| Number |
G-2005-0008 |
| Issued by |
 Europe |
| Issue date |
2005-03-08 |
| Effective date |
2005-03-18 |
| EASA approval number |
2005-2139 |
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211-524
-
B-02
-
B-B-02
-
B2-19
-
B2-39
-
B2-B-19
-
B3-02
-
B4-02
-
B4-D-02
-
C2-19
-
C2-B-19
-
D4-19
-
D4-39
-
D4-B-19
-
D4-B-39
-
D4X-19
-
D4X-B-19
-
G2-19
-
G2-T-19
-
G3-19
-
G3-T-19
-
H-36
-
H-T-36
-
H2-19
-
H2-T-19
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes CAA UK AD 006-04-2002
|
| Publication(s) and related information |
Rolls-Royce Alert NMSB RB.211-72-AD428 Revision 5 dated 18 March 2005; NMSB RB.211-72-E148 original issue dated 13 March 2003; RB.211-72-E150; and NMSB RB.211-72-E171 Revision 1 dated 08 February 2005. Copies of these may be obtained from Rolls-Royce plc, Technical Publications, PO Box 31, Derby, DE24 8BJ, United Kingdom. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
