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2020-0153 : Fuselage – Rear Fuselage Clips, Shear Webs and Angles – Replacement

Number 2020-0153
Issued by Europe  Europe
Issue date 2020-07-10
Effective date 2020-07-24
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • 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 Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2014-0177 dated 25 July 2014.
Publication(s) and related information Airbus SB A320-53-1266 original issue dated 11 January 2013, or Revision 01 dated 20 June 2013, or Revision 02 dated 13 August 2014, or Revision 03 dated 07 May 2015, or Revision 04 dated 07 June 2016, or Revision 05 dated 24 March 2017, or Revision 06 dated 30 November 2017, or Revision 07 dated 18 May 2018, or Revision 08 dated 11 January 2019, or Revision 09 dated 25 February 2019. Airbus SB A320-53-1363 original issue dated 03 March 2020. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 20-088
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 28 May 2020 as PAD 20-088 for consultation until 25 June 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 Programming and Continued Airworthiness 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.