OpenLegislation

Division 21.B.453 Issuance of a repair design approvalF1

United Kingdom

Original text. Later amendments are not shown.

  1. (a)

    The F2CAA shall issue an approval of a major repair design, provided that:

    1. 1..

      the applicant has demonstrated its capability in accordance with point 21.A.432B;

    2. 2..

      the applicant has complied with point 21.A.433;

    3. 3..

      the CAA, through its verification of the demonstration of compliance in accordance with the level of involvement established pursuant to point 21.B.100(a), has not found any non-compliance with the type-certification basis and environmental protection requirements; and

    4. 4..

      no feature or characteristic has been identified that may make the product unsafe for the uses for which certification is requested.

  2. (b)

    The CAA shall issue an approval of a minor repair design, provided that the applicant has complied with points (2) and (4) of point (a) and provided that the CAA, through its verifications of the demonstration of compliance in accordance with the level of involvement pursuant to point 21.B.100(b), has not found any non-compliance with the type-certification basis and environmental protection requirements.

Annotations

Textual amendments

F1

Substituted by Commission Delegated Regulation (EU) 2019/897 of 12 March 2019 amending Regulation (EU) No 748/2012 as regards the inclusion of risk-based compliance verification in Annex I and the implementation of requirements for environmental protection (Text with EEA relevance).

F2

Word in Annex 1 point 21.B.453 substituted (31.12.2020) by The Aviation Safety (Amendment) (EU Exit) Regulations 2020 (S.I. 2020/1116), regs. 1(2), 61(8)(b)

Notes on Section B

Textual amendments

F1

Words in Annex 1 Pt. 21 s. B heading substituted (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 209 (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)