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ADs [at] easa.europa [dot] eu
|
| Number |
25-135 |
| Issued by |
 Europe |
| Issue date |
2025-09-01 |
| EASA approval number |
|
| ATA Chapter |
53 |
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
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2015-0217 dated 30 October 2015.
|
| Publication(s) and related information |
Airbus SB A300-53-6177 original issue dated 20 May 2015, or Revision 1 dated 06 July 2018, or Revision 2 dated 18 July 2025.
Airbus SB A300-53-6176 original issue dated 20 May 2015, or Revision 1 dated 29 November 2016, or Revision 2 dated 06 August 2018.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. This Proposed AD will be closed for consultation on 29 September 2025.
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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