| Number |
2010-0213 |
| Issued by |
 Europe |
| Issue date |
2010-12-03 |
| Effective date |
2010-10-28 |
| EASA approval number |
|
| ATA Chapter |
63 |
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 |
This AD has been republished to remove a part serial number (1028) from
Appendix 1 of this AD and to correct paragraphs (2) and (3) for consistency.
|
| Supersedure |
None
|
| Publication(s) and related information |
ECD ASB EC135-63A-017 original issue dated 11 October 2010.
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. 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[@]easa.europa[dot]eu
|
