| Number |
2025-0151R2 |
| Issued by |
 Europe |
| Issue date |
2025-09-12 |
| Effective date |
2025-09-19 |
| EASA approval number |
|
| ATA Chapter |
25 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A321
-
A321-251NX
-
A321-252NX
-
A321-253NX
-
A321-271NX
-
A321-272NX
|
| Revision |
This AD revises EASA AD 2025-0151R1 dated 25 July 2025
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2022-0176 dated 24 August 2022 and EASA AD 2024-0057 dated 28 February 2024.
|
| Publication(s) and related information |
Airbus AOT A25N024-22 original issue dated 03 August 2022.
Airbus AOT A25N027-23 original issue dated 16 January 2024 or Revision 01 dated 26 February 2024.
Airbus SB A320-25-1CJM original issue dated 10 December 2024.
Safran SB 005-25-37 original issue dated 01 August 2022 or Revision 1 dated 06 April 2023.
Safran SB 005-25-38 original issue dated 01 August 2022 or Revision 1 dated 06 April 2023.
Safran SB 005-25-45 Revision 1 dated 09 February 2024 or Revision 2 dated 22 July 2024.
Safran SB 005-25-46 Revision 1 dated 09 February 2024 or Revision 2 dated 22 July 2024.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
25-077 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 26 May 2025 as PAD 25-077 for consultation until 16 June 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.
|
