| Publication(s) and related information |
Airbus AOT A57N018-21 original issue dated 08 November 2021, or Rev. 01 dated 14 June 2023.
Airbus SB A320-57-1173 original issue dated 31 January 2013, or Rev. 01 dated 30 April 2013, or Rev. 02 dated 30 July 2013, or Rev. 03 dated 18 September 2013, or Rev. 04 dated 11 February 2014.
Airbus SB A320-57-1186 original issue dated 13 August 2013, or Rev. 01 dated 14 October 2013, or Rev. 02 dated 26 November 2013, or Rev. 03 dated 30 April 2014, or Rev. 04 dated 17 July 2014, or Rev. 05 dated 19 September 2014, or Rev. 06 dated 17 October 2014, or Rev. 07 dated 24 November 2014, or Rev. 08 dated 26 January 2015, or Rev. 09 dated 26 March 2015, or Rev. 10 dated 12 February 2016, or Rev. 11 dated 18 August 2020, or Rev. 12 dated 26 July 2021, or Rev. 13 dated 21 January 2022, or Rev. 14 dated 03 May 2022, or Rev. 15 dated 09 January 2023.
Airbus SB A320-57-1187 original issue dated 13 October 2013, or Rev. 01 dated 07 March 2014, or Rev. 02 dated 31 July 2014, or Rev. 03 dated 27 November 2014, or Rev. 04 dated 27 March 2015, or Rev. 05 dated 10 July 2015, or Rev. 06 dated 19 October 2015, or Rev. 07 dated 01 February 2016, or Rev. 08 dated 13 December 2016, or Rev. 09 dated 21 April 2017, or Rev. 10 dated 21 March 2018, or Rev. 11 dated 04 October 2019, or Rev. 12 dated 18 January 2022, or Rev. 13 dated 03 May 2022.
Airbus SB A320-57-1193 original issue dated 16 October 2015, or Rev. 01 dated 15 February 2016, or Rev. 02 dated 18 May 2016, or Rev. 03 dated 03 August 2016, or Rev. 04 dated 30 September 2016, or Rev. 05 dated 28 November 2016, or Rev. 06 dated 04 July 2017, or Rev. 07 dated 01 December 2017, or Rev. 08 dated 27 February 2018.
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. This AD was posted on 21 October 2024 as PAD 24-124 for consultation until 18 November 2024. 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 Safety 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.
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