Safety Publications Tool

2025-0083R1 : Equipment/Furnishings – Cargo Bulkhead Frame 24A Vertical Members – Inspection

Number 2025-0083R1
Issued by Europe  Europe
Issue date 2026-03-24
Effective date 2026-03-31
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
      • 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 2025-0083 dated 14 April 2025.
Correction Not applicable
Supersedure The original issue of this AD supersedes EASA AD 2024-0231 dated 04 December 2024.
Publication(s) and related information Airbus SB A320-25-1CFU original issue dated 26 September 2024 or revision 01 dated 02 July 2025. Airbus SB A320-25-1CFV original issue dated 26 September 2024 or revision 01 dated 02 July 2025. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
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 14 April 2025 as Final AD with Request for Comments, postponing the public consultation process until 12 May 2025. No comments were received during the consultation period. 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.