| Number |
2012-0169 |
| Issued by |
 Europe |
| Issue date |
2012-08-31 |
| Effective date |
2012-09-14 |
| EASA approval number |
|
| ATA Chapter |
55 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes United Kingdom (UK) Civil Aviation Authority (CAA) AD G-2005-0004 dated 18 January 2005, EASA approval 2005-564.
|
| Publication(s) and related information |
Slingsby Advanced Composites Ltd. SB 179 issue 3 dated 20 January 2005, or Marshall Slingsby Advanced Composites SB 179 issue 4 dated 15 March 2007.
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. 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[dot]eu.
|
