| Number |
2014-0180R1 |
| Issued by |
 Europe |
| Issue date |
2014-10-16 |
| Effective date |
2014-10-30 |
| EASA approval number |
|
| ATA Chapter |
62 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS DEUTSCHLAND
-
BO 105
-
BO 105 A
-
BO 105 C
-
BO 105 D
-
BO 105 LS A-3
-
BO 105 S
-
MBB-BK 117
-
MBB-BK 117 A-1
-
MBB-BK 117 A-3
-
MBB-BK 117 A-4
-
MBB-BK 117 B-1
-
MBB-BK 117 B-2
-
MBB-BK 117 C-1
-
MBB-BK 117 C-2
|
| Revision |
This AD revises EASA AD 2014-0180 issued 28 July 2014, including the correction issued 30 July 2014.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
AHD ASB MBB-BK117-40A-115 Revision 0 dated 31 March 2014.
AHD ASB MBB-BK117C-2-62A-007 Revision 0 dated 31 March 2014.
AHD ASB BO105-40A-107 Revision 0 dated 31 March 2014.
AHD ASB BO105LS-40A-12 Revision 0 dated 31 March 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
14-086 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 23 May 2014 as PAD 14-086 for consultation until 20 June 2014. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.
|
