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21.B.326 Certificate of airworthiness

Annex I · Regulation (EU) No 748/2012 · EAR revision 27 Nov 2025

IRImplementing rule

21.B.326Certificate of airworthiness

(a)The competent authority of the Member State of registry shall issue a certificate of airworthiness for: (1) new aircraft: (i) upon presentation of the documentation required by point 21.A.174(b)(2); (ii) where the competent authority of the Member State of registry is satisfied that the aircraft is in compliance with the applicable CO 2 emissions requirements on the date on which the certificate of airworthiness is first issued; (2) used aircraft transferred from another Member State having a certificate of airworthiness issued in accordance with this Annex, upon presentation of a copy of the current certificate of airworthiness and one of the following: (i) the documentation required by point 21.A.174(b)(3)(i)(A); (ii) the documentation required by point 21.A.174(b)(3)(i)(B); (3) used aircraft not having a certificate of airworthiness issued in accordance with this Annex, upon presentation of the documentation required by point 21.A.174(b)(3)(ii) demonstrating that the following conditions are met: (i) the aircraft or the UAS, as applicable, conforms to a design approved under a type certificate, and any supplemental type certificate, change or repair approved in accordance with this Annex; (ii) the applicable airworthiness directives have been complied with; (iii) an airworthiness review has been carried out in accordance with the applicable requirement of Annex I (Part-M) or Annex Vb (Part-ML) to Regulation (EU) No 1321/2014, or Annex I (Part-ML.UAS) to Delegated Regulation (EU) 2024/1107, as applicable; (iv) the aircraft was in compliance with the applicable CO 2 emissions requirements on the date on which the certificate of airworthiness was first issued.

(b)For the cases referred to in points (a)(1), (a)(2)(ii) and (a)(3), the Member State of registry shall issue a certificate of airworthiness where it is satisfied that the aircraft or the UAS, as applicable, conforms to an approved design and is in a condition for safe operation. This may include inspections by the competent authority of the Member State of registry.

IR · 21.B.326 — Regulation (EU) No 748/2012 · Initial Airworthiness Easy Access Rules · EAR revision 27 Nov 2025

AMCAcceptable means of compliance

AMC1 21.B.326(a)(3)and 21.B.327(a)(3) (Restricted) Certificate of airworthiness

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ACCEPTANCE OF THE EVALUATION PROGRAMME BY THE COMPETENT AUTHORITY When an application for an airworthiness certificate is submitted without a statement reflecting the aircraft’s airworthiness status, as specified in point 21.A.174(d), an evaluation programme should be submitted to the competent authority for acceptance. If the competent authority finds that the proposed evaluation programme is suitable to properly evaluate the status of the aircraft with regard to its configuration and maintenance, including conformity to the approved type design, existing modifications and repairs and maintenance, and continuing airworthiness status, it should accept it and notify the applicant about the acceptance and, if applicable, about the involvement of the authority in the proposed investigation activities. In making this determination, the competent authority should, if relevant, take into account its own experience with imports of aircraft originating from the same third-country regulatory framework or with known shortcomings typically observed in the same aircraft models that may require particular attention. If the competent authority finds that the proposed evaluation programme is insufficient to properly evaluate the status of the aircraft, it should reject the evaluation programme and provide a justification for its decision to do so.

AMC · AMC1 21.B.326(a)(3) — Regulation (EU) No 748/2012 · ED Decision 2026/005/R · Initial Airworthiness Easy Access Rules · EAR revision 27 Nov 2025

GMGuidance material

GM1 21.B.326(a)(1)(ii)and (a)(3)(iv) Certificate of airworthiness

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CO2 EMISSIONS PRODUCTION CUT-OFF REQUIREMENTS Volume III of Annex 16 to the Chicago Convention (‘ICAO Annex 16') includes CO2 emissions production cut-off standards that apply to subsonic jet aeroplanes with a Maximum Take-Off Mass (MTOM) greater than 5 700 kg and propeller-driven aeroplanes with a MTOM greater than 8 618 kg, for which a type certificate was issued but that were not certified for CO2 emissions in accordance with Volume III of ICAO Annex 16, and for which the individual certificate of airworthiness (CofA) was first issued on or after 1 January 2028 (Sections 2.1.1.(f) and (g) of Chapter 2 of Part II of Volume III of ICAO Annex 16). These production cut-off standards were introduced with the first edition of Volume III of ICAO Annex 16. — For a new aeroplane (21.B.326(a)(1)(ii)): The competent authority assesses whether an aeroplane CO2 emissions production cut-off requirement applies to the aeroplane, and, if such a requirement applies, that the aeroplane conforms to this requirement before issuing the first CofA. — For a used aeroplane that does not have an airworthiness certificate issued in accordance with Part 21 (for example, an aeroplane imported from a third country) (21.B.326(a)(3)(iv)): The competent authority assesses whether an aeroplane CO2 emissions production cut-off requirement applied to the aeroplane when its first CofA was issued, and, if such a requirement applied, that the aeroplane conformed to that requirement on the date on which the CofA was first issued. The competent authority may check that the CO2 metric value provided by the applicant for a CofA corresponds to the CO2 metric value approved by the Agency for the aeroplane type. Note: For a used aeroplane that has an airworthiness certificate issued in accordance with Part 21 (for example, an aeroplane transferred from a Member State), the compliance with the applicable environmental protection requirements was already assessed for the issuance of the previous CofA. The competent authority may refer to the corresponding certified CO2 emissions evaluation metric values that are published by the Agency in the EASA Aeroplane CO2 Emissions Database2. These specific requirements ensure that the CO2 emissions production cut-off requirement that may apply to the aeroplane is not overlooked. Further guidance material on the applicability of the aeroplane CO2 emissions requirements is provided in ICAO Doc 9501 ‘Environmental Technical Manual’, Volume III ‘Procedures for the CO2 Emissions Certification of Aeroplanes’.

2 https://www.easa.europa.eu/en/domains/environment/easa-aeroplane-co2-emissions-database-0

GM · GM1 21.B.326(a)(1)(ii) — Regulation (EU) No 748/2012 · ED Decision 2026/005/R · Initial Airworthiness Easy Access Rules · EAR revision 27 Nov 2025

All rules in SECTION B — PROCEDURES FOR COMPETENT AUTHORITIES

Consolidated from the EASA Easy Access Rules (revision 27 Nov 2025, extracted 17 Aug 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.

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