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ADs [at] easa.europa [dot] eu
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| Number |
25-047R1 |
| Issued by |
 Europe |
| Issue date |
2025-03-13 |
| EASA approval number |
|
| Contributor |
EASA Large Aeroplanes Department |
| ATA Chapter |
55 |
Approval Holder
/ Type Designation |
|
| Revision |
This PAD is revised to include certain MSN from Group 2 that were missing from the original issue.
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2023-0125 dated 22 June 2023.
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| Publication(s) and related information |
ATR SB ATR42-55-0020 original issue dated 02 March 2023, or Revision 01 dated 24 July 2023, or Revision 02 dated 03 September 2024, or Revision 03 dated 31 January 2025.
ATR SB ATR72-55-1013 original issue dated 02 March 2023, or Revision 01 dated 24 July 2023, or Revision 02 dated 03 September 2024, or Revision 03 dated 31 January 2025.
ATR SB ATR42-55-0025 original issue dated 03 February 2025.
ATR SB ATR72-55-1018 original issue dated 03 February 2025.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. This Proposed AD will be closed for consultation on 10 April 2025.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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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