Number |
2017-0243 |
Issued by |
Europe |
Issue date |
2017-12-06 |
Effective date |
2017-12-20 |
EASA approval number |
|
Contributor |
EASA Rotorcraft Section |
ATA Chapter |
04 |
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 2013-0178 dated 07 August 2013.
|
Publication(s) and related information |
AH MSM Revision 23, Chapter 04, dated 26 June 2017.
AH ASB EC135-04A-012 original issue dated 11 September 2017.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
17-155 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 03 November 2017 as PAD 17-155 for consultation until 01 December 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.
|