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2025-0068 : Equipment / Furnishings – Galleys – Inspection

Number 2025-0068
Issued by Europe  Europe
Issue date 2025-03-28
Effective date 2025-04-11
EASA approval number
ATA Chapter 25
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
    • 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
      • A321-271N
      • A321-271NX
      • A321-272N
      • A321-272NX
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2024-0038 dated 05 February 2024.
Publication(s) and related information Airbus SB A320-25-1BVS original issue dated 18 December 2020, or Revision 1 dated 17 June 2022, or Revision 2 dated 10 August 2022. Airbus SB A320-25-1BVT original issue dated 18 December 2020, or Revision 1 dated 17 June 2022. Airbus SB A320-25-1CBN original issue dated 12 August 2022, or Revision 1 dated 20 March 2023, or Revision 02 dated 30 August 2024. Airbus SB A320-25-1CBP original issue dated 12 August 2022, or Revision 1 dated 20 March 2023, or Revision 02 dated 30 August 2024. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 25-025
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 03 February 2025 as PAD 25-025 for consultation until 03 March 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.