| Number |
2015-0017 |
| Issued by |
 Europe |
| Issue date |
2015-02-04 |
| Effective date |
2015-02-10 |
| EASA approval number |
|
| ATA Chapter |
80 |
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
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2014-0235 dated 27 October 2014.
|
| Publication(s) and related information |
AHD ASB BO105-80A-150 original issue dated 27 October 2014, or Revision 1 dated 02 February 2015.
AHD ASB BO105 LS‐80A‐036 original issue dated 27 October 2014, or Revision 1 dated 02 February 2015.
AHD BO105 C/CS TempRev 1, EASA approved on 29 January 2015.
AHD BO105 CB/CBS TempRev 1, EASA approved on 29 January 2015.
AHD BO105 CB-5/CBS-5 TempRev 1, EASA approved on 29 January 2015.
AHD BO105 DB/DBS TempRev 1, EASA approved on 29 January 2015.
AHD BO105 DBS-5 TempRev 1, EASA approved on 29 January 2015.
AHD BO105 LS A-3 TempRev 1, EASA approved on 29 January 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.
|
