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21.A.263 Privileges
Available versions for ERULES-1963177438-3902
Regulation (EU) 2022/1358
found in: Initial Airworthiness and Environmental Protection (No 748/2012) Part-21 Part-21L (Jul 2024)
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21.A.263 Privileges Regulation (EU) 2022/1358 (a) (Reserved) (b) (Reserved) (c) The holder of a design organisation approval shall be entitled, within the scope of its terms of approval issued under point [21.A.251](#_DxCrossRefBm1649097315) and under the relevant procedures of the design management system: 1. to classify changes to a type certificate or to a supplemental type certificate and repair designs as ‘major’ or ‘minor’; 2. to approve minor changes to a type certificate or to a supplemental type certificate and minor repair designs under this [Annex](#_DxCrossRefBm1649096844) (Part 21) or under [Annex Ib](#_DxCrossRefBm1649096843) (Part 21 Light); 3. to declare the compliance of a minor change or minor repair to the design of an aircraft for which design compliance has been declared by the declarant under point [21L.A.43](#_DxCrossRefBm1649097270) of Subpart C of Section A of Annex Ib (Part 21 Light;) 4. to declare compliance of a changed aircraft design, in accordance with point [21L.A.43](#_DxCrossRefBm1649097270) of Annex Ib (Part 21 Light), in the event that the natural or legal person who originally made a declaration of design compliance with respect to that aircraft under point [21L.A.43](#_DxCrossRefBm1649097270) of Annex Ib (Part 21 Light) is no longer active or is unresponsive to requests for the declaration of compliance of design changes; 5. to approve certain major repair designs under Subpart M of this [Annex](#_DxCrossRefBm1649096844) to products or auxiliary power units (APUs); 6. to approve for certain aircraft the flight conditions under which a permit to fly can be issued in accordance with point [21.A.710](#_DxCrossRefBm1649097267)(a)(2), except for permits to fly to be issued for the purpose of point [21.A.701](#_DxCrossRefBm1649097379)(a)(15); 7. to issue a permit to fly in accordance with point [21.A.711](#_DxCrossRefBm1649097268)(b) for an aircraft it has designed or modified, or for which it has approved, in accordance with point [21.A.263](#_DxCrossRefBm1649096918)(c)(6), the flight conditions under which the permit to fly can be issued, and where the holder of a design organisation approval itself: (i) controls the configuration of the aircraft, and (ii) attests conformity with the design conditions approved for the flight; 8. to approve certain major changes to a type certificate under Subpart D of this Annex or under Subpart D of Section A of [Annex Ib](#_DxCrossRefBm1649096843) (Part 21 Light); and 9. to issue certain supplemental type certificates under Subpart E of this [Annex](#_DxCrossRefBm1649096844) or under Subpart E of Section A of [Annex Ib](#_DxCrossRefBm1649096843) (Part 21 Light) and approve certain major changes to those certificates.