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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(c)(5) of Annex I (Part 21), the process described under AMC No 2 to 21.A.263(c)(5), (8) and (9) applies.
Details
Source-Title: AMC1 21L.A.208 Requirements for the approval of a major repair design View latest amendments
Erulesid: ERULES-1963177438-22028 Compare versions
Domain: Initial airworthiness
Amendedby: Issue 1
Applicabilitydate: 21 October, 2023
Entryintoforcedate: 21 October, 2023
Regulatorysource: ED Decision 2023/013/R Navigate
Regulatorysubject: Part 21 Light
Typeofcontent: AMC to IR (Acceptable means of compliance to implementing rule)
Parentir: 21L.A.208 Requirements for the approval of a major repair design
Origin: EASA
Category: EAR