| Number |
2026-0047 |
| Issued by |
 Europe |
| Issue date |
2026-03-10 |
| Effective date |
2026-03-24 |
| EASA approval number |
|
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A300-600
-
A300B4-603
-
A300B4-605R
-
A300B4-622
-
A300B4-622R
-
A310
-
A310-203
-
A310-222
-
A310-304
-
A310-308
-
A310-322
-
A310-324
-
A310-325
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2022-0078 dated 04 May 2022.
|
| Publication(s) and related information |
Airbus SB A310-53-2138 original issue dated 28 May 2014, or Revision 01 dated 14 December 2021, or Revision 02 dated 18 November 2025.
Airbus SB A300-53-6175 original issue dated 28 May 2014, or Revision 01 dated 07 December 2021, or Revision 02 17 July 2023, or Revision 03 dated 18 November 2025.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
26-013 |
| Remarks |
1.
If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2.
This AD was posted on 26 January 2026 as PAD 26-013 for consultation until 16 February 2026. 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.
|
