| Number |
2022-0168R3 |
| Issued by |
 Europe |
| Issue date |
2026-05-13 |
| Effective date |
2026-05-27 |
| EASA approval number |
|
| ATA Chapter |
42 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS DEUTSCHLAND
-
EC135/635
-
EC135 P3
-
EC135 T3
-
EC635 P3
-
EC635 T3
-
MBB-BK 117
-
MBB-BK 117 D-2
-
MBB-BK 117 D-3
-
MBB-BK 117 D-3m
|
| Revision |
This AD revises EASA AD 2022-0168R2 dated 28 October 2025. The original issue of this AD superseded EASA AD 2022-0143 dated 08 July 2022.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2022-0143 dated 08 July 2022.
|
| Publication(s) and related information |
AH ASB EC135H-05A-001 original issue dated 07 July 2022.
AH ASB MBB-BK117 D-2-05A-003 original issue dated 07 July 2022.
AH ASB MBB-BK117 D-3-05A-001 original issue dated 07 July 2022.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1.
If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2.
Based on the required actions and the compliance time, the original issue of this AD was posted on 12 August 2022 as a Final AD with Request for Comments, postponing the public consultation process until after its publication. 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.
|
