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ADs [at] easa.europa [dot] eu
|
| Number |
26-064 |
| Issued by |
 Europe |
| Issue date |
2026-05-13 |
| EASA approval number |
|
| ATA Chapter |
55 |
Approval Holder
/ Type Designation |
-
LEONARDO S.p.A. HELICOPTERS
-
A109/A119
-
A109A
-
A109AII
-
A109C
-
A109E
-
A109K2
-
A109LUH
-
A109S
-
AW109SP
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Leonardo S.p.A. ASB 109-164 original issue dated 19 December 2024, and Revision A dated
02 February 2026, and Revision B dated 20 April 2026.
Leonardo S.p.A. ASB 109EP-190 original issue dated 19 December 2024, and Revision A dated
02 February 2026, and Revision B dated 20 April 2026.
Leonardo S.p.A. ASB 109K-083 original issue dated 19 December 2024, and Revision A dated
02 February 2026, and Revision B dated 20 April 2026.
Leonardo S.p.A. ASB 109L-128 original issue dated 19 December 2024, and Revision A dated
02 February 2026, and Revision B dated 20 April 2026.
Leonardo S.p.A. ASB 109S-128 original issue dated 19 December 2024, and Revision A dated
02 February 2026, and Revision B dated 20 April 2026.
Leonardo S.p.A. ASB 109SP-168, original issue dated 19 December 2024 Revision A dated
02 February 2026, and Revision B dated 20 April 2026.
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 10 June 2026.
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.
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