Number |
2015-0167 |
Issued by |
Europe |
Issue date |
2015-08-12 |
Effective date |
2015-08-26 |
EASA approval number |
|
Contributor |
EASA Rotorcraft Section |
ATA Chapter |
52 |
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 |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2012-0111 dated 22 June 2012.
|
Publication(s) and related information |
Eurocopter AS332 ASB No. 01.00.79 Revision 1 dated 06 June 2012 and Airbus Helicopters AS332 ASB No. 01.00.79 Revision 2 dated 23 June 2015.
Eurocopter EC225 ASB No. 04A007 Revision 1, dated 06 June 2012, and Airbus Helicopters EC225 ASB No. 04A007 Revision 2, dated 23 June 2015.
Airbus Helicopters SB AS332-52.00.43 original issue, dated 23 June 2015.
Airbus Helicopters SB EC225-52-008 original issue, dated 23 June 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
15-093 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 10 July 2015 as PAD 15-093 for consultation until 07 August 2015. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|