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PAD 25-108 : Fuselage – Centre Fuselage / Main Landing Gear Door Keel Beam Hinge and Actuator Fittings – Inspection

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Number 25-108
Issued by Europe  Europe
Issue date 2025-07-22
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
      • A321-271N
      • A321-271NX
      • A321-272N
      • A321-272NX
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2024-0097R2 dated 12 July 2024.
Publication(s) and related information Airbus SB A320-53-1195 Revision 03 dated 08 November 2011, or Revision 04 dated 22 August 2012, or Revision 05 dated 22 November 2013, or Revision 06 dated 29 August 2014, or Revision 07 dated 28 July 2016, or Revision 08 dated 27 September 2017, or Revision 09 dated 23 October 2018, or Revision 10 dated 11 June 2021, or Revision 11 dated 08 November 2023. Airbus SB A320-53-1196 Revision 02 dated 08 November 2011, or Revision 03 dated 22 August 2012, or Revision 04 dated 22 November 2013, or Revision 05 dated 29 August 2014, or Revision 06 dated 28 July 2016, or Revision 07 dated 27 September 2017, or Revision 08 dated 23 October 2018, or Revision 09 dated 17 December 2020, or Revision 10 dated 08 November 2023. Airbus SB A320-53-1325 original issue dated 26 April 2016, or Revision 01 dated 22 December 2017, or Revision 02 dated 14 January 2019, or Revision 03 dated 23 June 2021, or Revision 04 dated 07 November 2023, or Revision 05 dated 05 February 2025. Airbus SB A320-53-1326 original issue dated 05 July 2016, or Revision 01 dated 22 December 2017, or Revision 02 dated 10 February 2021, or Revision 03 dated 07 November 2023. Airbus SB A320-53-1502 original issue dated 07 November 2023. Airbus SB A320-53-1503 original issue dated 07 November 2023. 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 19 August 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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