Number |
2015-0187 |
Issued by |
Europe |
Issue date |
2015-09-09 |
Effective date |
2015-09-23 |
EASA approval number |
|
Contributor |
EASA Propulsion Section |
ATA Chapter |
72 |
Approval Holder / Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211-22B
-
RB211-524
-
B-02
-
B-B-02
-
B2-19
-
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 |
None
|
Publication(s) and related information |
Rolls-Royce NMSB RB.211-72-AG729 original issue dated 1 August 2011.
Rolls-Royce NMSB RB.211-72-AG800 original issue dated 5 March 2012.
Rolls-Royce SB RB.211-72-B540 original issue dated 28 July 1995.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
15-103 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 06 August 2015 as PAD 15-103 for consultation until 03 September 2015. 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.
|