Safety Publications Tool

2020-0019 : Fuselage – Lateral Window Frame Upper Fastener Holes – Inspection

Number 2020-0019
Issued by Europe  Europe
Issue date 2020-02-05
Effective date 2020-02-19
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 Not applicable
Supersedure None
Publication(s) and related information Airbus SB A320-53-1335 original issue dated 12 March 2019. Airbus SB A320-53-1336 original issue dated 12 March 2019. Airbus SB A320-53-1448 original issue dated 05 August 2019. Airbus SB A320-53-1449 original issue dated 05 August 2019. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 19-169
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD This Proposed AD will be closed for consultation on 08 October 2019. 2. This AD was posted on 10 September 2019 as PAD 19-169 for consultation until 08 October 2019. The Comment Response Documents 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.