| Number |
2025-0276 |
| Issued by |
 Europe |
| Issue date |
2025-12-10 |
| Effective date |
2025-12-24 |
| EASA approval number |
|
| ATA Chapter |
57 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A380
-
A380-841
-
A380-842
-
A380-861
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2025-0074 dated 07 April 2025.
|
| Publication(s) and related information |
Airbus SB A380-57-8148 Revision 01 dated 06 February 2020.
Airbus SB A380-57-8269 original issue dated 06 February 2020.
Airbus RI R575-40267 original Issue (Issue A) dated 11 December 2017, or Issue B dated 28 November 2024.
Airbus RI R575-42389 original Issue (Issue A) dated 20 February 2025, or Issue B dated 04 March 2025.
Airbus RI R575-42397 original Issue (Issue A) dated 18 March 2025.
Airbus RI R575-58442 original Issue (Issue A) dated June 2016, or Issue B dated August 2017, or Issue C dated December 2017, or Issue D dated 26 November 2024. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
29 January 2026: The Comment Response Document has been published and notified. No changes have been made to the AD in response to the comments received. 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 10 December 2025 postponing the public consultation until 07 January 2026. 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.
|
