| Number |
2012-0255 |
| Issued by |
 Europe |
| Issue date |
2012-11-30 |
| Effective date |
2012-12-14 |
| EASA approval number |
|
| ATA Chapter |
78 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211-524
-
D4-19
-
D4-39
-
D4-B-19
-
D4-B-39
-
D4X-19
-
D4X-B-19
-
G2-19
-
G2-T-19
-
G3-19
-
G3-T-19
-
H-36
-
H-T-36
-
H2-19
-
H2-T-19
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2009-0253 dated 30 November 2009.
|
| Publication(s) and related information |
Rolls-Royce NMSB RB.211-78-AG084 Revision 3 dated 24 November 2009, or Revision 4 dated 22 December 2009, or Revision 5 dated 4 February 2011, or Revision 6 dated 16 November 2012, or Revision 7 dated 23 November 2012.
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.
|
