| 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. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 18 June 2025 as PAD 25-088 for consultation until 02 July 2025.
The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed ('zipped') file, attached to the record for this AD.
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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