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ADs [at] easa.europa [dot] eu
|
Number |
24-042 |
Issued by |
Europe |
Issue date |
2024-04-09 |
EASA approval number |
|
Contributor |
EASA VTOL Department |
ATA Chapter |
25,30,53 |
Approval Holder / Type Designation |
-
AIRBUS HELICOPTERS
-
SA 330 / AS 332 / EC 225
-
AS 332 C
-
AS 332 C1
-
AS 332 L
-
AS 332 L1
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2018-0142R1 dated 09 December 2019.
|
Publication(s) and related information |
AH AS332 Emergency ASB 01.00.91 original issue dated 03 July 2018, or Revision 1 dated
04 December 2019.
AH AS332 Emergency ASB 01.00.96 original issue dated 04 December 2019.
AH ASB AS332-04-00-0001 original issue dated 27 March 2024.
The use of later approved revisions of above-mentioned documents is acceptable for compliance with the requirements of this AD. |
Remarks |
1. This Proposed AD will be closed for consultation on 07 May 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.
|