance with this Annex, and establishes the rights and obligations of the applicants for, and holders of, those certificates.
21L.A.142 Eligibility
Any natural or legal person under whose name an aircraft is registered or will be registered in a Member State (‘Member State of registry’) may apply for a certificate of airworthiness or for a restricted certificate of airworthiness for that aircraft under the conditions laid down in this Subpart.
21L.A.143 Application for a certificate of airworthiness or a restricted certificate of airworthiness
(a) |
A natural or legal person shall apply for a certificate of airworthiness or a restricted certificate of airworthiness in a form and manner established by the competent authority of the Member State of registry. |
(b) |
A natural or legal person may apply for:
|
(c) |
For a new aircraft that conforms to a type certificate issued by the Agency, the applicant shall include in the application:
|
(d) |
For a new aircraft that conforms to a declaration of design compliance which is registered by the Agency, the applicant shall include in the application:
|
(e) |
For a used aircraft originating from a Member State, the applicant shall include in the application an airworthiness review certificate issued in accordance with Annex I (Part-M) or Annex Vb (Part-ML) to Regulation (EU) No 1321/2014. |
(f) |
For a used aircraft originating from a non-Member State, the applicant shall include in the application:
|
(g) |
Unless otherwise agreed, the statements referred to in points (c)(1), (d)(1) and (f)(1) shall be issued no more than 60 days before the presentation of the aircraft to the competent authority of the Member State of registry. |
21L.A.144 Obligations of the applicant for a certificate of airworthiness or a restricted certificate of airworthiness
The applicant for a certificate of airworthiness or for a restricted certificate of airworthiness shall:
(a) |
present the manuals, placards, listings, and instrument markings and other necessary information required by the applicable type-certification basis or by the applicable detailed technical specifications for declarations of design compliance in one or more of the official language(s) of the European Union acceptable to the competent authority of the Member State of registry; |
(b) |
demonstrate that their aircraft is identified in accordance with Subpart Q of this Annex; |
(c) |
arrange for inspections of the competent authority of the Member State of registry to assess whether the aircraft has any non-conformities that could affect the safety of the aircraft. |
21L.A.145 Transferability and re-issuance of a certificate of airworthiness and of a restricted certificate of airworthiness within Member States
Where the ownership of an aircraft has changed:
(a) |
if it remains on the same register, the certificate of airworthiness, or the restricted certificate of airworthiness issued in accordance with Subpart H of Section B of this Annex, shall be transferred together with the aircraft; |
(b) |
if the aircraft is intended to be registered in another Member State, the natural or legal person under whose name the aircraft will be registered shall apply to the competent authority of the new Member State of registry for a new certificate of airworthiness or a restricted certificate of airworthiness and shall include in this application the former certificate of airworthiness or restricted certificate of airworthiness issued in accordance with Subpart H of Section B of this Annex and a valid airworthiness review certificate issued in accordance with Annex I (Part-M) or Annex Vb (Part-ML) to Regulation (EU) No 1321/2014. |
21L.A.146 Continued validity of a certificate of airworthiness and of a restricted certificate of airworthiness
(a) |
A certificate of airworthiness or a restricted certificate of airworthiness shall remain valid as long as:
|
(b) |
Upon surrender or revocation, the certificate shall be returned to the competent authority of the Member State of registry. |
SUBPART I – NOISE CERTIFICATES AND RESTRICTED NOISE CERTIFICATES
21L.A.161 Scope
This Subpart establishes the procedure for applying for a noise certificate or a restricted noise certificate for an aircraft whose design has been certified or declared in accordance with this Annex and establishes the rights and obligations of the applicants for, and holders of, those certificates.
21L.A.162 Eligibility
Any natural or legal person under whose name an aircraft is registered or will be registered in a Member State may apply for a noise certificate or a restricted noise certificate for that aircraft under the conditions laid down in this Subpart.
21L.A.163 Application
(a) |
A natural or legal person shall apply for a noise certificate or a restricted noise certificate in a form and manner established by the competent authority of the Member State of registry. |
(b) |
A natural or legal person may apply for:
|
(c) |
The applicant shall include in the application:
|
(d) |
Unless otherwise agreed, the statements referred to in point (c)(1)(i) shall be issued no more than 60 days before the presentation of the aircraft to the competent authority of the Member State of registry. |
21L.A.164 Transferability and re-issuance of noise certificates and restricted noise certificates within Member States
Where the ownership of an aircraft has changed:
(a) |
if the aircraft remains on the same register, the noise certificate, or the restricted noise certificate issued in accordance with Subpart I of Section B of this Annex, shall be transferred together with the aircraft; |
(b) |
if the aircraft is intended to be registered in another Member State, the natural or legal person under whose name the aircraft will be registered shall apply to the competent authority of the new Member State of registry for a new noise certificate or restricted noise certificate and shall include in this application the former noise certificate or restricted noise certificate issued in accordance with Subpart I of Section B of this Annex. |
21L.A.165 Continued validity of a noise certificate and of a restricted noise certificate
(a) |
A noise certificate or a restricted noise certificate shall remain valid as long as:
|
(b) |
Upon surrender or revocation, the certificate shall be returned to the competent authority of the Member State of registry. |
SUBPART J – DECLARED DESIGN ORGANISATIONS
21L.A.171 Scope
This Subpart establishes:
(a) |
the procedure for declaring the design capability by natural and legal persons who design products under this Section; and |
(b) |
the rights and obligations of the persons making declarations of design capability referred to in point (a). |
21L.A.172 Eligibility
Any natural or legal person (‘organisation’ in this Subpart) required by point 21L.A.22, point 21L.A.82 or point 21L.A.204 to demonstrate their design capability may declare their capability under the conditions laid down in this Subpart.
21L.A.173 Declaration of design capability
(a) |
Prior to or at the same time as applying for a design approval under this Section, or prior to submitting the application for the approval of flight conditions in accordance with point 21.A.710 of Annex I (Part 21) of a product designed by it, whatever comes first, the organisation shall submit a declaration of design capability to the Agency. |
(b) |
The declaration, and any subsequent changes thereto, shall be made in a form and manner established by the Agency. |
(c) |
The declaration shall include the information necessary for the Agency to become familiar with the organisation and the intended scope of work, and shall include at least the following:
|
(d) |
The declaration of design capability shall be submitted to the Agency. |
21L.A.174 Management system for design
(a) |
The declared design organisation shall establish, implement, and maintain a management system for design with clear accountability and lines of responsibility throughout the organisation that:
|
(b) |
The declared design organisation shall have, as part of their management system for design, a means to provide design assurance by establishing, implementing and maintaining a system for the control and supervision of the design, and of design changes and repairs, of products. This system shall:
|
(c) |
The declared design organisation shall establish, as part of their management system for design, an independent function to monitor the compliance of the organisation with the relevant requirements, and compliance with, and adequacy of, the management system for design. This monitoring shall include a system to provide feedback to the person or a group of persons referred to in point (b) of point 21L.A.175, and to the accountable manager referred to in point (a) of point 21L.A.175 to ensure, as necessary, corrective action. |
(d) |
The declared design organisation shall establish, maintain and keep updated processes and procedures that ensure the design compliance of products with the applicable type-certification basis, applicable detailed technical specifications and applicable environmental protection requirements. The declared design organisation shall make documentary evidence of these processes and procedures available to the Agency upon request. |
(e) |
Where any parts or any changes to the products are designed by partner organisations or subcontractors, the processes and procedures in point (d) shall include a description of how the design organisation is able to give, for all parts, the assurance of compliance required by point (b)(2), and shall contain, directly or by cross-reference, descriptions and information on the design activities and organisation of those partners or subcontractors. |
(f) |
If the declared design organisation holds (an)other organisation certificate(s) issued on the basis of Regulation (EU) 2018/1139 and the delegated and implementing acts adopted on the basis thereof, the declared design organisation may integrate the design management system with the management system that is required for the issuance of the other certificate(s). |
21L.A.175 Resources of the declared design organisation
(a) |
The declared design organisation shall nominate a head of the design organisation with the authority for ensuring that, within the organisation, all design activities are performed to the required standards and that the declared design organisation is continuously in compliance with the requirements for the management system for design referred to in points (a) to (c) of point 21L.A.174 and the processes and procedures referred to in point (d) of point 21L.A.174. |
(b) |
The head of the design organisation shall nominate and identify key personnel within the organisation that are responsible for:
|
(c) |
The person or group of persons identified in point (b) shall:
|
(d) |
The declared design organisation shall ensure that:
|
(e) |
The declared design organisation shall document the organisational structure of their organisation, along with the key personnel who are responsible for ensuring that the organisation is in compliance with this Subpart, keep them updated and make them available to the Agency upon request. |
21L.A.176 Scope of work
The declared design organisation shall identify the types of design work, the categories of products for which design activities are conducted, and the functions and duties that the organisation performs in regard to the airworthiness and environmental compatibility of products.
