| Number |
2011-0038-E |
| Issued by |
 Europe |
| Issue date |
2011-03-04 |
| Effective date |
2011-03-08 |
| EASA approval number |
|
| ATA Chapter |
65 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
AS 350 B
-
AS 350 B1
-
AS 350 B2
-
AS 350 BA
-
AS 350 BB
-
AS 350 D
-
AS 355
-
AS 355 E
-
AS 355 F
-
AS 355 F1
-
AS 355 F2
-
AS 355 N
|
| Revision |
Not applicable
|
| Correction |
This AD correction is issued to publish the correct version of the two different
versions of this AD that were inadvertently published and distributed on 04
March 2011, one of which was incorrect, and thereby avoiding the use of the
incorrect one.
|
| Supersedure |
This AD supersedes EASA Emergency AD 2010-0082-E dated 27 April 2010,
including the Correction dated 28 April 2010.
|
| Publication(s) and related information |
Eurocopter AS350 ASB No. 05.00.62, Revision 2, and
Eurocopter AS355 ASB No. 05.00.57, Revision 2, both dated 1 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. The safety assessment has requested not to implement the full
consultation process and an immediate publication and notification.
3. Enquiries regarding this AD should be referred to the Airworthiness
Directives, Safety Management & Research Section, Certification
Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.
|
