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ADs [at] easa.europa [dot] eu
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| Number |
25-088 |
| Issued by |
 Europe |
| Issue date |
2025-06-18 |
| EASA approval number |
|
| ATA Chapter |
29 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2025-0035 dated 12 February 2025.
|
| Publication(s) and related information |
Airbus SB A350-29-P051 original issue dated 28 October 2024, or revision 01 dated 20 December 2024, or revision 02 dated 11 April 2025.
Airbus SB A350-29-P052 original issue dated 28 October 2024, or revision 01 dated 06 February 2025, or revision 02 dated 06 May 2025.
Airbus SB A350-42-P020 original issue dated 10 August 2023.
Airbus A350 AFM DU 00025056.0001001 dated 11 September 2019.
Airbus A350 AFM DU 00025057.0001001 dated 11 September 2019.
Airbus A350 AFM DU 00025058.0001001 dated 11 September 2019.
Airbus A350 AFM DU 00025059.0001001 dated 11 September 2019.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| Remarks |
1. This Proposed AD will be closed for consultation on 02 July 2025.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred
on a product, part or appliance not affected by this PAD, 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 PAD 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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