21L.A.177 Obligations of the declared design organisation
A declared design organisation shall:
(a) |
work in accordance with clearly defined procedures, practices and processes; |
(b) |
if the declared design organisation intends to conduct flight testing, maintain and keep updated an operations manual that provides a description of the organisation’s policies and processes for flight testing and make this manual available to the Agency upon request; |
(c) |
determine whether the designs of products, including changes and repairs, do not have any unsafe features and comply with the applicable type-certification basis, and with the applicable environmental protection requirements, and provide the Agency with statements/documentation confirming this; |
(d) |
provide the Agency with information or instructions relating to continued airworthiness actions; |
(e) |
comply with the requirements in Subpart A of this Annex applicable to declared design organisations. |
21L.A.178 Notification of changes and cessation of activities
The declared design organisation shall notify the Agency without undue delay of the following:
(a) |
any changes to the information that has been declared in accordance with point (c) of point 21L.A.173; |
(b) |
changes to the management system for design that are significant for the demonstration of compliance of the product designed by them; |
(c) |
the cessation of some or all of the activities covered by the declaration. |
SUBPART K – PARTS
21L.A.191 Scope
This Subpart establishes how the compliance of parts with the airworthiness requirements shall be shown.
21L.A.192 Showing of compliance
(a) |
The showing of compliance with the airworthiness requirements of parts to be installed in a type-certified product or an aircraft for which design compliance has been declared shall be made:
|
(b) |
In all cases where the approval of a part is explicitly required by Union law or Agency measures, the part shall comply with the applicable ETSO or with the specifications recognised as equivalent by the Agency in the particular case. |
21L.A.193 Release of parts for installation
(a) |
A part or product shall only be installed in a product when it is identified by the holder of a type certificate, supplemental type certificate, design change, repair design approval or with a declaration of design compliance as being suitable for installation, and when it is:
|
(b) |
By way of derogation from point (a)(3) and provided that the conditions in point (c) are met, the following parts do not require an authorised release certificate (EASA Form 1) in order to be installed in a type-certified product or in an aircraft for which design compliance has been declared:
|
(c) |
Parts listed in point (b) are eligible for installation in a type-certified product or in an aircraft for which design compliance has been declared 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, which declares the name of the part, the part number, and the conformity of the part with its design data, and which contains the date of issuance. |
SUBPART M – DESIGN OF REPAIRS TO TYPE-CERTIFIED PRODUCTS
21L.A.201 Scope
This Subpart establishes:
(a) |
the procedure for applying for the approvals of repair designs to type-certified products; |
(b) |
the rights and obligations of the applicants for, and holders of, those approvals referred to in point (a); |
(c) |
provisions for standard repairs that do not require an approval. |
21L.A.202 Standard repairs
(a) |
Standard repairs are repair designs to a type-certified product approved in accordance with Subpart B of Section B of this Annex and which:
|
(b) |
Points 21L.A.203 to 21L.A.211 are not applicable to standard repairs. |
21L.A.203 Classification of repair designs to a type-certified product
(a) |
Repair designs to a type-certified product shall be classified as minor or major. |
(b) |
A ‘minor repair’ is a repair design that has no appreciable effect on the mass, balance, structural strength, reliability, certified noise or emissions level, operational characteristics, or other characteristics affecting the airworthiness or the environmental compatibility of the product. |
(c) |
All other repair designs are ‘major repairs’. |
(d) |
The requirements for the approval of minor repair designs are those established in point 21L.A.207. |
(e) |
The requirements for the approval of major repair designs are those established in point 21L.A.208. |
21L.A.204 Eligibility
(a) |
Any natural or legal person who has demonstrated, or is in the process of demonstrating, their design capability in accordance with point 21L.A.23, may apply for the approval of a major repair design to a type-certified product under the conditions laid down in this Subpart. |
(b) |
Any natural or legal person may apply for the approval of a minor repair design to a type-certified product under the conditions laid down in this Subpart. |
21L.A.205 Application for the approval of a repair design to a type-certified product
(a) |
An application for an approval of a repair design to a type-certified product shall be made in a form and manner established by the Agency. |
(b) |
For the approval of a major repair design, the applicant shall include in the application, or submit after the initial application, a compliance demonstration plan:
|
21L.A.206 Demonstration of compliance
(a) |
The applicant for the approval of a major repair design shall demonstrate compliance with the applicable type-certification basis and applicable environmental protection requirements as established and notified to the applicant by the Agency in accordance with point 21L.B.201 and shall provide the Agency with the means by which such compliance has been demonstrated. |
(b) |
The applicant for the approval of a major repair design shall provide the Agency with a recorded justification of the means of compliance within compliance documents according to the compliance demonstration plan. |
(c) |
When carrying out testing and inspections to demonstrate compliance in accordance with point (a), the applicant shall have verified and documented this verification prior to carrying out any test:
|
(d) |
The flight testing for the purpose of obtaining an approval of a major repair design shall be conducted in accordance with methods for such flight testing specified by the Agency. The applicant shall make all the flight tests necessary to determine compliance with the applicable type-certification basis and the applicable environmental protection requirements. |
(e) |
An applicant for the approval of a major repair design shall allow the Agency to:
|
(f) |
Upon completion of the compliance demonstration, the applicant shall declare to the Agency that:
|
21L.A.207 Requirements for the approval of a minor repair design
In order to be issued with an approval of a minor repair design to a type-certified product, the applicant shall:
(a) |
demonstrate that the repair design and the areas affected by the repair design comply:
|
(b) |
declare compliance with the type-certification basis and the applicable environmental protection requirements that apply in accordance with point (a)(1), or with the certification specifications chosen in accordance with point (a)(2), record the justifications of compliance in the compliance documents, and record that no feature or characteristic has been identified that may make the changed product unsafe or environmentally incompatible for the uses for which certification is requested; |
(c) |
submit to the Agency the justification of compliance for the repair and the declaration of compliance. |
21L.A.208 Requirements for the approval of a major repair design
In order to be issued with an approval of a major repair design to a type-certified product, the applicant shall:
(a) |
demonstrate that the repair design and the areas affected by the repair design comply with the type-certification basis and the applicable environmental protection requirements as established and notified to the applicant by the Agency in accordance with point 21L.B.201; |
(b) |
demonstrate compliance in accordance with point 21L.A.206; |
(c) |
if the applicant has specified that they provided certification data on the basis of an arrangement with the owner of the type-certification data in accordance with point 21L.A.205(b)(5), demonstrate that the type-certificate holder:
|
(d) |
demonstrate that there are no unresolved issues from the physical inspection of the first article of that product with the repair design in the final changed configuration carried out by the Agency in accordance with point 21L.A.206(e)(3). |
21L.A.209 Approval of a repair design under a privilege
(a) |
The approval of a repair design that it has designed may be issued by an approved design organisation without an application according to point 21L.A.205 in accordance with the scope of its privileges provided for in points (2) and (5) of point 21.A.263(c) of Annex I (Part 21) instead of the Agency, as recorded in the terms of approval. |
(b) |
When issuing a repair approval in accordance with point (a), the design organisation shall:
|
21L.A.210 Obligations of a holder of a repair design approval
The holder of a repair design approval shall:
(a) |
if they are not the type-certificate or supplemental type-certificate holder, and certification data has been supplied in accordance with 21L.A.205 (b)(5), establish an arrangement with the relevant holder; |
(b) |
provide to the organisation performing the repair all the necessary instructions to install or embody the repair design; |
(c) |
support any production organisation producing parts for the repair design, and ensure that those parts are produced using production data that is based upon the design data that is provided by the repair design approval holder; |
(d) |
ensure that the repair design includes all the necessary instructions and limitations, if a repair design is approved subject to limitations. These instructions and limitations shall be transmitted to the operator by the holder of the repair design approval in accordance with a procedure agreed with the Agency; |
(e) |
undertake the obligations of a repair design approval holder of Subpart A of this Annex. |
21L.A.211 Unrepaired damage
Damage to a product, the design of which has been approved in accordance with Section B, may not require a repair design if an evaluation of the airworthiness consequences justifies it. Such an evaluation is to be made by either the Agency or by a design organisation which is appropriately approved in accordance with Subpart J of Section A of Annex I (Part 21), under a procedure accepted by the Agency. If the evaluation concludes that the unrepaired damage requires limitations, those shall be processed in accordance with point (d) of point 21L.A.210.
