How are repair designs to an aircraft with a declared design compliance classified under 21L.A.223?

They are classified as either major or minor using the criteria in points (b) and (c) of 21L.A.203.

For a major repair design, where must the design compliance be declared?

In accordance with point 21L.A.226.

21L.A.223 Classification of repair designs to an aircraft for which design compliance has been declared

Q: What is the classification basis for repair designs under 21L.A.223(a)?

The criteria laid down in points (b) and (c) of 21L.A.203.

Q: For a minor repair design, where must the design compliance be declared?

In accordance with point 21L.A.225.

Q: Does 21L.A.223 apply to repair designs for aircraft that have not undergone a declaration under Subpart C?

No, it applies only to repair designs to an aircraft which was subject to a declaration made in accordance with Subpart C of this Annex.

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21L.A.223 Classification of repair designs to an aircraft for which design compliance has been declared

Regulation (EU) 2022/1358

(a) Repair designs to an aircraft which was subject to a declaration made in accordance with Subpart C of this Annex shall be classified as either a major or minor, using the criteria laid down in points (b) and (c) of 21L.A.203.

(b) The design compliance of a minor repair design shall be declared in accordance with point 21L.A.225.

Details

Source-Title: 21L.A.223 Classification of repair designs to an aircraft for which design compliance has been declared View latest amendments

Erulesid: ERULES-1963177438-21212 Compare versions

Domain: Initial airworthiness

Applicabilitydate: 25 August, 2023

Entryintoforcedate: 25 August, 2022

Regulatorysource: Regulation (EU) 2022/1358 Navigate

Regulatorysubject: Part 21 Light

Typeofcontent: IR (Implementing rule)

Origin: EASA

Category: EAR

21L.A.223 Classification of repair designs to an aircraft for which design compliance has been declared

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