| Number |
2008-0078R1 |
| Issued by |
 Europe |
| Issue date |
2011-12-15 |
| Effective date |
2011-12-15 |
| EASA approval number |
|
| ATA Chapter |
75 |
Approval Holder
/ Type Designation |
-
SMA AERO ENGINES GmbH
-
TEXTRON AVIATION INC.
|
| Revision |
This AD revises EASA AD 2008-0078 dated 24 April 2008. This AD revises EASA AD 2008-0078, reducing the Applicability by excluding all aeroplanes on which the SB-C182-71-006 Revision 1 modification has been done, and clarifying that this optional modification constitutes terminating action for the repetitive inspections required by this AD.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
SMA SB N° SB-C182-75-002, currently at Revision 4 dated 17 October 2011.
SMA SB N° SB-C182-71-006 Revision 1 dated 1 June 2011.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
|
| PAD number |
08-015R1 |
| Remarks |
1. If requested and appropriately substantiated, EASA can accept Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 01 February 2008 as PAD 08-015 for consultation until 29 February 2008, and subsequently republished on 07 April 2008 as PAD 08-015R1 for additional consultation until 21 April 2008. No comments were received during this period.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs[@]easa.europa[dot]eu.
|
