Safety Publications Tool

2020-0085R1 : Powerplant – Aft Engine Mount Retainers – Replacement

Number 2020-0085R1
Issued by Europe  Europe
Issue date 2021-08-06
Effective date 2021-08-13
EASA approval number
ATA Chapter 71
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A318
      • A318-111
      • A318-112
    • A319
      • A319-111
      • A319-112
      • A319-113
      • A319-114
      • A319-115
    • A320
      • A320-211
      • A320-212
      • A320-214
      • A320-215
      • A320-216
    • A321
      • A321-111
      • A321-112
      • A321-211
      • A321-212
      • A321-213
Revision This AD revises EASA AD 2020-0085 dated 06 April 2020.
Correction Not applicable
Supersedure The original issue of this AD superseded EASA AD 2017-0251 dated 15 December 2017.
Publication(s) and related information Airbus AOT A71N001-12 rev. 01 dated 09 August 2012, or rev. 02 dated 27 February 2013. Airbus AOT A71N011-15 original issue dated 16 September 2015, or rev. 01 dated 01 February 2016. Airbus SB A320-71-1060 original issue dated 09 October 2014, or rev. 01 dated 07 April 2015, or rev. 02 dated 18 December 2015. Airbus SB A320-71-1071 original issue dated 08 November 2016, or rev. 01 dated 17 October 2017, or rev. 02 dated 22 October 2019. Goodrich Aerostructures SB RA32071-146 rev. 02 dated 26 July 2012. Goodrich Aerostructures SB RA32071-160 original issue dated 18 September 2014 or rev.01 dated 23 September 2016. Goodrich Aerostructures SB RA32071-164 original issue dated 06 October 2016, or rev. 01 dated 19 July 2017, or rev. 02 dated 04 April 2018, or rev. 03 dated 14 September 2018. Goodrich Aerostructures SB RA32071-174 original issue dated 17 September 2019. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 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.