| Publication(s) and related information |
Airbus SB A300-57-9001 Revision 01 dated 22 August 2017, or Revision 02 dated 27 March 2018, or Revision 03 dated 16 July 2025.
Airbus SB A300-57-9002 Revision 02 dated 22 August 2017, or Revision 03 dated 07 February 2019, or Revision 04 dated 25 June 2025.
Airbus SB A300-57-9016 original issue dated 13 June 2005.
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 01 October 2025 as PAD 25-155 for consultation until 29 October 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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