Number |
2011-0148R1 |
Issued by |
Europe |
Issue date |
2012-07-30 |
Effective date |
2012-07-30 |
EASA approval number |
|
Contributor |
EASA Rotorcraft Section |
ATA Chapter |
85 |
Approval Holder / Type Designation |
-
AIRBUS HELICOPTERS DEUTSCHLAND
-
MBB-BK 117
-
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
|
Revision |
This AD revises EASA AD 2011-0148 dated 05 August 2011, which superseded EASA AD 2011-0131 dated 08 July 2011.
This AD has been revised to correct the Applicability, as the Model MBB-BK117 A-4 had inadvertently been omitted when AD 2011-0148 superseded
AD 2011-0131 whose Applicability was correct. In addition, the Model MBB-BK117 A-1 has been deleted from the Applicability, as none are in operation
any longer.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
ECD ASB MBB-BK117-80-166 Revision 1 dated 04 August 2011.
The use of later approved revisions of this document 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 Safety Information
Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa.eu
|