| Number |
2010-0227R1 |
| Issued by |
 Europe |
| Issue date |
2017-04-07 |
| Effective date |
2017-04-07 |
| EASA approval number |
|
| ATA Chapter |
67 |
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 |
This AD revises AD 2010-0227 dated 03 November 2010 (including its Correction dated 08 November 2010), which superseded EASA AD 2008-0064R1 dated 15 April 2008.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2008-0064R1 dated 15 April 2008.
|
| Publication(s) and related information |
ECD ASB EC135-67A-017 Revision 3 dated 26 July 2010, or Airbus Helicopters ASB EC135-67A-017 Revision 4 dated 03 April 2017.
ECD SB EC135-67-018 Revision 1 dated 15 May 2008.
The use of later approved revisions of these documents 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 EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|
