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2024-0147R1 : Fuselage – Centre Fuselage Forward Pressure Bulkhead – Inspection

Number 2024-0147R1
Issued by Europe  Europe
Issue date 2024-08-07
Effective date 2024-08-13
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
    • A320
      • A320-211
      • A320-212
      • A320-214
      • A320-215
      • A320-216
      • A320-231
      • A320-232
      • A320-233
    • A321
      • A321-111
      • A321-112
      • A321-131
      • A321-211
      • A321-212
      • A321-213
      • A321-231
      • A321-232
Revision This AD revises EASA AD 2024-0147 dated 30 July 2024, which superseded EASA AD 2014-0209 dated 19 September 2014
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus SB A320-53-1268 original issue dated 08 January 2013, or Revision 01 dated 23 July 2013, or Revision 02 dated 15 July 2014, or Revision 03 dated 07 May 2015, or Revision 04 dated 29 July 2016, or Revision 05 dated 02 June 2017, or Revision 06 dated 30 November 2017. Airbus SB A320-53-1372 original issue dated 15 May 2018, or Revision 01 dated 25 July 2019 or Revision 02 dated 09 September 2021. Airbus SB A320-53-1383 original issue dated 05 March 2019. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 20-042
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The original issue of this AD was posted on 26 February 2020 as PAD 20-042 for consultation until 25 March 2020. 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.