Number |
2017-0147 |
Issued by |
Europe |
Issue date |
2017-08-10 |
Effective date |
2017-08-24 |
EASA approval number |
|
Contributor |
EASA Light Rotorcraft Section |
ATA Chapter |
67 |
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 |
None
|
Publication(s) and related information |
AH ASB EC135-67A-031 original issue dated 30 March 2017.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
PAD number |
17-052 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 26 April 2017 as PAD 17-052 for consultation until 24 May 2017. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|