| Number |
2013-0138R1 |
| Issued by |
 Europe |
| Issue date |
2013-07-15 |
| Effective date |
2013-07-15 |
| EASA approval number |
|
| ATA Chapter |
63 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA 330 / AS 332 / EC 225
-
AS 332 C
-
AS 332 C1
-
AS 332 L
-
AS 332 L1
-
AS 332 L2
-
EC 225 LP
|
| Revision |
This AD revises EASA Emergency AD 2013-0138-E dated 09 July 2013, which superseded EASA Emergency AD 2012-0250-E dated 21 November 2012.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Eurocopter EC225 ASB No.04A009 Revision 2 dated 21 November 2012 and ASB No.EC225-04A009 Revision 3 dated 08 July 2013.
Eurocopter ASB No. EC225-45A010 original issue, dated 08 July 2013.
Eurocopter ASB No. EC225-05A036 original issue, dated 08 July 2013.
Eurocopter AS332 ASB No.01.00.82 Revision 2 dated 21 November 2012 and ASB No.AS332-01.00.82 Revision 3 dated 08 July 2013.
Eurocopter ASB No. AS332-05.00.96 original issue, dated 08 July 2013.
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 Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|
