| Number |
2017-0002 |
| Issued by |
 Europe |
| Issue date |
2017-01-09 |
| Effective date |
2017-01-23 |
| EASA approval number |
|
| ATA Chapter |
63 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS DEUTSCHLAND
-
EC135/635
-
EC135 P1
-
EC135 P2
-
EC135 P2+
-
EC135 P3
-
EC135 T1
-
EC135 T2
-
EC135 T2+
-
EC135 T3
-
EC635 P2+
-
EC635 P3
-
EC635 T1
-
EC635 T2+
-
EC635 T3
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2010-0213 dated 14 October 2010, including its Correction dated 03 December 2010.
|
| Publication(s) and related information |
ECD ASB EC135-63A-017 original issue dated 11 October 2010, or AH ASB EC135-63A-017 Revision 01 dated 29 September 2016, or Revision 02 dated 05 December 2016.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
| PAD number |
16-166 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 07 December 2016 as PAD 16-166 for consultation until 04 January 2017. The Comment Response Document can be found at https://ad.easa.europa.eu.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|
