Please feel free to send us your comments by email at
ADs [at] easa.europa [dot] eu
|
| Number |
25-082 |
| Issued by |
 Europe |
| Issue date |
2025-06-05 |
| EASA approval number |
|
| ATA Chapter |
62 |
Approval Holder
/ Type Designation |
-
LEONARDO S.p.A. HELICOPTERS
-
A109/A119
-
A109A
-
A109AII
-
A109C
-
A109E
-
A109K2
-
A109LUH
-
A109S
-
A119
-
AW109SP
-
AW119MKII
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Leonardo S.p.A. ASB 109K-080 original issue dated 25 November 2024, or Rev. A dated 12 May 2025.
Leonardo S.p.A. ASB 109S-123 original issue dated 25 November 2024, or Rev. A dated 12 May 2025.
Leonardo S.p.A. ASB 109L-125 original issue dated 25 November 2024, or Rev. A dated 12 May 2025.
Leonardo S.p.A. ASB 109-162 original issue dated 25 November 2024, or Rev. A dated 12 May 2025.
Leonardo S.p.A. ASB 109SP-166 original issue dated 25 November 2024, or Rev. A dated 12 May 2025.
Leonardo S.p.A. ASB 109EP-186 original issue dated 25 November 2024, or Rev. A dated 12 May 2025.
Leonardo S.p.A. ASB 119-153 original issue dated 25 November 2024, or Rev. A dated 12 May 2025.
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 03 July 2025.
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.
|
