| Number |
2025-0236 |
| Issued by |
 Europe |
| Issue date |
2025-10-23 |
| Effective date |
2025-11-06 |
| 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. |
| PAD number |
25-135 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 01 September 2025 as PAD 25-135 for consultation until 29 September 2025. 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.
|
