| Number |
2014-0230 |
| Issued by |
 Europe |
| Issue date |
2014-10-21 |
| Effective date |
2014-11-04 |
| EASA approval number |
|
| ATA Chapter |
63 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS DEUTSCHLAND
-
BO 105
-
BO 105 A
-
BO 105 C
-
BO 105 D
-
BO 105 S
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2011-0091R2 dated 08 November 2012.
|
| Publication(s) and related information |
ECD ASB BO105-10-125 dated 02 September 2010, or Revision 1 dated 04 April 2011, or Revision 2 dated 23 May 2012, or AHD ASB BO105-10-125 Revision 3 dated 27 May 2014.
AHD SB BO105-10-126 dated 19 June 2013, or Revision 1 dated 6 August 2013.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
BO105 Maintenance Manual, Chapter 11, Sections 11-12 through 11-19, including revised Table 11-2 (pages 4 and 5 of ASB BO105-10-125 Revision 3) and picture 11-14 (page 6 of ASB BO105-10-125 Revision 3). |
| PAD number |
14-142 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 19 September 2014 as PAD 14-142 for consultation until 17 October 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.
|
