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2022-0204R1 : [Correction] Landing Gear – Main Landing Gear Sliding Tube – Inspection / Replacement

Number 2022-0204R1
Issued by Europe  Europe
Issue date 2023-02-17
Effective date 2023-02-22
EASA approval number
ATA Chapter 32
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 2022-0204 dated 30 September 2022.
Correction This AD is re-published to delete an erroneous reference to Note 4 - which does not exist.
Supersedure The original issue of this AD superseded EASA AD 2018-0135R1 dated 06 July 2018.
Publication(s) and related information Airbus SB A320-32-1441, original issue dated 28 December 2016, or Revision 01 dated 14 December 2017, or Revision 02 dated 23 August 2022. Airbus SB A320-32-1416 original issue dated 10 March 2014. Safran SB 200-32-321 original issue dated 09 September 2015, or Revision 01 dated 01 November 2016, or Revision 02 dated 03 October 2017, or Revision 03 dated 08 January 2020, or Revision 04 dated 03 November 2021. Safran SB 201-32-68 original issue dated 09 September 2015, or Revision 01 dated 01 November 2016, or Revision 02 dated 03 October 2017, or Revision 03 dated 08 January 2020, or Revision 04 dated 03 November 2021. Safran SB 200-32-286 original issue dated 03 September 2004, or Revision 01 dated 01 May 2005, or Revision 02 dated 15 June 2007, or Revision 03 dated 03 October 2008. Safran SB 201-32-43 original issue dated 03 September 2004, or Revision 01 dated 01 May 2005, or Revision 02 dated 15 June 2007, or Revision 03 dated 03 October 2008. Safran SB 200-32-313 original issue dated 25 February 2013, or Revision 01 dated 24 June 2014. Safran SB 201-32-62 original issue dated 25 February 2013, or Revision 01 dated 24 June 2014. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 22-104
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 29 July 2022 as PAD 22-104 for consultation until 26 August 2022. 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.