| Number |
2013-0178 |
| Issued by |
 Europe |
| Issue date |
2013-08-07 |
| Effective date |
2013-08-21 |
| EASA approval number |
|
| ATA Chapter |
04 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS DEUTSCHLAND
-
EC135/635
-
EC135 P1
-
EC135 P2
-
EC135 P2+
-
EC135 T1
-
EC135 T2
-
EC135 T2+
-
EC635 P2+
-
EC635 T1
-
EC635 T2+
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2009-0207 dated 30 September 2009.
|
| Publication(s) and related information |
ECD MSM EC 135 Chapter 04 Revision 15.
ECD MSM EC 135 Chapter 04 Temporary Revision 16a.
The use of later approved revisions of this document 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. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|
