| Number |
2008-0165R1 |
| Issued by |
 Europe |
| Issue date |
2017-06-30 |
| Effective date |
2017-06-30 |
| EASA approval number |
|
| ATA Chapter |
62 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
SA 365 C1
-
SA 365 C2
-
SA 365 C3
-
SA 365 N
-
SA 365 N1
|
| Revision |
This AD revises EASA AD 2008-0165 dated 28 August 2008, which superseded EASA Emergency AD 2006-0321-E dated 18 October 2006.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Eurocopter AS365 ASB 05.00.51, SA366 ASB 05.35, and SA365 ASB 05.28 (single document), original issue dated 04 April 2006, or Revision 1 dated 12 October 2006, or Revision 2 dated 22 November 2007, or Revision 3 dated 18 August 2008, or
Airbus Helicopters AS365 ASB 05.00.51, SA366 ASB 05.35, and SA365 ASB 05.28 (single document), Revision 4 dated 20 November 2014.
The use of later approved revisions of this document 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.
|
