Please feel free to send us your comments by email at
ADs [at] easa.europa [dot] eu
|
| Number |
26-053 |
| Issued by |
 Europe |
| Issue date |
2026-04-21 |
| EASA approval number |
|
| ATA Chapter |
24 |
Approval Holder
/ Type Designation |
-
ATR
-
ATR42
-
ATR72
-
101
-
102
-
201
-
202
-
211
-
212
-
212A
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2023-0078R1 dated 20 April 2023.
|
| Publication(s) and related information |
ATR AOM 2021/05 issue 1 dated 19 April 2021, issue 2 dated 03 May 2021, issue 3 dated 11 May
2021, issue 4 dated 16 March 2022, issue 5 dated 30 November 2022, issue 6 dated 07 March 2023,
issue 7 dated 13 April 2023 and issue 8 dated 20 April 2023.
ATR SB ATR42-24-0062 original issue dated 01 March 2023, or Revision 01 dated 16 May 2023.
ATR SB ATR72-24-1032 original issue dated 01 March 2023, or Revision 01 dated 16 May 2023.
ATR SB ATR42-24-0063 original issue dated 26 January 2026.
ATR SB ATR72-24-1033 original issue dated 26 January 2026.
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 19 May 2026.
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.
|
