| Number |
2012-0206 |
| Issued by |
 Europe |
| Issue date |
2012-10-02 |
| Effective date |
2012-10-16 |
| EASA approval number |
|
| ATA Chapter |
25 |
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
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
EC 155 B
-
EC 155 B1
-
SA 365 N
-
SA 365 N1
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2012-0084 dated 16 May 2012.
|
| Publication(s) and related information |
Eurocopter ASB AS365-25.01.18, Revision 1 dated 09 August 2012.
Eurocopter ASB EC155-25A114, Revision 1 dated 09 August 2012.
Eurocopter ASB AS332-25.02.49, Revision 1 dated 09 August 2012.
Eurocopter ASB EC225-25A110, Revision 1 dated 09 August 2012.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
12-112 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 21 August 2012 as PAD 12-112 for consultation until 18 September 2012. The Comment Response Document can be found at https://ad.easa.europa.eu.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.
|
