Safety Publications Tool

2020-0040R1 : Fuselage – Overwing Emergency Exit Cut-Outs in Section 15 – Modification

Number 2020-0040R1
Issued by Europe  Europe
Issue date 2020-06-16
Effective date 2020-06-23
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
Revision This AD revises EASA AD 2020-0040 dated 28 February 2020.
Correction Not applicable
Supersedure The original issue of this AD superseded DGAC France AD 2002-259(B) dated 15 May 2002.
Publication(s) and related information Airbus SB A320-53-1274 original issue dated 15 July 2014, or Rev. 01 dated 18 June 2015, or Rev. 02 dated 16 September 2016, or Rev. 03 dated 09 June 2017. Airbus SB A320-53-1277 original issue dated 29 January 2013, or Rev. 01 dated 03 November 2016, or Rev. 02 dated 11 September 2019. Airbus SB A320-53-1031 original issue dated 09 December 1994, or Rev. 01 dated 14 November 1997, or Rev. 02 dated 05 December 2001. Airbus SB A320-53-1032 original issue dated 09 December 1994, or Rev. 01 dated 15 January 1998, or Rev. 02 dated 05 December 2001. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 14-144R2
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 09 October 2014 as PAD 14-144, then republished on 02 November 2015 as PAD 14-144R1 for consultation until 30 November 2015, then republished on 22 June 2017 as PAD 14-144R2 for consultation until 20 July 2017. 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.