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PAD 24-085R1 : Fuselage – Double Joggle Area at Frame 16 and Frame 20 – Inspection

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Number 24-085R1
Issued by Europe  Europe
Issue date 2024-09-30
EASA approval number
Contributor EASA Large Aeroplanes Department
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
    • A320
      • A320-211
      • A320-212
      • A320-214
      • 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 This PAD is republished for consultation for additional 2 weeks after comments were received and the Required Action(s) and Compliance Time(s) paragraph (2) was adapted and paragraph (3) was added.
Correction Not applicable
Supersedure This AD supersedes EASA AD 2023-0212 dated 06 December 2023.
Publication(s) and related information SB A320-53-1373 original issue dated 14 June 2018, or Revision 01 dated 03 December 2021, or Revision 2 dated 16 November 2023. Airbus SB A320-53-1374 original issue dated 14 June 2018, or Revision 01 dated 03 December 2021, or Revision 2 dated 16 November 2023. Airbus SB A320-53-1375 original issue dated 01 December 2022. Airbus SB A320-53-1376 original issue dated 01 December 2022. Airbus SB A320-53-1378 original issue dated 14 June 2018, or Revision 01 dated 17 September 2019, or Revision 02 dated 20 April 2023. Airbus SB A320-53-1379 original issue dated 14 June 2018, or Revision 01 dated 17 September 2019, or Revision 02 dated 13 January 2021, or Revision 03 dated 20 April 2023. Airbus SB A320-53-1380 original issue dated 14 June 2018, or Revision 01 dated 13 September 2019, or Revision 02 dated 20 April 2023. Airbus SB A320-53-1381 original issue dated 14 June 2018, or Revision 01 dated 18 September 2019, or Revision 02 dated 20 April 2023. Airbus SB A320-53-1422 original issue dated 01 December 2022. Airbus SB A320-53-1423 original issue dated 01 December 2022, or Revision 01 dated 23 October 2023. Airbus SB A320-53-1424 original issue dated 01 December 2022. Airbus SB A320-53-1425 original issue dated 01 December 2022. 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 14 October 2024. 2. The original issue of this PAD was posted on 12 July 2024 for consultation until 09 August 2024. 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. 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.