| Number |
2025-0283 |
| Issued by |
 Europe |
| Issue date |
2025-12-17 |
| Effective date |
2025-12-29 |
| EASA approval number |
|
| ATA Chapter |
54 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
This AD is republished to correct a typographical error in Note 1 of this AD (reference to an incorrect
paragraph number).
|
| Supersedure |
This AD supersedes EASA AD 2024-0060R1 dated 16 April 2024.
|
| Publication(s) and related information |
Airbus SB A350-54-P009 original issue dated 22 December 2023, or Revision 01 dated 17 October 2025.
Collins Aerospace SB RA35071-029 original issue dated 16 November 2023, or Revision 01 dated 30 September 2025.
Airbus RDAF 81078446/002/2022 issue A dated 05 July 2022.
Airbus RDAF 81081734/002/2022 issue A dated 09 September 2022.
Airbus RDAF 81139320/003/2022 issue A dated 10 November 2022.
Airbus RDAF 81147946/013/2022 issue A dated 15 December 2022.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
25-172 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 10 November 2025 as PAD 25-172 for consultation until 08 December 2025. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file, attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.
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