| Number |
2025-0274R1 |
| Issued by |
 Europe |
| Issue date |
2026-07-07 |
| Effective date |
2026-07-14 |
| EASA approval number |
|
| ATA Chapter |
26 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A318
-
A318-111
-
A318-112
-
A318-121
-
A318-122
-
A319
-
A319-111
-
A319-112
-
A319-113
-
A319-114
-
A319-115
-
A319-131
-
A319-132
-
A319-133
-
A319-151N
-
A319-153N
-
A319-171N
-
A319-173N
-
A320
-
A320-211
-
A320-212
-
A320-214
-
A320-215
-
A320-216
-
A320-231
-
A320-232
-
A320-233
-
A320-251N
-
A320-252N
-
A320-253N
-
A320-271N
-
A320-272N
-
A320-273N
-
A321
-
A321-111
-
A321-112
-
A321-131
-
A321-211
-
A321-212
-
A321-213
-
A321-231
-
A321-232
-
A321-251N
-
A321-251NX
-
A321-252N
-
A321-252NX
-
A321-253N
-
A321-253NX
-
A321-253NY
-
A321-271N
-
A321-271NX
-
A321-271NY
-
A321-272N
-
A321-272NX
|
| Revision |
This AD revises EASA AD 2025-0274 dated 09 December 2025, including its correction dated 11 December 2025.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2025-0253 dated 14 November 2025.
|
| Publication(s) and related information |
Airbus SB A320-26-1137 original issue dated 20 June 2025, Revision 1 dated 10 July 2025, or Revision 2 dated 11 September 2025, or Revision 03 dated 12 March 2026.
Airbus SB A320-26-1138 original issue dated 20 June 2025, Revision 1 dated 10 July 2025, or Revision 2 dated 11 September 2025, or Revision 03 dated 12 March 2026.
SAFRAN VSB 330TS08Y-26-001 original issue dated 30 September 2024, or Revision 1 dated 31 March 2026.
SAFRAN VSB 335TS08Y-26-006 original issue dated 22 October 2024, or Revision 1 dated 20 March 2026.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
SAFRAN SIL 306-26-001 at original issue dated 03 December 2024. |
| Remarks |
1.
If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. Based on the required actions and the compliance time, the original issue of this AD was posted on 09 December 2025 as Final AD with Request for Comments, postponing the public consultation process until 06 January 2026. The Comment Response Document can be found in the EASA Safety Publications Tool, in a 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.
|
