| Number |
2013-0042 |
| Issued by |
 Europe |
| Issue date |
2013-02-26 |
| Effective date |
2013-03-12 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 500
-
RB211 Trent 553-61
-
RB211 Trent 553A2-61
-
RB211 Trent 556-61
-
RB211 Trent 556A2-61
-
RB211 Trent 560A2-61
-
RB211 TRENT 700
-
768-60
-
772-60
-
772B-60
-
772C-60
-
RB211 TRENT 800
-
875-17
-
877-17
-
884-17
-
884B-17
-
892-17
-
892B-17
-
895-17
-
RB211-524
-
G2-T-19
-
G3-T-19
-
H-T-36
-
H2-T-19
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2009-0073R1 dated 08 April 2009.
|
| Publication(s) and related information |
Rolls-Royce NMSB RB.211-72-AF964 Revision 3 dated 11 January 2013.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
| PAD number |
13-017 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 21 January 2013 as PAD 13-017 for consultation until 18 February 2013. The Comment Response Document can be found at https://ad.easa.europa.eu.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa.eu.
|
