| Number |
2009-0272 |
| Issued by |
 Europe |
| Issue date |
2009-12-18 |
| Effective date |
2010-01-01 |
| EASA approval number |
|
| ATA Chapter |
62 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS DEUTSCHLAND
-
EC135/635
-
EC135 P1
-
EC135 P2
-
EC135 T1
-
EC135 T2
-
EC635 T1
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes LBA Germany AD D-2005-233 dated 24 June 2005, EASA
approval 2005-6109.
|
| Publication(s) and related information |
ECD ASB EC135-62A-021, Initial Issue dated 23 June 2005.
Rotorcraft Flight Manual (FLM) revisions as listed in Appendix I of this AD.
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 required actions and the risk allowance have granted the issuance of
a Final AD with Request for Comments, postponing the public
consultation process after publication.
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.
|
