| Number |
2012-0060 |
| Issued by |
 Europe |
| Issue date |
2012-04-18 |
| Effective date |
2012-05-02 |
| EASA approval number |
|
| ATA Chapter |
73 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211-524
-
G2-19
-
G2-T-19
-
G3-19
-
G3-T-19
-
H-36
-
H-T-36
-
H2-19
-
H2-T-19
-
RB211-535
-
RB211-535E4-37
-
RB211-535E4-B-37
-
RB211-535E4-C-37
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce Propulsion Systems NMSB RB211-72-AG493 Revision 1, dated 11 November 2011.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
| PAD number |
12-007 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 01 February 2012 as PAD 12-007 for consultation until 29 February 2012. 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[dot]eu.
|
