| Number |
2025-0104 |
| Issued by |
 Europe |
| Issue date |
2025-05-07 |
| Effective date |
2025-05-21 |
| EASA approval number |
|
| ATA Chapter |
36 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2023-0111R1 dated 28 May 2024.
|
| Publication(s) and related information |
Airbus AOT A36L009-22 original issue dated 25 August 2022, Revision 01 dated 03 October 2022, Revision 02 dated 15 May 2023 or Revision 03 dated 24 April 2024.
Airbus AFM-TR 811 issue 1, EASA approval date 25 August 2022.
Airbus AFM-TR 813 issue 1, EASA approval date 10 May 2023.
Airbus SB A330-36-3055 original issue dated 31 May 2024, and revision 1 dated 14 November 2024.
Airbus SB A330-36-3057 original issue dated 28 October 2024.
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 25 August 2022.
Airbus A330/A340 MMEL MER dated 10 February 2025. |
| PAD number |
25-055 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 26 March 2025 as PAD 25-055 for consultation until 23 April 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.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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