What documents and information must be provided to EASA under point 21L.A.226(c) for a major repair design?

The documents and information required by point 21L.A.226(c) must be provided to EASA by the declarant. The section does not list the specific documents, but states they are those required by that point.

Can the declarant submit the required information to EASA before filing the declaration of design compliance for a major repair?

Yes, the declarant may provide the documents and information required by point 21L.A.226(c) to EASA in advance of the submission of the declaration of design compliance for the 'major' change.

Which EASA point governs the first-article inspection that may be needed after reviewing the pre-submitted information for a major repair?

The first-article inspection is governed by point 21L.B.221(b).

Under which EASA decision and point is the guidance on the declaration of design compliance for major repair designs issued?

The guidance is issued under ED Decision 2023/013/R and relates to point 21L.A.226(c).

GM1 21L.A.226(c) Declaration of design compliance of major repair designs

Q: What is the advantage to the declarant of providing the required information to EASA early for a major repair design?

Providing the information in advance is advantageous for the declarant to facilitate EASA's investigations and to determine the need for the first-article inspection under point 21L.B.221(b).

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GM1 21L.A.226(c) Declaration of design compliance of major repair designs

ED Decision 2023/013/R

INFORMATION TO BE PROVIDED TO EASA

The documents and information that are required to be provided to EASA in point 21L.A.226(c) may be provided to EASA by the declarant in advance of the submission of the declaration of design compliance for the ‘major’ change. This would be advantageous for the declarant to facilitate EASA’s investigations and to determine the need for the first-article inspection under point 21L.B.221(b).

Details

Source-Title: GM1 21L.A.226(c) Declaration of design compliance of major repair designs View latest amendments

Erulesid: ERULES-1963177438-22076 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: GM to IR (Guidance material to implementing rule)

Parentir: 21L.A.226 Declaration of design compliance of major repair designs

Origin: EASA

Category: EAR