SUBPART N – DESIGN OF REPAIRS TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED
21L.A.221 Scope
This Subpart establishes:
(a) |
the procedure for declaring the compliance of repair designs to an aircraft which was subject to a declaration made in accordance with Subpart C of this Annex; |
(b) |
the rights and obligations of the declarant making a declaration of compliance of the change referred to in point (a); |
(c) |
provisions regarding the standard repairs that do not require a declaration of design compliance. |
21L.A.222 Standard repairs
(a) |
Standard repairs are repair designs to an aircraft which was subject to a declaration made in accordance with Subpart C of this Annex and which:
|
(b) |
Points 21L.A.223 to 21L.A.229 are not applicable to standard repairs. |
21L.A.223 Classification of repair designs to an aircraft for which design compliance has been declared
(a) |
Repair designs to an aircraft which was subject to a declaration made in accordance with Subpart C of this Annex shall be classified as either a major or minor, using the criteria laid down in points (b) and (c) of 21L.A.203. |
(b) |
The design compliance of a minor repair design shall be declared in accordance with point 21L.A.225. |
(c) |
The design compliance of a major repair design shall be declared in accordance with point 21L.A.226. |
21L.A.224 Eligibility
(a) |
A declarant who made a declaration of aircraft design compliance in accordance with Subpart C of this Annex may declare compliance of a minor repair design of that aircraft under the conditions laid down in this Subpart. In addition, such a declaration of compliance may be also made, under the conditions laid down in this Subpart, by a design organisation approved in accordance with point (c)(3) of point 21.A.263 of Annex I (Part 21). |
(b) |
Only the declarant who made a declaration of aircraft design compliance in accordance with Subpart C of this Annex may declare the compliance of a major repair design to an aircraft for which design compliance has been declared in accordance with Subpart C of this Annex, under the conditions laid down in this Subpart. |
(c) |
By derogation from point (b), if the declarant who made a declaration of aircraft design compliance in accordance with Subpart C of this Annex is no longer active or is unresponsive to requests for repair designs, the compliance of a changed aircraft design may also be declared in accordance with Subpart C of this Annex by a design organisation approved in accordance with point (c)(2) of point 21.A.263 of Annex I (Part 21) within the scope of their terms of approval, or by any other natural or legal person who is able to undertake the obligations laid down in point 21L.A.47 with respect to that changed aircraft. |
21L.A.225 Declaration of design compliance for minor repair designs
(a) |
Prior to incorporating or embodying or agreeing with a production organisation to incorporate or embody a minor repair design to an aircraft for which design compliance has been declared in accordance with Subpart C of this Annex, the declarant or the organisation that has designed the minor repair shall declare that the minor repair design complies with the detailed technical specifications and the applicable environmental protection requirements with which compliance had been declared according to point 21L.A.43. |
(b) |
The declaration of design compliance shall be made in a form and manner established by the Agency. |
(c) |
The declarant or the organisation that has designed the minor change shall maintain a register of minor repair designs to aircraft for which design compliance has been declared, and make any declaration made in accordance with point (a) available to the Agency upon request. |
21L.A.226 Declaration of design compliance of major repair designs
(a) |
Prior to incorporating or embodying or agreeing with a production organisation to incorporate or embody a major repair design to an aircraft for which design compliance has been declared in accordance with Subpart C of this Annex, the declarant shall declare that the design of the major repair complies with the detailed technical specifications and the applicable environmental protection requirements with which compliance had been declared according to point 21L.A.43. |
(b) |
The declaration of design compliance shall be made in a form and manner established by the Agency. |
(c) |
The declaration shall contain at least the following information:
|
(d) |
The declarant that designs a major repair shall submit the declaration referred to in point (c) to the Agency. Together with this declaration, the declarant shall provide to the Agency:
|
(e) |
The declaration of a major repair to a declaration of design compliance shall be limited to the specific configuration(s) in the declaration of design compliance to which the change relates. |
21L.A.227 Compliance activities for declaring compliance of a major repair design
Prior to making a declaration of compliance in accordance with point 21L.A.226, the declarant shall, for that specific design:
(a) |
establish a compliance demonstration plan detailing the means for compliance demonstration that shall be followed during the compliance demonstration. This document shall be updated as necessary; |
(b) |
record the justification of compliance within compliance documents according to the compliance demonstration plan; |
(c) |
perform testing and inspections as necessary in accordance with the compliance demonstration plan; |
(d) |
ensure and record the conformity of the test articles and equipment and ensure that the test specimen conforms to the specifications, drawings, manufacturing processes, construction and assembly means in the design; |
(e) |
ensure that the test and measuring equipment to be used for testing are adequate for testing and appropriately calibrated; |
(f) |
allow the Agency to conduct or participate in any inspections or tests of aircraft in the final or suitably mature design and production configuration that are necessary to determine that the product with the repair design has no feature or characteristic that makes the aircraft unsafe or environmentally incompatible for the intended use; |
(g) |
carry out flight testing, in accordance with the flight conditions for such flight testing specified by the Agency, as necessary in order to determine that the aircraft complies with the applicable detailed technical specifications and the applicable environmental protection requirements. |
21L.A.228 Obligations of the declarant of a declaration of design compliance of a repair design
The declarant of a declaration of design compliance shall:
(a) |
for minor repair designs maintain a register of those declarations and shall make those declarations available to the Agency upon request; |
(b) |
provide to the organisation performing the repair all the necessary instructions to install or embody the repair design; |
(c) |
support any production organisation producing parts for the repair design, and ensure that those parts are produced using production data that is based upon the design data that is provided by the declarant; |
(d) |
if a repair design is declared subject to limitations, transmit these limitations to the operator using a documented procedure that is made available to the Agency upon request; |
(e) |
undertake the obligations of a declarant of design compliance of a repair design of Subpart A of this Annex. |
21L.A.229 Unrepaired damage
The declarant of design compliance of an aircraft in accordance with Subpart C of this Annex or an approved design organisation with privileges provided in accordance with point (c)(3) of point 21.A.263 of Annex I (Part 21) and with the appropriate scope of approval shall conduct an evaluation of the airworthiness and environmental compatibility consequences of any damage to such aircraft that is left unrepaired and that is not covered by previously declared data. Any necessary limitations shall be processed in accordance with point (d) of point 21L.A.228.
