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1. For the aircraft referred to in points (a) and (b) of Article 2(1), other than unmanned aircraft, and their engines, propellers, parts and non-installed equipment, the Commission is empowered to adopt delegated acts in accordance with Article 128, laying down detailed rules with regard to:

(a) detailed environmental protection requirements for products, parts and non-installed equipment, in situations referred to in the second subparagraph of Article 9(2);

(b) the conditions for establishing and notifying to an applicant by the Agency in accordance with Article 77:

(i) the type-certification basis applicable to a product for the purposes of the type-certification referred to in Article 11 and point (b) of Article 18(1);

(ii) the certification basis applicable to a product for the purposes of the approval of operational suitability data referred to in Article 11 including:

— the minimum syllabus of maintenance certifying staff type rating training;

— the minimum syllabus of pilot type rating and the reference data for the objective qualification of associated simulators;

— the master minimum equipment list, as appropriate;

— aircraft type data relevant to cabin crew;

— additional specifications to ensure compliance with Section III;

(iii) the certification basis applicable to a part or non-installed equipment, including safety-related equipment and instruments referred to in Article 30(7), for the purposes of the certification referred to in Articles 12 and 13;

(c) the specific conditions for compliance of aircraft referred to in point (b)(ii) of Article 2(1) with the essential requirements referred to in Article 9;

(d) the conditions for issuing, maintaining, amending, limiting, suspending or revoking the certificates referred to in Articles 11, 12, 13 and point (b) of Article 18(1), including:

(i) the conditions for situations in which, with a view to achieving the objectives set out in Article 1 and while taking account of the nature and risk of the particular activity concerned, such certificates are to be required or are not to be required, or declarations are to be permitted, as applicable;

(ii) the conditions concerning the duration of those certificates and concerning the renewal of those certificates where their duration is limited;

(e) the conditions for the issuing, amending, limiting, suspending or revoking of the certificates of airworthiness and noise certificates referred to in Article 14(1), as well as restricted certificates of airworthiness and restricted noise certificates referred to in point (a) of the first subparagraph of Article 18(2);

(f) the conditions for the issuing, maintaining, amending, limiting, suspending, revoking and use of the permits to fly referred to in point (b) of the first subparagraph of Article 18(2);

(g) the conditions for issuing, maintaining, amending, limiting, suspending or revoking the approvals referred to in Article 15(1), and for the situations in which, with a view to achieving the objectives set out in Article 1 and while taking account of the nature and risk of the particular activity concerned, such approvals are to be required or are not to be required or declarations are to be permitted, as applicable;

(h) the privileges and responsibilities of the holders of the certificates issued pursuant to Articles 11, 12, 13, Articles 14(1), 15(1), point (b) of Article 18(1) and Article 18(2) and of the organisations that made declarations in accordance with point (a) of Article 18(1) and point (g) of this paragraph;

(i) the conditions for establishing the detailed specifications applicable to the design of products, design of parts and design of non-installed equipment which are subject to a declaration in accordance with point (a) of Article 18(1);

(j) the conditions and procedures to assess, in accordance with point (a) of Article 18(1), the airworthiness and environmental compatibility of the design of products, the design of parts, and the design of non-installed equipment without the need to issue a certificate, including the conditions and limitations for operations;

(k) the conditions for organisations that have been issued with an approval in accordance with Article 15(1) to be granted the privilege to issue the certificates referred to in Articles 11, 12, 13 and point (b) of the first subparagraph of Article 18(2).

2. As regards the airworthiness and environmental compatibility of aircraft referred to in points (a) and (b) of Article 2(1), other than unmanned aircraft, and their engines, propellers, parts and non-installed equipment, the Commission is empowered to adopt delegated acts, in accordance with Article 128, to amend Annexes II and III, where necessary for reasons of technical, operational or scientific developments or evidence in the field of airworthiness or environmental compatibility, in order and to the extent required to achieve the objectives set out in Article 1.

3. As regards the environmental compatibility of aircraft referred to in points (a) and (b) of Article 2(1), other than unmanned aircraft, and their engines, propellers, parts and non-installed equipment, the Commission is empowered to adopt delegated acts in accordance with Article 128, to amend the references to the provisions of the Chicago Convention referred to in the first subparagraph of Article 9(2), in order to update them in light of subsequent amendments to those provisions which enter into force after 4 July 2018 and which become applicable in all Member States, in so far as such adaptations do not broaden the scope of this Regulation.