Number |
2024-0120 |
Issued by |
Europe |
Issue date |
2024-06-27 |
Effective date |
2024-07-11 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
55 |
Approval Holder / Type Designation |
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
ATR SB ATR42-55-0021 original issue dated 25 January 2023, or Revision 01 dated 17 February 2023, or Revision 02 dated 31 March 2023, or Revision 03 dated 25 April 2024.
ATR SB ATR72-55-1014 original issue dated 25 January 2023, or Revision 01 dated 17 February 2023, or Revision 02 dated 31 March 2023, or Revision 03 dated 25 April 2024.
ATR AOM 2023/02 issue 1 dated 31 January 2023, or issue 2 dated 13 May 2024.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
24-052 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 17 May 2024 as PAD 24-052 for consultation until 14 June 2024.
No comments were received during the consultation period.
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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