| Number |
2011-0135 |
| Issued by |
 Europe |
| Issue date |
2011-11-18 |
| Effective date |
2011-07-20 |
| EASA approval number |
|
| Contributor |
EASA General Aviation Section |
| ATA Chapter |
57 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
This AD has been republished to correct a typographical error in the document
header, where 2010-0135 was replaced by 2011-0135.
|
| Supersedure |
This AD supersedes EASA Emergency AD 2010-0185-E dated 03 September 2010.
|
| Related information |
Aircraft Industries IB L13/107b, dated 18 July 2011.
Aircraft Industries MB L13/108a, dated 14 July 2011.
Aircraft Industries MB L13/112a, dated 16 May 2011.
Aircraft Design and Certification Ltd. modification ADxC-DC-39-001, approved
by EASA through STC 10035295, which includes associated documentation:
- ADxC-39-EO-013, Issue A, dated 01 April 11 (Template for installation of
structural modification),
- ADxC-39-001-AFM dated 30 March 11 (AFM supplement), and
- ADxC-39-001-AMM dated 11 June 11 (MM supplement).
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. 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, Executive Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.
|
