Please feel free to send us your comments by email at
ADs [at] easa.europa [dot] eu
|
| Number |
26-038 |
| Issued by |
 Europe |
| Issue date |
2026-03-24 |
| EASA approval number |
|
| ATA Chapter |
42 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS DEUTSCHLAND
-
MBB-BK 117
-
MBB-BK 117 D-2
-
MBB-BK 117 D-3
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
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.
AH SB MBB-BK117-46-00-0002 original issue (Issue 001) dated 11 November 2024.
AH SB MBB-BK117-46-00-0003 original issue (Issue 001) dated 07 March 2025.
AH SB MBB-BK117-42-00-0001 original issue (Issue 001) dated 11 November 2024, or Issue 002 dated 07 March 2025, or Issue 003 (ASB) dated 08 January 2026.
AH ASB MBB-BK117-42-00-0003 original issue (Issue 001) dated 08 January 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 21 April 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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