| Number |
2025-0286 |
| Issued by |
 Europe |
| Issue date |
2025-12-17 |
| Effective date |
2025-12-31 |
| EASA approval number |
|
| ATA Chapter |
23 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2025-0043R1, including its Correction, dated 31 July 2025.
|
| Publication(s) and related information |
Airbus OEB 58 issue 1.0.
Airbus SB A330-23-3514 original issue dated 24 October 2025.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
Airbus A330/A340 MMEL MER dated 10 February 2025. |
| PAD number |
25-174 |
| Remarks |
1.
If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2.
This AD was posted on 13 November 2025 as PAD 25-174 for consultation until 11 December 2025. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa[dot]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
|