SUBPART O – EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS
(Reserved)
SUBPART P – PERMIT TO FLY
21L.A.241 Permit to fly and flight conditions
(a) |
The procedures for applying for the issuance of permits to fly and related flight conditions for aircraft within the scope of this Annex shall be those established in Subpart P of Section A of Annex I (Part 21) and those established in points (b) and (c) of point 21L.A.241. |
(b) |
When applying for a permit to fly in accordance with point 21.A.707 of Annex I (Part 21), the applicant shall arrange for the competent authority to conduct a conformity inspection of the aircraft when the application for a permit to fly relates to:
|
(c) |
When applying for flight conditions in accordance with point 21.A.709 of Annex I (Part 21), the applicant shall arrange for the Agency:
|
SUBPART Q – IDENTIFICATION OF PRODUCTS AND PARTS
21L.A.251 Scope
This Subpart establishes the requirements for the identification of products and parts designed and produced under this Annex.
21L.A.252 Design of markings
(a) |
The holder of a type certificate, supplemental type certificate, approval of a change to type certificate or approval of a repair design, or the declarant of a declaration of design compliance shall specify in the design data the marking of products and parts designed in accordance with this Annex. |
(b) |
The specifications of the marking shall include the following information:
|
(c) |
The specification of parts in accordance with point (ii) of point (b)(2) shall include the letter ‘(R)’ at the end of the part number when:
|
21L.A.253 Identification of products
(a) |
Any natural or legal person who produces products under Subpart G of Section A of Annex I (Part 21) or under Subpart G or R of this Annex for which the design has been approved or declared in accordance with this Annex shall identify that product as specified in accordance with 21L.A.252 by means of a fireproof marking on a fireproof plate. |
(b) |
The identification plate shall be secured in such a manner that it is accessible and legible, and will not likely be defaced or removed during normal service, or lost or destroyed in an accident, and in the case of a propeller, propeller blade, or propeller hub, placed on a non-critical surface of the item. |
(c) |
For manned balloons, the identification plate shall be secured to the balloon envelope and shall be located, if practicable, where it is legible to the operator when the balloon is inflated. In addition, the basket, load frame assembly and any heater assembly shall be permanently and legibly marked with the name of the production organisation, part number, or its equivalent, and the serial number, or its equivalent. |
21L.A.254 Handling of identification data
(a) |
Any natural or legal person performing maintenance work in accordance with Regulation (EU) No 1321/2014 may, in accordance with methods, techniques and practices established by the Agency:
|
(b) |
Unless for the purposes stated in point (a) of point 21L.A.254, no person shall remove, change, or place the identification information referred to in point (a) of point 21L.A.253. |
(c) |
Unless for the purposes stated in point (a) of point 21L.A.254, no person shall remove or install any identification plate referred to in point (a) of point 21L.A.253. |
(d) |
No person shall install an identification plate removed in accordance with point (a)(2) on any aircraft, engine, propeller, propeller blade, or propeller hub other than the one from which it was removed. |
21L.A.255 Identification of parts
Any natural or legal person who produces parts under Subpart G of Section A of Annex I (Part 21) or under Subpart G or R of this Annex for a product for which the design has been approved or declared in accordance with this Annex shall permanently and legibly mark that part as specified in accordance with point 21L.A.252.
SUBPART R – STATEMENT OF CONFORMITY FOR AIRCRAFT AND AUTHORISED RELEASE CERTIFICATE (EASA FORM 1) FOR ENGINES AND PROPELLERS, OR PARTS THEREOF, WHICH CONFORM TO A DECLARATION OF DESIGN COMPLIANCE
21L.A.271 Scope
This Subpart establishes the procedures for the issuance of statements of conformity for aircraft (EASA Form 52B) and authorised release certificates (EASA Form 1) for engines and propellers, or parts thereof, that have been produced in conformity with the design data of a declaration of design compliance, and the rights and obligations of the declarant.
21L.A.272 Eligibility
Any natural or legal person who is granted access to the applicable design data and is able to undertake the obligations stated in point 21L.A.275 may issue a statement of conformity (EASA Form 52B) for an aircraft or an authorised release certificate (EASA Form 1) for an engine or propeller, or a part thereof, under the conditions laid down in this Subpart.
21L.A.273 Production control system
A natural or legal person issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1) with the applicable declared design data of an aircraft, engine or propeller, or a part thereof, that they have produced, shall establish, implement and maintain a system for controlling production that:
(a) |
includes processes and procedures that ensure that the aircraft, engine or propeller, and any part thereof, conforms with the applicable declared design data; |
(b) |
ensures that each statement of conformity (EASA Form 52B) or authorised release certificate (EASA Form 1) is only signed by authorised persons; |
(c) |
if flight tests are necessary within the scope of production, has processes in place that ensure that any flight tests are conducted in a safe manner; |
(d) |
ensures that the natural or legal person is in receipt of all the necessary airworthiness and environmental compatibility data to determine conformity; |
(e) |
has procedures in place that ensure that the airworthiness and environmental compatibility data is correctly incorporated in its production data, kept up to date and made available to all the personnel who need access to such data to perform their duties; |
(f) |
includes an inspection system that ensures that any aircraft, engine or propeller, and any part thereof, that are produced by the natural or legal person including their partners, or are supplied from or subcontracted to outside parties, conform with the applicable declared design data and are in a condition for safe operation; |
(g) |
includes an archiving system that records the requirements that have been placed on other organisations such as suppliers and subcontractors. The archived data shall be made available to the competent authority for continuing airworthiness purposes; |
(h) |
ensures that the maintenance of a newly manufactured aircraft is conducted in accordance with the applicable maintenance instructions and that the aircraft is kept in an airworthy condition, and if applicable, a certificate of release to service is issued for any maintenance that has been completed; |
(i) |
includes an internal occurrence reporting system in the interest of safety, to enable the collection and assessment of the occurrence reports collected in accordance with point 21L.A.3 in order to identify adverse trends or to address deficiencies, and to extract reportable occurrences. This system shall include the evaluation of relevant information relating to occurrences and the promulgation of the related information. |
21L.A.274 Issuance of a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1)
(a) |
When issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1), the natural or legal person shall include all of the following:
|
(b) |
The natural or legal person shall issue a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1) upon:
|
21L.A.275 Obligations of a natural or legal person issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1)
The natural or legal person issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1) shall:
(a) |
inform the competent authority that they intend to produce an aircraft, engine or propeller, or a part thereof, in conformity with the design data of a declaration of design compliance and that they will issue statements of conformity (EASA Form 52B) or authorised release certificates (EASA Form 1) in accordance with this Subpart; |
(b) |
ensure that the details of any completed work are recorded; |
(c) |
maintain, at the place of production, the technical data and drawings necessary to determine whether the aircraft, engine or propeller, or a part thereof, conforms to the applicable declared design data; |
(d) |
provide continuing airworthiness support to the declarant of a declaration of design compliance for any aircraft, engine or propeller, or a part thereof, that they have produced; |
(e) |
for new aircraft that they have produced, ensure that the aircraft is kept in an airworthy condition and that maintenance is performed, unless Regulation (EU) No 1321/2014 requires the maintenance to be performed under such rules, including any necessary repairs in accordance with the applicable design data prior to the issuance of an aircraft statement of conformity (EASA Form 52B); |
(f) |
when issuing a certificate of release to service after such maintenance, determine that each completed aircraft has been subjected to the necessary maintenance and is in a condition for safe operation, prior to issuing the certificate; |
(g) |
undertake the obligations of a natural or legal person issuing statements of conformity (EASA Form 52B) or authorised release certificates (EASA Form 1) of Subpart A of this Annex; |
(h) |
inform the competent authority about the cessation of their activities under this Subpart. |
SECTION B
PROCEDURES FOR COMPETENT AUTHORITIES
SUBPART A – GENERAL PROVISIONS
(reserved)
SUBPART B – TYPE CERTIFICATES
21L.B.41 Certification specifications
The Agency, in accordance with Article 76(3) of Regulation (EU) 2018/1139, shall issue certification specifications and other detailed specifications, including certification specifications for airworthiness, and environmental compatibility that competent authorities, organisations and personnel may use to demonstrate the compliance of products and parts with the relevant essential requirements set out in Annexes II, IV and V to that Regulation, as well as with those for environmental protection set out in Article 9(2) of and Annex III to that Regulation. Such specifications shall be sufficiently detailed and specific to indicate to applicants the conditions under which certificates are to be issued, amended or supplemented.
