| Number |
2015-0010R1 |
| Issued by |
 Europe |
| Issue date |
2015-02-04 |
| Effective date |
2015-02-04 |
| EASA approval number |
|
| ATA Chapter |
80 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises EASA AD 2015-0010 dated 16 January 2015, which superseded EASA AD 2014-0212 dated 19 September 2014.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2014-0212 dated 19 September 2014.
|
| Publication(s) and related information |
GROB Aircraft AG MSB1078-196 original issue dated 14 July 2014 or MSB1078-196/1 dated 01 December 2014. (for G 115E and G 115EG).
GROB Aircraft AG MSB1121-144 original issue dated 14 July 2014 or MSB1121-144/1 dated 12 January 2015. (for G 120A and G 120A-I).
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. 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.eu.
|
