| Number |
2011-0127 |
| Issued by |
 Europe |
| Issue date |
2011-07-01 |
| Effective date |
2011-07-15 |
| 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 |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes DGAC France AD F-2008-004 dated 04 June 2008.
|
| Publication(s) and related information |
EUROCOPTER EC155 ASB No. 63A011 dated 7 May 2008.
EUROCOPTER AS365 ASB No. 63.00.17 dated 7 May 2008.
EUROCOPTER SA360/365 ASB No. 65.47 dated 5 May 2008.
EUROCOPTER SA366 ASB No. 65.03 dated 7 May 2008.
EUROCOPTER Repair Sheet No. 365-63-36-08 dated 4 April 2008.
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
11-045 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. This AD was posted on 05 May 2011 as PAD 11-045 for consultation
until 02 June 2011. No comments were received during the consultation.
3. Enquiries regarding this AD should be referred to the Safety Information
Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa[dot]eu.
|