21L.B.42 Initial investigation
(a) |
Upon receiving an application for a type certificate under this Annex, the Agency shall verify whether the product is within the scope established in point 21L.A.21 and whether the applicant is eligible in accordance with point 21L.A.22 to apply for a type certificate for the product. |
(b) |
When the conditions of point (a) are not fulfilled, the Agency shall reject the application. |
21L.B.43 Type-certification basis for a type certificate
(a) |
The Agency shall establish the type-certification basis and notify it to the applicant. The type-certification basis shall consist of:
|
(b) |
The Agency may amend the type-certification basis at any point before the issuance of the type certificate if it has determined that experience from other similar products in service, or products that have similar design features, has shown that unsafe conditions may develop, and the type-certification basis that was established and notified to the applicant does not address this unsafe condition. |
21L.B.44 Special conditions
(a) |
The Agency shall prescribe special detailed technical specifications, named ‘special conditions’, for a product if the related certification specifications do not contain adequate or appropriate safety standards for the product because:
|
(b) |
Special conditions contain such safety standards as the Agency finds necessary in order to establish a level of safety equivalent to that of the applicable certification specifications. |
21L.B.45 Designation of the applicable environmental protection requirements for a type certificate
The Agency shall designate and notify to the applicant for a type certificate for an aircraft or for an engine, the applicable environmental requirements in accordance with point 21.B.85 of Annex I (Part 21).
21L.B.46 Investigation
Upon receiving an application for a type certificate under this Annex, the Agency shall:
(a) |
conduct a review of the initial compliance demonstration plan and any subsequent update provided by the applicant in order to establish the completeness of the plan and the appropriateness of the proposed means and methods of demonstrating compliance with the type-certification basis established in accordance with point 21L.B.43 and with the applicable environmental protection requirements designated in accordance with point 21L.B.45; if the compliance demonstration plan is incomplete or the means and methods are not appropriate to achieve compliance demonstration, the Agency shall inform the applicant and request an amendment of it; |
(b) |
when satisfied that the compliance demonstration plan provided is appropriate so that the applicant can demonstrate compliance, approve the compliance demonstration plan and any subsequent updates of the compliance demonstration plan; |
(c) |
after receiving the declaration of compliance in accordance with point (f) of point 21L.A.25, conduct a physical inspection and assessment of the first article of that product in the final configuration, taking into consideration the critical design review carried out in accordance with point (a) of point 21L.B.242, in order to verify the compliance of the product with the applicable type-certification basis and the applicable environmental protection requirements; the Agency shall verify the compliance of the product, considering the likelihood of an unidentified non-compliance with the type-certification basis or the applicable environmental protection requirements, and the potential impact of that non-compliance on the safety or environmental compatibility of the product; |
(d) |
if during the establishment of the type-certification basis, designation of the applicable environmental protection requirements or during the review of the compliance demonstration plan the Agency determines that the product design contains any element for which an unidentified non-compliance with the type-certification basis or the applicable environmental protection requirements may have an adverse impact on the safety or environmental compatibility of the product, the Agency shall determine which investigations are necessary in addition to those described in point (c) in order to verify the compliance demonstration; the Agency shall notify the applicant of any additional investigations and which elements of the design would be subject to those investigations. |
21L.B.47 Issuance of a type certificate
(a) |
The Agency shall issue without undue delay an aircraft, engine or propeller type certificate, provided that:
|
(b) |
The type certificate shall include:
|
21L.B.48 Continuing airworthiness oversight of products for which a type certificate has been issued
If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means, detects a non-compliance with the type-certification basis or the applicable environmental protection requirements, the Agency shall raise a finding in accordance with point 21L.B.21, or issue an airworthiness directive under the conditions of point 21L.B.23.
21L.B.49 Transfer of a type certificate
(a) |
When the Agency receives an application for verification of whether a type certificate can be transferred by its holder in accordance with point 21L.A.29 or when the Agency considers a request to adopt a type certificate in accordance with point 21L.A.29, the Agency shall verify corresponding to points 21L.B.42 and 21L.B.46 whether the transferee is eligible to be a type-certificate holder in accordance with point 21L.A.22 and is able to undertake the obligations of a type-certificate holder under point 21L.A.28. |
(b) |
When the Agency concludes that the conditions referred to in point (a) are met by the transferee, it shall inform the type-certificate holder or the natural or legal person requesting to adopt a type certificate that a transfer of the type certificate to that natural or legal person is accepted by the Agency. |
SUBPART C – DECLARATIONS OF DESIGN COMPLIANCE
21L.B.61 Detailed technical specifications and applicable environmental protection requirements for declarations of product design compliance
(a) |
The Agency, in accordance with Article 76(3) of Regulation (EU) 2018/1139, shall establish and make available the detailed technical specifications that natural and legal persons can use to demonstrate compliance with the relevant essential requirements set out in Annex II to that Regulation when declaring compliance of the aircraft design in accordance with Subpart C of Section A of this Annex. |
(b) |
The detailed technical specifications referred to in point (a) shall provide design standards which reflect the state of the art and best design practices, and which build on the best available experience and scientific and technical progress, and on the best available evidence and analysis of aircraft design, for aircraft that are within the scope established under point 21L.A.41. These detailed technical specifications may include or refer to:
|
(c) |
For the purposes of ensuring the environmental compatibility of the design, the Agency shall establish and make available the environmental protection requirements to be used as the basis for the declaration of design compliance, which shall include:
|
21L.B.62 Initial oversight investigation
(a) |
Upon receiving a declaration of design compliance, the Agency shall verify that the aircraft is within the scope of Subpart C of Section A of this Annex and that the declaration contains all the information specified in point 21L.A.43. The Agency shall acknowledge the receipt of the declaration, including the assignment of an individual declaration of design compliance reference number to the declarant for that aircraft configuration. |
(b) |
The Agency shall conduct a physical inspection and assessment of the first article of that aircraft in the final configuration, taking into consideration the safety review carried out in accordance with point (a)(2) of point 21L.B.242. If the Agency finds evidence, in the declaration or through the physical inspection and assessment carried out in accordance with the first sentence, indicating that the aircraft could be incapable of conducting a safe flight or could be environmentally incompatible during in-service operations, the Agency shall raise a finding in accordance with point 21L.B.21. |
21L.B.63 Registration of a declaration of design compliance
The Agency shall register a declaration of design compliance for an aircraft provided that:
(a) |
the declarant has declared compliance in accordance with point (a) of point 21L.A.43; |
(b) |
the declarant has provided to the Agency the documents required in accordance with point (c) of point 21L.A.43; |
(c) |
the declarant has made a commitment that the obligations in accordance with point 21L.A.47 will be undertaken; |
(d) |
there are no unresolved findings from the physical inspection and assessment of the first article of the aircraft in the final configuration carried out in accordance with point (b) of point 21L.B.62. |
21L.B.64 Continuing airworthiness oversight of aircraft for which design compliance has been declared
If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means, detects a non-compliance with the applicable detailed technical specifications or the applicable environmental protection requirements, the Agency shall raise a finding in accordance with point 21L.B.21, or issue an airworthiness directive under the conditions of point 21L.B.23.
