Safety Publications Tool

2025-0111 : Fuselage – Service Door Stop Fitting Hole – Inspection / Repair

Number 2025-0111
Issued by Europe  Europe
Issue date 2025-05-14
Effective date 2025-05-28
EASA approval number
ATA Chapter 53
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 Not applicable
Supersedure This AD supersedes EASA AD 2018-0289R1 dated 10 February 2021.
Publication(s) and related information Airbus SB A320-53-1330 original issue dated 01 November 2017, or Revision 01 dated 07 April 2021, or Revision 02 dated 27 February 2024. Airbus SB A320-53-1339 original issue dated 01 November 2017, or Revision 01 dated 07 April 2021, or Revision 02 dated 07 December 2022, or Revision 03 dated 05 March 2024. Airbus SB A320-53-1386 original issue dated 18 April 2019, or Revision 01 dated 12 November 2024. Airbus SB A320-53-1387 original issue dated 18 April 2019, or Revision 01 dated 12 November 2024. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 25-031
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 07 February 2025 as PAD 25-031 for consultation until 07 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.