| Number |
2026-0115 |
| Issued by |
 Europe |
| Issue date |
2026-06-15 |
| Effective date |
2026-06-29 |
| 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. |
| PAD number |
26-064 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 13 May 2026 as PAD 26-064 for consultation until 10 June 2026. 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.
|