SUBPART D – CHANGES TO TYPE CERTIFICATES
21L.B.81 Type-certification basis and applicable environmental protection requirements for a major change to a type certificate
(a) |
The Agency shall establish the type-certification basis for a major change to a type certificate and notify it to the applicant. |
(b) |
For a major change to a type certificate and the areas affected by the change, the type-certification basis shall consist of the certification specifications incorporated by reference in the type certificate, unless:
|
(c) |
The Agency shall designate the applicable environmental protection requirements for the major change to a type certificate in accordance with point 21.B.85 of Annex I (Part 21) and notify them to the applicant. |
21L.B.82 Investigation and issuance of an approval of a minor change to a type certificate
(a) |
Upon receiving an application for the approval of a minor change to a type certificate under this Annex, the Agency shall approve the minor change when:
|
(b) |
An approval of a minor change to a type certificate shall be limited to the specific configuration(s) in the type certificate to which the change relates. |
21L.B.83 Investigation of a major change to a type certificate
Upon receiving an application for a major change to a type certificate under this Annex, the Agency shall:
(a) |
conduct a review of the initial compliance demonstration plan and any subsequent update provided by the applicant in order to establish the completeness of the plan and the appropriateness of the proposed means and methods of demonstrating compliance with the type-certification basis and the applicable environmental protection requirements established and designated in accordance with point 21L.B.81; if the compliance demonstration plan is incomplete or the means and methods are not appropriate to achieve compliance demonstration, the Agency shall inform the applicant and request an amendment of it; |
(b) |
when satisfied that the compliance demonstration plan provided is appropriate so that the applicant can demonstrate compliance, approve the compliance demonstration plan and also approve any subsequent updates of the compliance demonstration plan; |
(c) |
determine the likelihood of an unidentified non-compliance of the major change with the type-certification basis or with the applicable environmental protection requirements, and the potential impact of that non-compliance on the safety or environmental compatibility of the product, and determine on that basis whether a physical inspection and assessment of the first article of that product in the final changed configuration is necessary in order to verify the compliance of the product with the applicable type-certification basis and the applicable environmental protection requirements, taking into consideration the critical design review if carried out in accordance with point (a)(3) of point 21L.B.242; the Agency shall notify the applicant before conducting this inspection and assessment; |
(d) |
if during the establishment of the type-certification basis, the designation of the applicable environmental protection requirements or during the review of the compliance demonstration plan, the Agency determines that the design of the major change contains any element for which an unidentified non-compliance with the type-certification basis or the applicable environmental protection requirements may have an adverse impact on the safety or environmental compatibility of the changed product, the Agency shall determine which investigations are necessary in addition to those of point (c) in order to verify the compliance demonstration; the Agency shall notify the applicant of those additional investigations and which elements of the design would be subject to investigation. |
21L.B.84 Issuance of an approval of a major change to a type certificate
(a) |
The Agency shall approve the major change when:
|
(b) |
An approval of a major change to a type certificate shall be limited to the specific configuration(s) in the type certificate to which the change relates. |
21L.B.85 Continuing airworthiness oversight of changed products for which a type certificate has been issued
If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means, detects a non-compliance with the type-certification basis or the applicable environmental protection requirements of a product for which a change to a type certificate has been approved, the Agency shall raise a finding in accordance with point 21L.B.21, or issue an airworthiness directive under the conditions of point 21L.B.23.
SUBPART E – SUPPLEMENTAL TYPE CERTIFICATES
21L.B.101 Type-certification basis and applicable environmental protection requirements for a supplemental type certificate
(a) |
The Agency shall establish the type-certification basis for a supplemental type certificate and notify it to the applicant. |
(b) |
For major changes to a type certificate in the form of a supplemental type certificate, the type-certification basis for the areas affected by the change shall be that which is incorporated by reference in the type certificate, unless:
|
(c) |
The Agency shall designate the applicable environmental protection requirements for a major change to a type certificate in accordance with point 21.A.85 of Annex I (Part 21) and notify them to the applicant. |
21L.B.102 Investigation
Upon receiving an application for a supplemental type certificate under this Annex, the Agency shall:
(a) |
conduct a review of the initial compliance demonstration plan and any subsequent update provided by the applicant in order to establish the completeness of the plan and the appropriateness of the proposed means and methods of demonstrating compliance with the type-certification basis and the applicable environmental protection requirements established and designated in accordance with point 21L.B.101; if the compliance demonstration plan is incomplete or the means and methods are not appropriate to achieve compliance demonstration, the Agency shall inform the applicant and request an amendment of it; |
(b) |
when satisfied that the compliance demonstration plan provided is appropriate so that the applicant can demonstrate compliance, approve the compliance demonstration plan and any subsequent updates of the compliance demonstration plan; |
(c) |
determine the likelihood of an unidentified non-compliance of the major change with the type-certification basis or the applicable environmental protection requirements, and the potential impact of that non-compliance on the safety or environmental compatibility of the product, and determine on that basis whether a physical inspection and assessment of the first article of that product in the final changed configuration is necessary in order to verify the compliance of the product with the applicable type-certification basis and the applicable environmental protection requirements, taking into consideration the critical design review if carried out in accordance with point (a) of point 21L.B.242; the Agency shall notify the applicant before conducting this inspection and assessment; |
(d) |
if during the establishment of the type-certification basis, the designation of the applicable environmental protection requirements or during the review of the compliance demonstration plan, the Agency determines that the major change to the design contains any element for which an unidentified non-compliance with the type-certification basis or the applicable environmental protection requirements may have an adverse impact on the safety or environmental compatibility of the changed product, the Agency shall determine which investigations are necessary in addition to those of point (c) in order to verify the compliance demonstration; the Agency shall notify the applicant of those additional investigations and which elements of the design would be subject to this investigation. |
21L.B.103 Issuance of a supplemental type certificate
(a) |
Upon receiving an application for a supplemental type certificate under this Annex, the Agency shall issue a supplemental type certificate when:
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(b) |
A supplemental type certificate shall be limited to the specific configuration(s) in the type certificate to which the related major change relates. |
21L.B.104 Continuing airworthiness oversight of products for which a supplemental type certificate has been issued
If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means, detects a non-compliance with the type-certification basis or the applicable environmental protection requirements of a product for which a supplemental type certificate has been issued, the Agency shall raise a finding in accordance with point 21L.B.21, or issue an airworthiness directive under the conditions of point 21L.B.23.
