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2020-0037 : [Correction] Fuselage – Frame Foot Coupling at Frame 43 – Inspection / Repair

Number 2020-0037
Issued by Europe  Europe
Issue date 2020-02-28
Effective date 2020-03-12
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 Not applicable
Correction This AD is republished to correct typographical errors.
Supersedure None
Publication(s) and related information Airbus SB A320-53-1269 original issue dated 17 January 2013, or Revision 01 dated 10 July 2013, or Revision 02 dated 07 February 2019. Airbus SB A320-53-1270 original issue dated 17 January 2013, or Revision 01 dated 27 September 2013, or Revision 02 dated 11 April 2014. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 19-209
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 28 November 2019 as PAD 19-209 for consultation until 26 December 2019. 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.