| Number |
2024-0078 |
| Issued by |
 Europe |
| Issue date |
2024-03-20 |
| Effective date |
2024-04-03 |
| EASA approval number |
|
| Contributor |
EASA Large Aeroplanes Department |
| ATA Chapter |
25 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2022-0196 dated 20 September 2022.
|
| Publication(s) and related information |
Airbus AOT A25P023-22 original issue dated 20 September 2022, Revision 01 dated 27 September 2022, Revision 02 dated 30 November 2023 and Revision 03 dated 16 January 2024.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
24-026 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 19 February 2024 as PAD 24-026 for consultation until 18 March 2024.
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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