| Number |
2023-0176R1 |
| Issued by |
 Europe |
| Issue date |
2026-03-06 |
| Effective date |
2026-03-13 |
| EASA approval number |
|
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises EASA AD 2023-0176 dated 06 October 2023.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2023-0011R1 dated 23 February 2023.
|
| Publication(s) and related information |
Airbus AOT A53P016-22 original issue dated 09 January 2023, Revision 01 dated 13 February 2023,
Revision 02 dated 13 March 2023, Revision 03 dated 13 September 2023, or Revision 04 dated 04 March 2026.
Airbus SB A350-53-P089 original issue dated 19 December 2025.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1.
If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2.
Based on the required actions and the compliance time, the original issue of this AD was posted on 06 October 2023 as Final AD with Request for Comments, postponing the public consultation process until after publication.
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.
|
