| Number |
2012-0215R1 |
| Issued by |
 Europe |
| Issue date |
2013-01-04 |
| Effective date |
2013-01-04 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211-524
-
B-02
-
B2-19
-
B3-02
-
B4-02
-
C2-19
-
D4-19
-
D4-39
-
D4-B-19
-
G2-19
-
G3-19
-
H-36
-
H2-19
-
RB211-535
-
RB211-535C-37
-
RB211-535E4-37
-
RB211-535E4-B-37
|
| Revision |
This AD revises EASA AD 2012-0215 dated 18 October 2012 (including the Correction dated 24 October 2012).
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce NMSB RB.211-72-AG046 original issue dated 17 December 2009, or Revision 1 dated 17 January 2011, or Revision 2 dated 17 June 2012, or Revision 3 dated 6 December 2012.
Rolls-Royce NMSB RB.211-72-AG183 original issue dated 17 December 2009, or Revision 1 dated 16 November 2010, or Revision 2 dated 8 June 2012, or Revision 3 dated 6 December 2012.
Rolls-Royce NMSB RB.211-72-AF572 Revision 2 dated 2 April 2009.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
12-107 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 10 August 2012 as PAD 12-107 for consultation until 07 September 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.
|
