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2025-0274 : [Correction] Fire Protection – Fire Panel – Inspection

Number 2025-0274
Issued by Europe  Europe
Issue date 2025-12-11
Effective date 2025-12-16
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 Not applicable
Correction This AD is re-published to correct the reference to a certain part in the SB in paragraph (7) of this AD.
Supersedure This AD supersedes 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. Airbus SB A320-26-1138 original issue dated 20 June 2025, Revision 1 dated 10 July 2025 or Revision 2 dated 11 September 2025. SAFRAN VSB 330TS08Y-26-001 original issue dated 30 September 2024. SAFRAN VSB 335TS08Y-26-006 original issue dated 22 October 2024. 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 29 January 2026: The Comment Response Document has been published and notified. No changes have been made to the AD in response to the comments received. 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 09 December 2025 postponing the public consultation until 06 January 2026. 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.