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ADs [at] easa.europa [dot] eu
|
Number |
24-069 |
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 355
-
AS 355 E
-
AS 355 F
-
AS 355 F1
-
AS 355 F2
-
AS 355 N
-
AS 355 NP
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes DGAC France AD F-1984-045-022R4 dated 02 February 1994 and EASA AD 2021-0193 dated 20 August 2021.
|
Publication(s) and related information |
AH AS 355 E AMM Chapter 04 ALS Revision 012 dated 10 July 2023.
AH AS 355 F AMM Chapter 04 ALS Revision 012 dated 10 July 2023.
AH AS 355 F1 AMM Chapter 04 ALS Revision 012 dated 10 July 2023.
AH AS 355 N AMM Chapter 04 ALS Revision 012 dated 10 July 2023.
AH AS 355 F2 AMM Chapter 04 ALS Revision 013 dated 10 July 2023.
AH AS 355 NP AMM Chapter 04 ALS Revision 011 dated 10 July 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.
|