AMC1 21L.A.208 Requirements for the approval of a major repair design

• ED Decision 2023/013/R found in: Initial Airworthiness and Environmental Protection (748/2012) Part-21 Part-21L (Jul 2024)

AMC1 21L.A.208 Requirements for the approval of a major repair design ED Decision 2023/013/R (a)     For major repairs approved by EASA, the applicant should use all the AMC and GM to point 21L.A.25. (b)     For major repairs approved by the design organisation approval (DOA) holder on the basis of its privilege as per point [21.A.263](#_DxCrossRefBm1649096918)(c)(5) of Annex I (Part 21), the process described under [AMC No 2 to 21.A.263(c)(5), (8) and (9)](#_DxCrossRefBm1649097059) applies. ##### AMC1 21L.A.208 Requirements for the approval of a major repair design *ED Decision 2023/013/R* (a) For major repairs approved by EASA, the applicant should use all the AMC and GM to point 21L.A.25. (b) For major repairs approved by the design organisation approval (DOA) holder on the basis of its privilege as per point [21.A.263](#_DxCrossRefBm485230409)(c)(5) of Annex I (Part 21), the process described under [AMC No 2 to 21.A.263(c)(5), (8) and (9)](#_DxCrossRefBm485230550) applies.