| Publication(s) and related information |
ATR SB ATR42-31-0111 original issue dated 09 July 2019, or Revision 01 dated 12 December 2019, or Revision 02 dated 04 July 2022.
ATR SB ATR42-31-0112 original issue dated 04 September 2019, or Revision 01 dated 12 December 2019.
ATR SB ATR72-31-1117 original issue dated 09 July 2019, or Revision 01 dated 26 July 2019, or Revision 02 dated 27 November 2019, or Revision 03 dated 25 March 2020, or Revision 04 dated 30 July 2020.
ATR SB ATR72-31-1118 original issue dated 12 December 2019, or Revision 01 dated 12 December 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. This AD was posted on 30 August 2022 as PAD 22-120 for consultation until 27 September 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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