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ADs [at] easa.europa [dot] eu
|
| Number |
26-133 |
| Issued by |
 Europe |
| Issue date |
2026-11-04 |
| EASA approval number |
|
| ATA Chapter |
52 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A310
-
A310-203
-
A310-203C
-
A310-221
-
A310-222
-
EASA STC 10013960
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2024-0092R1 dated 10 July 2024.
|
| Publication(s) and related information |
Airbus AOT A52W016-24 original issue dated 18 March 2024, or Revision 01 dated 01 July 2024.
The use of later approved revisions of the above-mentioned document is acceptable for compliance
with the requirements of this AD. |
| Remarks |
1. This Proposed AD will be closed for consultation on 02 December 2026.
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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