21L.A.224 Eligibility

• Regulation (EU) 2022/1358 found in: Initial Airworthiness and Environmental Protection (748/2012) Part-21 Part-21L (Jul 2024)

21L.A.224 Eligibility Regulation (EU) 2022/1358 (a)     A declarant who made a declaration of aircraft design compliance in accordance with [Subpart C](#_DxCrossRefBm1649097717) 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](#_DxCrossRefBm1649096918) of Annex I (Part 21). (b)     Only the declarant who made a declaration of aircraft design compliance in accordance with [Subpart C](#_DxCrossRefBm1649097717) 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](#_DxCrossRefBm1649097717) 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a declaration of aircraft design compliance in accordance with [Subpart C](#_DxCrossRefBm1649097717) of this Annex is no longer active or is unresponsive to requests for repair designs, the compliance of a changed aircraft design may also be declared in accordance with [Subpart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](#_DxCrossRefBm1649097717) of this Annex by a design organisation approved in accordance with point (c)(2) of point [21.A.263](#_DxCrossRefBm1649096918) 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](#_DxCrossRefBm1649097833) with respect to that changed aircraft. #### 21L.A.224 Eligibility *Regulation (EU) 2022/1358* (a) A declarant who made a declaration of aircraft design compliance in accordance with [Subpart C](#_DxCrossRefBm485231213) 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](#_DxCrossRefBm485230409) of Annex I (Part 21). (b) Only the declarant who made a declaration of aircraft design compliance in accordance with [Subpart C](#_DxCrossRefBm485231213) 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](#_DxCrossRefBm485231213) 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](#_DxCrossRefBm485231213) 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](#_DxCrossRefBm485231213) of this Annex by a design organisation approved in accordance with point (c)(2) of point [21.A.263](#_DxCrossRefBm485230409) 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](#_DxCrossRefBm485231329) with respect to that changed aircraft.