Number |
2014-0162R2 |
Issued by |
Europe |
Issue date |
2019-02-05 |
Effective date |
2019-02-05 |
EASA approval number |
|
Contributor |
EASA Rotorcraft Section |
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
AIRBUS HELICOPTERS
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
SA 365 N
-
SA 365 N1
|
Revision |
This AD revises EASA AD 2014-0162R1 dated 11 July 2014.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
AH ASB AS365 05.00.68 original issue dated 07 April 2014, or Revision 1 dated 19 May 2015, or
Revision 2 dated 20 December 2018.
AH SB AS365-53.00.57 original issue dated 20 December 2018.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD
with Request for Comments, postponing the public consultation process until after publication.
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.
|