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Navigate / EASA / INITIAL AIRWORTHINESS AND ENVIRONMENTAL PROTECTION NOV 2025 / Annex Ib / SECTION A - TECHNICAL REQUIREMENTS / SUBPART N -- DESIGN OF REPAIRS TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED /

21L.A.222 Standard repairs

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21L.A.222 Standard repairs

Regulation (EU) 2022/1358

(a) Standard repairs are repair designs to an aircraft which was subject to a declaration made in accordance with Subpart C of this Annex and which:

1. follow the design data included in the certification specifications issued by the Agency, containing the acceptable methods, techniques and practices for carrying out and identifying standard repairs, including the associated instructions for continued airworthiness; and

2. are not in conflict with the design data covered by the declaration of aircraft design compliance made in accordance with Subpart C of this Annex.

(b) Points 21L.A.223 to 21L.A.229 are not applicable to standard repairs.

Frequently Asked Questions

Regulation (EU) 2022/1358.

* Aviation.Bot's Suggestion - Always consult the original regulation for confirmation

Standard repairs apply to an aircraft which was subject to a declaration made in accordance with Subpart C of this Annex.

* Aviation.Bot's Suggestion - Always consult the original regulation for confirmation

The repair design must (1) follow the design data included in the certification specifications issued by the Agency, containing the acceptable methods, techniques and practices for carrying out and identifying standard repairs, including the associated instructions for continued airworthiness; and (2) not be in conflict with the design data covered by the declaration of aircraft design compliance made in accordance with Subpart C of this Annex.

* Aviation.Bot's Suggestion - Always consult the original regulation for confirmation

Points 21L.A.223 to 21L.A.229 are not applicable to standard repairs.

* Aviation.Bot's Suggestion - Always consult the original regulation for confirmation

No, points 21L.A.223 to 21L.A.229 are not applicable to standard repairs, so no separate approval under those points is required.

* Aviation.Bot's Suggestion - Always consult the original regulation for confirmation

The certification specifications must contain the acceptable methods, techniques and practices for carrying out and identifying standard repairs, including the associated instructions for continued airworthiness.

* Aviation.Bot's Suggestion - Always consult the original regulation for confirmation

No, a standard repair must not be in conflict with the design data covered by the declaration of aircraft design compliance made in accordance with Subpart C of this Annex.

* Aviation.Bot's Suggestion - Always consult the original regulation for confirmation

An aircraft that was subject to a declaration made in accordance with Subpart C of this Annex.

* Aviation.Bot's Suggestion - Always consult the original regulation for confirmation

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