| Publication(s) and related information |
ATR AOM 2020/13 Issue 1 dated 28 September 2020, Issue 2 dated 14 October 2020, Issue 3 dated 09 November 2020, or Issue 4 dated 28 January 2021.
ATR SB ATR42-27-0113 original issue dated 09 December 2020, or Revision 01 dated 10 March
2021.
ATR SB ATR42-31-0121 original issue dated 12 May 2023.
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 05 June 2023 as PAD 23-063 for consultation until 03 July 2023.
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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