SUBPART F – CHANGES TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED
21L.B.121 Initial oversight investigation of a declaration of design compliance of a major change to the design of an aircraft for which design compliance has been declared
(a) |
Upon receiving a declaration of design compliance for a major change to the design of an aircraft for which design compliance has been declared, the Agency shall verify that the change is within the scope of point 21L.A.101 and that the declaration contains all the information specified in point 21L.A.107. The Agency shall acknowledge the receipt of the declaration, including the assignment of an individual declaration of design compliance reference number to the declarant. |
(b) |
The Agency shall assess, based upon the risk of a non-compliance leading to a design that is not capable of safe flight or being environmentally incompatible, whether a physical inspection and assessment of the changed product is needed, and subsequently inform the declarant if that is the case. This assessment of the risk shall take into consideration:
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(c) |
If the Agency finds evidence in the declaration, or through the physical inspection and assessment if carried out in accordance with point (b) of point 21L.B.121, indicating that the changed aircraft could be incapable of conducting a safe flight or could be environmentally incompatible during in-service operations, the Agency shall raise a finding in accordance with point 21L.B.21. |
21L.B.122 Registration of a declaration of design compliance for a major change to an aircraft design
(a) |
The Agency shall register a declaration of design compliance for a major change to the design of an aircraft for which design compliance has been declared, provided that:
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(b) |
The Agency shall only register a declaration of a major change to the design of an aircraft for which design compliance has been declared if it is limited to the specific configuration(s) in the registered declaration of design compliance to which the change relates. |
21L.B.123 Continuing airworthiness oversight of a changed aircraft for which design compliance has been declared
If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means, detects a non-compliance with the applicable detailed technical specifications or the applicable environmental protection requirements of a change for which design compliance has been declared, the Agency shall act in accordance with point 21L.B.64.
SUBPART G – DECLARED PRODCUTION ORGANISATIONS
(reserved)
SUBPART H – CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS
(reserved)
SUBPART I – NOISE CERTIFICATES
(reserved)
SUBPART J – DECLARED DESIGN ORGANISATIONS
21L.B.181 Initial oversight investigation
(a) |
Upon receiving a declaration from an organisation declaring their design capability, the Agency shall verify that:
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(b) |
The Agency shall acknowledge the receipt of the declaration, including the assignment of an individual declared design organisation reference number to the declarant. |
21L.B.182 Registration of a declaration of design capability
The Agency shall register the declaration of design capability on a suitable database, including the declared scope of work, provided that:
(a) |
the declarant has declared their capability in accordance with point 21L.A.173; |
(b) |
the declarant has made a commitment that the obligations in accordance with point 21L.A.177 will be undertaken; |
(c) |
there are no unresolved issues in accordance with point 21L.B.181. |
21L.B.183 Oversight
(a) |
The Agency shall oversee the declared design organisation in order to verify the continuous compliance of the organisation with the applicable requirements of Section A. |
(b) |
The oversight shall include a product critical design review or physical inspection, and a first article inspection of every new design of the declared design organisation. |
21L.B.184 Oversight programme
(a) |
The Agency shall establish and maintain an oversight programme in order to ensure compliance with point 21L.B.183. The oversight programme shall take into account the specific nature of the organisation, the complexity of its activities and the results of past certification and/or oversight activities, and it shall be based on the assessment of the associated risks. It shall include, within each oversight planning cycle:
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(b) |
The oversight programme shall include records of the dates when assessments, audits, inspections and meetings are due, and when assessments, audits, inspections and meetings have been effectively carried out. |
(c) |
An oversight planning cycle that does not exceed 24 months shall be applied. |
(d) |
Notwithstanding point (c), the oversight planning cycle may be extended to 36 months if the Agency has established that during the previous 24 months:
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(e) |
Notwithstanding point (c), the oversight planning cycle may be further extended to a maximum of 48 months if, in addition to the conditions provided in point (d), the organisation has established, and the Agency has approved, an effective continuous system for reporting to the Agency on the safety performance and regulatory compliance of the organisation itself. |
(f) |
The oversight planning cycle may be reduced if there is evidence that the safety performance of the organisation has decreased. |
(g) |
At the completion of each oversight planning cycle, the Agency shall issue a recommendation report on the continuation of the activities conducted by the declared design organisation based on its declaration of design capability, reflecting the results of the oversight. |
21L.B.185 Oversight activities
(a) |
When the Agency verifies the compliance of the declared design organisation in accordance with point 21L.B.183 and the oversight programme established in accordance with point 21L.B.184, it shall:
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(b) |
The Agency shall collect and process any information deemed necessary for conducting oversight activities. |
(c) |
If the Agency detects a non-compliance of the declared design organisation with the applicable requirements of Section A, with a procedure or manual required by Section A, or with the declaration submitted, the Agency shall act in accordance with points 21L.B.21 and 21L.B.22. |
21L.B.186 Changes to declarations
(a) |
Upon receiving a notification of changes in accordance with point 21L.A.178, the Agency shall verify the completeness of the notification in accordance with point 21L.B.181. |
(b) |
The Agency shall update its oversight programme established according to point 21L.B.184 and investigate whether it is necessary to establish any conditions under which the organisation may operate during the change. |
(c) |
When the change affects any aspect of the declaration that is registered in accordance with point 21L.B.182, the Agency shall update the register. |
(d) |
Upon completion of the activities required by points (a) to (c), the Agency shall acknowledge the receipt of the notification to the declared design organisation. |
SUBPART K – PARTS
(Reserved)
SUBPART M – DESIGN OF REPAIRS TO TYPE-CERTIFIED PRODUCTS
21L.B.201 Type-certification basis and applicable environmental protection requirements for a repair design approval
The Agency shall designate any amendments to the type-certification basis and the applicable environmental requirements incorporated by reference in, as applicable, either the type certificate or the supplemental type certificate, which the Agency considers necessary for maintaining a level of safety and environmental compatibility equal to that previously established and notify them to the applicant for the approval of a repair design.
21L.B.202 Investigation and issuance of an approval for a minor repair design
(a) |
Upon receiving an application for the approval of a minor repair design to a type-certified product under this Annex, the Agency shall approve the minor repair design when:
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(b) |
An approval of a minor repair design shall be limited to the specific configuration(s) in the type certificate to which the repair design relates. |
21L.B.203 Investigation of an application for the approval of a major repair design
Upon receiving an application for the approval of a major repair design under this Annex, the Agency shall:
(a) |
conduct a review of the initial compliance demonstration plan and any subsequent update provided by the applicant in order to establish the completeness of the plan and the appropriateness of the proposed means and methods of demonstrating compliance with the type-certification basis and the applicable environmental protection requirements established and designated in accordance with point 21L.B.201; if the compliance demonstration plan is incomplete or the means and methods are not appropriate to achieve compliance demonstration, the Agency shall inform the applicant and request an amendment of it; |
(b) |
when satisfied that the compliance demonstration plan provided is appropriate so that the applicant can demonstrate compliance, approve the compliance demonstration plan and any subsequent updates of the compliance demonstration plan; |
(c) |
determine the likelihood of an unidentified non-compliance of the major repair design with the type-certification basis or with the applicable environmental protection requirements, and the potential impact of that non-compliance on the safety or environmental compatibility of the product, and determine on that basis whether a physical inspection and assessment of the first article of that product in the final configuration with the repair design is necessary in order to verify the compliance of the product with the applicable type-certification basis; the Agency shall notify the applicant before conducting this inspection and assessment; |
(d) |
if, during the review of the compliance demonstration plan, the Agency determines that the major repair design contains any element for which an unidentified non-compliance with the type-certification basis or with the applicable environmental protection requirements may have an adverse impact on the safety or environmental compatibility of the changed product, the Agency shall determine which investigations are necessary in addition to those of point (c) in order to verify the compliance demonstration; the Agency shall notify the applicant of those additional investigations and which elements of the design would be subject to investigation. |
21L.B.204 Issuance of an approval of a major repair design
(a) |
Upon receiving an application for the approval of a major repair design to a type-certified product under this Annex, the Agency shall approve the major repair design when:
|
(b) |
An approval of a major repair design shall be limited to the specific configuration(s) in the type certificate to which the repair design relates. |
21L.B.205 Continuing airworthiness oversight of products for which a repair design has been approved
If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means detects a non-compliance of a product, for which a repair design has been approved, with the type-certification basis or with the applicable environmental protection requirements, the Agency shall raise a finding in accordance with point 21L.B.21, or issue an airworthiness directive under the conditions of point 21L.B.23.
