| Publication(s) and related information |
ATR SB ATR42-53-0151 original issue dated 20 February 2020, or Revision 1 dated 29 June 2020, or Revision 2 dated 18 January 2023.
ATR SB ATR72-53-1108 original issue dated 26 February 2020, or Revision 1 dated 29 June 2020, or Revision 2 dated 18 January 2023.
ATR SB ATR42-53-0160 original issue dated 07 July 2025.
ATR SB ATR72-53-1120 original issue dated 07 July 2025.
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 25 July 2025 as PAD 25-112 for consultation until 22 August 2025. 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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