| Number |
2013-0244 |
| Issued by |
 Europe |
| Issue date |
2013-10-04 |
| Effective date |
2013-10-18 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
GENERAL ATOMICS AeroTec Systems GmbH
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes Luftfahrt-Bundesamt (LBA) Germany AD D-2005-438 (EASA approval 2005-6430) dated 14 December 2005.
|
| Publication(s) and related information |
RUAG Dornier 228 TLMCM-090305-ALL, Revision 5 dated 20 March 2011.
RUAG Dornier 228 TLMCM-228-00002-150610, Revision 1 dated 03 March 2011.
RUAG AMM-228-00014-080184, Revision 3 dated 30 October 2012.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
13-111 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 30 July 2013 as PAD 13-111 for consultation until 27 August 2013. The Comment Response Document can be found at https://ad.easa.europa.eu.
EASA AD No.: 2013-0244
TE.CAP.00110-003 © European Aviation Safety Agency. All rights reserved. 3/3
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.
|
