Publication(s) and related information |
Airbus SB A330-32-3240 original issue dated 08 December 2010, or Revision 01 dated 02 May 2011, or Revision 02 dated 02 December 2011, or Revision 03 dated 13 December 2012, or Revision 04 dated 16 April 2014, or Revision 05 dated 03 November 2014, or Revision 06 dated 22 December 2015, or Revision 07 dated 18 April 2016, or Revision 08 dated 04 April 2017, or Revision 09 dated 22 July 2019, or Revision 10 dated 25 March 2021, or Revision 11 dated 19 July 2022.
Airbus SB A340-32-4281 original issue dated 08 December 2010, or Revision 01 dated 02 December 2011, or Revision 02 dated 03 November 2014.
Airbus SB A340-32-5096 original issue dated 08 December 2010, or Revision 01 dated 02 December 2011, or Revision 02 dated 03 November 2014.
Airbus SB A330-32-3290 original issue dated 26 December 2017.
Airbus SB A330-32-3291 original issue dated 28 September 2018.
Airbus SB A340-32-4315 original issue dated 26 December 2017.
Airbus SB A340-32-4316 original issue dated 28 September 2018.
Safran Landing Systems SB A33/34-32-285 original issue dated 09 July 2010, or Revision 01 dated 04 October 2011, or Revision 02 dated 04 October 2012, or Revision 03 dated 11 September 2013, or Revision 04 dated 23 January 2014, or Revision 05 dated 14 August 2014, or Revision 06 dated 06 August 2015, or Revision 07 dated 24 November 2016.
Safran Landing Systems SB A34/56C-32-117 original issue dated 09 July 2010, or Revision 01 dated 04 October 2011, or Revision 02 dated 11 September 2013, or Revision 03 dated 31 March 2014.
Safran Landing Systems SB A34/56M-32-46 original issue dated 09 July 2010, or Revision 01 dated 04 October 2011, or Revision 02 dated 11 September 2013, or Revision 03 dated 31 March 2014.
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. The original issue of this AD was posted on 12 November 2021 as PAD 21-169 for consultation until 10 December 2021. The Revision 02 of this AD was posted on 05 July 2022 as PAD 22-088 for consultation until 02 August 2022. 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 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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