| Number |
2014-0179R2 |
| Issued by |
 Europe |
| Issue date |
2016-04-11 |
| Effective date |
2016-04-11 |
| EASA approval number |
|
| ATA Chapter |
63 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
EC 155 B
-
EC 155 B1
-
SA 365 C1
-
SA 365 C2
-
SA 365 C3
-
SA 365 N
-
SA 365 N1
|
| Revision |
This AD revises EASA AD 2014-0179R1 dated 29 July 2014.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2014-0165 dated 14 July 2014.
|
| Publication(s) and related information |
Airbus Helicopters ASB AS365-63.00.18 original issue dated 09 July 2014, or Revision 1 dated 07 March 2016.
Airbus Helicopters ASB SA365-65.50 original issue dated 09 July 2014.
Airbus Helicopters ASB SA366-63.09 original issue dated 09 July 2014.
Airbus Helicopters ASB EC155-63A012 Revision 1 dated 21 July 2014, or Revision 2 dated 07 March 2016.
The use of later approved revisions of these 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.
|
