Number |
2015-0166 |
Issued by |
Europe |
Issue date |
2015-08-11 |
Effective date |
2015-08-25 |
EASA approval number |
|
Contributor |
EASA Rotorcraft Section |
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 |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2014-0180R1, dated 16 October 2014.
|
Publication(s) and related information |
AHD ASB MBB-BK117-40A-115 original issue dated 31 March 2014, or Revision 1 dated 04 August 2014, and Revision 2 dated 30 July 2015.
AHD ASB MBB-BK117C-2-62A-007 original issue dated 31 March 2014, revision 01 dated 04 August 2014, and Revision 2 dated 30 July 2015.
AHD ASB BO105-40A-107 original issue dated 31 March 2014, or Revision 1 dated 08 September 2014, and Revision 2 dated 30 July 2015.
AHD ASB BO105LS-40A-12 original issue dated 31 March 2014, or Revision 1 dated 08 September 2014, and Revision 2 dated 30 July 2015.
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. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|