| Number |
2026-0004 |
| Issued by |
 Europe |
| Issue date |
2026-01-13 |
| Effective date |
2026-01-27 |
| EASA approval number |
|
| ATA Chapter |
04 |
Approval Holder
/ Type Designation |
-
LEONARDO S.p.A. HELICOPTERS
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2025-0090 dated 23 April 2025.
|
| Publication(s) and related information |
Leonardo AW189 document 89-A-AMPI-00-P (Air Vehicle Maintenance Planning Information),
Chapter 04, ALS Issue 030 dated 28 October 2025.
Leonardo AW189 document 89-E-AMPI-00-P (Air Vehicle Maintenance Planning Information),
Chapter 04, ALS Issue 014 dated 28 October 2025.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
25-185 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 11 December 2025 as PAD 25-185 for consultation until 08 January 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.
|
