| Number |
2009-0187R2 |
| Issued by |
 Europe |
| Issue date |
2011-05-06 |
| Effective date |
2011-05-20 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 700
-
RB211-524
-
G2-T-19
-
G3-T-19
-
H-T-36
-
H2-T-19
-
RB211-535
-
RB211-535E4-37
-
RB211-535E4-B-37
-
RB211-535E4-C-37
|
| Revision |
This AD revises AD 2009-0187R1 dated 08 September 2009 and corrected on 11
September 2009.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce Service Bulletin No. RB.211-72-AG073, Initial Issue.
Rolls-Royce Service Bulletin No. RB.211-72-AG073, Revision 1.
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 Airworthiness
Directives, Safety Management & Research Section, Certification
Directorate, EASA. E-mail ADs[at]easa.europa[dot]eu
|