21L.B.206 Unrepaired damage
An evaluation of the airworthiness consequences shall be conducted by the Agency, when requested to do under point 21L.A.211, in the event that a damaged product is left unrepaired and is not covered by previously approved data. The Agency shall establish any limitations necessary to ensure a safe flight with the damaged product.
SUBPART N – DESIGN OF REPAIRS TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED
21L.B.221 Initial oversight investigation of a declaration of design compliance of a major repair design to an aircraft for which design compliance has been declared
(a) |
Upon receiving a declaration of design compliance of a major repair design to an aircraft for which design compliance has been declared, the Agency shall verify that that the repair design is within the scope of point 21L.A.221 and that the declaration contains all the information specified in point 21L.A.226. The Agency shall acknowledge the receipt of the declaration, including the assignment of an individual declaration of design compliance reference number to the declarant. |
(b) |
The Agency shall assess, based upon the risk of a non-compliance leading to a design that is not capable of safe flight or being environmentally incompatible, whether a physical inspection and assessment of the aircraft with the major repair design is needed, and subsequently inform the declarant if that is the case. This assessment of the risk shall take into consideration:
|
(c) |
If the Agency finds evidence in the declaration, or through the physical inspection and assessment if carried out in accordance with point (b) of point 21L.B.221, indicating that the aircraft with the major repair design could be incapable of conducting a safe flight or could be environmentally incompatible during in-service operations, the Agency shall raise a finding in accordance with point 21L.B.21. |
21L.B.222 Registration of a declaration of a major repair design to an aircraft for which design compliance has been declared
(a) |
The Agency shall register a declaration of a major repair design to an aircraft for which design compliance has been declared provided that:
|
(b) |
The Agency shall only register a declaration of a major repair design to an aircraft for which design compliance has been declared if it is limited to the specific configuration(s) in the registered declaration of design compliance to which the major repair design relates. |
21L.B.223 Continuing airworthiness oversight of a repair design for which design compliance has been declared
If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means, detects a non-compliance of a repair design, for which design compliance has been declared, with the applicable detailed technical specifications or with the applicable environmental protection requirements, the Agency shall raise a finding in accordance with point 21L.B.21, or issue an airworthiness directive under the conditions of point 21L.B.23.
SUBPART O – EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS
(Reserved)
SUBPART P – PERMIT TO FLY
(reserved)
SUBPART Q – IDENTIFICATION OF PRODUCTS AND PARTS
SUBPART R – STATEMENT OF CONFORMITY FOR AIRCRAFT AND AUTHORISED RELEASE CERTIFICATES (EASA FORM 1) FOR ENGINES AND PROPELLERS, AND PARTS THEREOF, THAT CONFORM TO A DECLARATION OF DESIGN COMPLIANCE
Appendices to ANNEX Ib (Part 21 Light)
EASA FORMS
When the Forms of this Annex are issued in a language other than English, they shall include an English translation. |
The EASA (‘European Union Aviation Safety Agency’) Forms referred to in the appendices to this Part shall have the following obligatory features. Member States shall ensure that the EASA Forms they issue are recognisable and shall be responsible for having those Forms printed.
Appendix I |
EASA Form 24B Restricted certificate of airworthiness |
Appendix II |
EASA Form 45B Restricted noise certificate |
Appendix III |
EASA Form 52B Aircraft statement of conformity |
Appendix IV |
EASA Form 53B Certificate of release to service |
Appendix I
Restricted certificate of airworthiness – EASA Form 24B
Competent authority logo
RESTRICTED CERTIFICATE OF AIRWORTHINESS (DECLARED)
[Member State of registry] [COMPETENT AUTHORITY OF THE MEMBER STATE] |
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EASA Form 24B – Issue 1
This certificate shall be carried on board during all flights.
Appendix II
Restricted noise certificate – EASA Form 45B
For use by the Member State of registry |
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EASA Form 45B – Issue 1
Appendix III
Aircraft statement of conformity – EASA Form 52B
AIRCRAFT STATEMENT OF CONFORMITY |
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EASA Form 52B – Issue 1
Instructions for the use of the ‘Aircraft statement of conformity – EASA Form 52B’
1. PURPOSE AND SCOPE
1.1. |
The purpose of the aircraft statement of conformity (EASA Form 52B) issued under Subpart G or Subpart R of Section A of Annex Ib (Part 21 Light) or under Subpart G of Section A of Annex I (Part 21) is to enable the production organisation to apply for an individual aircraft certificate of airworthiness or restricted certificate of airworthiness from the competent authority of the Member State of registry. |
2. GENERAL
2.1. |
The statement of conformity must comply with the model format, including the block numbers and the location of each block. The size of each block may, however, be varied to suit the individual application, but not to the extent that would render the statement of conformity unrecognisable. If in doubt, consult the competent authority. |
2.2. |
The statement of conformity must be either pre-printed or computer generated, but in either case, the printing of lines and characters must be clear and legible. Pre-printed wording is permitted in accordance with the attached model, but no other certification statements are permitted. |
2.3. |
The completion of the statement may be either machine/computer-printed or handwritten, using block letters to allow for easy reading. English, and where relevant, one or more of the official language(s) of the issuing Member State, are acceptable. |
2.4. |
A copy of the statement and all the referenced attachments are to be retained by the approved production organisation. |
3. COMPLETION OF THE STATEMENT OF CONFORMITY BY THE ORIGINATOR
3.1. |
There should be an entry in all blocks to render the document a valid statement. |
3.2. |
A statement of conformity may not be issued to the competent authority of the Member State of registry unless the design of the aircraft and its installed products are approved or the declaration of design compliance is registered with the Agency. |
3.3. |
The information required in blocks 9, 10, 11, 12, 13 and 14 may be by reference to separate identified documents held on file by the production organisation, unless the competent authority agrees otherwise. |
3.4. |
This statement of conformity is not intended to include those items of equipment that may be required to be fitted in order to satisfy the applicable operational rules. However, some of these individual items may be included in block 10 or in the approved type design or the declared aircraft design. Operators are therefore reminded of their responsibility to ensure compliance with the applicable operational rules for their own particular operations.
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Appendix IV
Certificate of release to service – EASA Form 53B
CERTIFICATE OF RELEASE TO SERVICE [PRODUCTION ORGANISATION NAME] Production organisation reference: Certificate of release to service in accordance with 21L.A.126(e) or 21L.A.273(8) of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012 (delete as appropriate). Aircraft: …Type: …Constructor No/Registration: … has been maintained as specified in work order: … Brief description of work performed: Certifies that the work specified was carried out in accordance with 21L.A.126(e) or 21L.A.273(8) of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012 (delete as appropriate) and in respect to that work the aircraft is considered ready for release to service and therefore is in a condition for safe operation. Certifying staff (name): (signature): Location: Date:. . -. . -. .. . (day, month, year) |
EASA Form 53B – Issue 1
COMPLETION INSTRUCTIONS
The Block BRIEF DESCRIPTION OF WORK PERFORMED appearing in EASA FORM 53B should include a reference to the approved data used to perform the work.
The Block LOCATION appearing in EASA FORM 53B refers to the location where the maintenance has been performed, not to the location of the facilities of the organisation (if different).
(1) Regulation (EU) No 376/2014 of the European Parliament and of the Council of 3 April 2014 on the reporting, analysis and follow-up of occurrences in civil aviation, amending Regulation (EU) No 996/2010 of the European Parliament and of the Council and repealing Directive 2003/42/EC of the European Parliament and of the Council and Commission Regulations (EC) No 1321/2007 and (EC) No 1330/2007 (OJ L 122, 24.4.2014, p. 18).
(2) Commission Regulation (EU) No 965/2012 of 5 October 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 296, 25.10.2012, p. 1).
(4) 2 For use by the Member State of registry.
(5) Delete as applicable.