| Number |
2024-0229R1 |
| Issued by |
 Europe |
| Issue date |
2026-01-20 |
| Effective date |
2026-01-27 |
| EASA approval number |
|
| ATA Chapter |
62 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises EASA AD 2024-0229 dated 02 December 2024.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2023-0222-E dated 21 December 2023, including its Correction dated 22 December 2023.
|
| Publication(s) and related information |
AH Emergency ASB H160-B 62-32-0001 original issue dated 19 December 2023, Issue 002 dated 25 November 2024, and Issue 003 dated 13 October 2025.
The use of later approved revisions of the above-mentioned document 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. Based on the required actions and the compliance time, the original issue of this AD was posted on 02 December 2024 as Final AD with Request for Comments, postponing the public consultation process until 03 January 2025. 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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