| Number |
2025-0058R1 |
| Issued by |
 Europe |
| Issue date |
2025-03-19 |
| Effective date |
2025-03-31 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A340
-
A340-211
-
A340-212
-
A340-213
-
A340-311
-
A340-312
-
A340-313
|
| Revision |
This AD revises EASA AD 2025-0058 dated 17 March 2025.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus A340 ALS Part 4, SEMR Variation 8.1 dated 21 December 2023.
The use of later approved variations or revisions of the above-mentioned document, or of an ALS revision which includes the technical content of the Variation, is acceptable for compliance with the requirements of this AD. |
| PAD number |
25-020 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 29 January 2025 as PAD 25-020 for consultation until 26 February 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.
|
