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ADs [at] easa.europa [dot] eu
|
Number |
24-068 |
Issued by |
Europe |
Issue date |
2024-06-17 |
EASA approval number |
|
Contributor |
EASA VTOL Department |
ATA Chapter |
04 |
Approval Holder / Type Designation |
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
AS 350 B
-
AS 350 B1
-
AS 350 B2
-
AS 350 B3
-
AS 350 BA
-
AS 350 BB
-
AS 350 D
-
EC 130 B4
-
EC 130 T2
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes DGAC France AD F-1984-064-037R3 dated 02 February 1994
and EASA AD 2021-0194R1 dated 08 October 2021.
|
Publication(s) and related information |
AH AS 350 B AMM Chapter 04 ALS Revision 009 dated 09 October 2023.
AH AS 350 B1 AMM Chapter 04 ALS Revision 009 dated 09 October 2023.
AH AS 350 BB AMM Chapter 04 ALS Revision 009 dated 09 October 2023.
AH AS 350 BA AMM Chapter 04 ALS Revision 009 dated 09 October 2023.
AH AS 350 D AMM Chapter 04 ALS Revision 009 dated 09 October 2023.
AH AS 350 B2 AMM Chapter 04 ALS Revision 016 dated 27 November 2023.
AH AS 350 B3 AMM Chapter 04 ALS Revision 016 dated 27 November 2023.
AH EC 130 T2 AMM Chapter 04 ALS Revision 012 dated 27 November 2023.
AH EC 130 B4 AMM Chapter 04 ALS Revision 014 dated 27 November 2023.
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 01 July 2024.
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.
|