Please feel free to send us your comments by email at
ADs [at] easa.europa [dot] eu
|
| Number |
26-109 |
| Issued by |
 Europe |
| Issue date |
2026-09-18 |
| EASA approval number |
|
| ATA Chapter |
57 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A300-600
-
A300B4-603
-
A300B4-605R
-
A300B4-622
-
A300B4-622R
-
A300C4-605R variant F
-
A300F4-605R
-
A300F4-622R
-
A300-600ST (Beluga)
-
A310
-
A310-203
-
A310-222
-
A310-304
-
A310-308
-
A310-322
-
A310-324
-
A310-325
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus SB A300-57-6126 original issue dated 10 July 2026.
Airbus SB A310-57-2109 original issue dated 16 July 2026.
Airbus SB A300-57-9038 original issue dated 16 July 2026.
Airbus A300-57-6106 Rev 1 (original issue) dated 22 May 2007, or Rev 2 dated 18 June 2010, or Rev 3 dated 26 January 2012, or Rev 4 dated 24 July 2014.
Airbus A310-57-2090 Rev 1 (original issue) dated 22 May 2007, or Rev 2 dated 18 June 2010, or Rev 3 dated 23 January 2012, or Rev 4 dated 24 July 2014.
Airbus SB A310-57-2101 original issue dated 13 January 2012, or Rev 1 dated 21 September 2017.
Airbus SB A300-57-6112 original issue dated 13 January 2012.
Airbus SB A300-57-9024 original issue dated 13 January 2012. |
| Remarks |
1. This Proposed AD will be closed for consultation on 16 October 2026.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa[dot]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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