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ADs [at] easa.europa [dot] eu
|
| Number |
24-129 |
| Issued by |
 Europe |
| Issue date |
2024-10-25 |
| EASA approval number |
|
| Contributor |
EASA Large Aeroplanes Department |
| ATA Chapter |
27 |
Approval Holder
/ Type Designation |
-
ATR
-
ATR42
-
ATR72
-
101
-
102
-
201
-
202
-
211
-
212
-
212A
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
ATR SB ATR42-27-0115 original issue dated 09 August 2024.
ATR SB ATR42-27-0118 original issue dated 09 August 2024.
ATR SB ATR72-27-1075 original issue dated 09 August 2024.
ATR SB ATR72-27-1077 original issue dated 09 August 2024 or issue 1 dated 20 September 2024.
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 22 November 2024.
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.
|
