| Number |
2024-0004R1 |
| Issued by |
 Europe |
| Issue date |
2026-08-10 |
| Effective date |
2026-08-17 |
| EASA approval number |
|
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
-
LEONARDO S.p.A. HELICOPTERS
|
| Revision |
This AD revises EASA AD 2024-0004 dated 05 January 2024.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2022-0153 dated 28 July 2022.
|
| Publication(s) and related information |
Leonardo S.p.A. ASB 109EP-173 original issue dated 10 November 2020, Rev. A dated 21 July 2022, and Rev. B dated 24 August 2023, including Errata Corrige dated 29 August 2023, and Rev. C dated 10 July 2026.
Leonardo S.p.A. ASB 109EP-179 original issue dated 21 July 2022, and Rev. A dated 24 August 2023, and Rev. B dated 10 July 2026.
Leonardo S.p.A. ASB 109S-109 original issue dated 21 July 2022, and Rev. A dated 24 August 2023 and Rev. B dated 10 July 2026, and Rev. C dated 31 July 2026.
Leonardo S.p.A. ASB 109L-120 original issue dated 21 July 2022, and Rev. A dated 24 August 2023, and Rev. B dated 10 July 2026.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
23-110 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. The original issue of this AD was posted on 16 October 2023 as PAD 23-110 for consultation
until 13 November 2023. The Comment Response Document can be found in the EASA Safety
Publications Tool, in the compressed (zipped) file attached to the record for this AD.
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.
|
