| Number |
2010-0087 |
| Issued by |
 Europe |
| Issue date |
2010-05-06 |
| Effective date |
2010-05-19 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 800
-
875-17
-
877-17
-
884-17
-
884B-17
-
892-17
-
892B-17
-
895-17
|
| Revision |
Not applicable
|
| Correction |
This AD has been corrected as, inadvertently, a wrong effective date was indicated for the Heavy Flight Profile Parts.
|
| Supersedure |
This AD supersedes EASA AD 2008-0099 dated 21 May 2008 and corrected
on 12 June 2008
|
| Publication(s) and related information |
Rolls-Royce Alert Non Modification Service Bulletin RB211-72-AF825
Revision 3.
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. The required actions and the risk assessment have granted the
issuance of a Final AD with Requests for Comments, postponing the
public consultation process after publication.
3. Enquiries regarding this AD should be referred to the Airworthiness
Directives, Safety Management & Research Section, Certification
Directorate, EASA. E-mail ADs@easa.europa.eu.
|
