| Number |
2012-0170R2 |
| Issued by |
 Europe |
| Issue date |
2014-06-20 |
| Effective date |
2014-06-20 |
| EASA approval number |
|
| ATA Chapter |
05, 65 |
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 N1
|
| Revision |
This AD revises EASA AD 2012-0170R1, dated 18 October 2013.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Eurocopter AS365 ASB No. 05.00.54 Revision 4 dated 16 May
2011.Eurocopter AS365 ASB No. 05.00.61 Revision 2 dated 05 July 2012, or
Revision 3 dated 25 June 2013, or Airbus Helicopters AS365 ASB No.
05.00.61 Revision 4 dated 08 April 2014.
Eurocopter AS365 SB No. 65.00.17 Revision 1 dated 21 March 2011.
Eurocopter SA366 ASB No. 05.37 Revision 4 dated 16 May 2011.
Eurocopter SA366 ASB No. 05.41 Revision 2 dated 05 July 2012.
Eurocopter SA366 SB No. 65.04 Revision 1 dated 21 March 2011.
Eurocopter EC155 ASB No. 05A015 Revision 5 dated 25 July 2011.
Eurocopter EC155 ASB No. 05A022 Revision 2 dated 04 July 2012, or
Revision 3 dated 25 June 2013, or Airbus Helicopters EC155 ASB No. 05A022
dated 08 April 2014.
Eurocopter EC155 SB No. 65-006 Revision 1 dated 21 March 2011.
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 of 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 Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|
