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PAD 25-191 : Equipment / Furnishings – Galley – Inspection

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Number 25-191
Issued by Europe  Europe
Issue date 2025-12-15
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 2025-0068 dated 28 March 2025.
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 or Revision 03 dated 05 June 2024. Airbus SB A320-25-1BVT original issue dated 18 December 2020, or Revision 1 dated 17 June 2022 or Revision 2 dated 05 June 2024. 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.
Remarks 1. This Proposed AD will be closed for consultation on 12 January 2025. 2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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.

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