| Number |
2023-0066 |
| Issued by |
 Europe |
| Issue date |
2023-03-24 |
| Effective date |
2023-04-07 |
| EASA approval number |
|
| Contributor |
EASA VTOL Department |
| ATA Chapter |
25 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS DEUTSCHLAND
-
EC135/635
-
EC135 P1
-
EC135 P2
-
EC135 P2+
-
EC135 P3
-
EC135 T1
-
EC135 T2
-
EC135 T2+
-
EC135 T3
-
EC635 P2+
-
EC635 P3
-
EC635 T1
-
EC635 T2+
-
EC635 T3
-
MBB-BK 117
-
MBB-BK 117 C-2
-
MBB-BK 117 D-2
-
MBB-BK 117 D-3
-
MBB-BK 117 D-3m
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
AH ASB EC135-85A-078 original issue dated 31 January 2023.
AH ASB EC135H-85A-009 original issue dated 31 January 2023.
AH ASB MBB-BK117 C-2-85A-051 original issue dated 31 January 2023.
AH ASB MBB-BK117 D-2-85A-024 original issue dated 31 January 2023.
AH ASB MBB-BK117 D-3-85A-012 original issue dated 31 January 2023.
AH "EC135 P1, P2, P3, T1, T2, T3, limited to CDS, CPDS, P2+, T2+, Chapter 04, Airworthiness Limitations Section", Revision 002 dated 06 April 2021.
AH"EC135 P3H, T3H Chapter 04, Airworthiness Limitations Section", Revision 002 dated 06 April 2021.
AH DN.009.0015.0 EC135 Instructions for Continued Airworthiness original issue dated 12 August 2022.
AH MBB-BK117 C-2 and C-2e Chapter 04 ALS NR 002 dated 30 March 2022.
AH MBB-BK117 D-2 Chapter 04 ALS NR 003 dated 25 September 2020.
AH MBB-BK117 D-2m Chapter 04 ALS NR 003 dated 25 September 2020.
AH DN.010.0080.1 MBB-BK117 Instructions for Continued Airworthiness Revision 1 dated 28 November 2022.
AH MBB-BK117 D-3 Chapter 04 ALS NR 001 dated 14 December 2021.
AH MBB-BK117 D-3m Chapter 04 ALS NR 000 (to be published).
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
23-021 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 15 February 2023 as PAD 23-021 for consultation until 15 March 2023. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
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.
|
