Number |
2010-0188R1 |
Issued by |
Europe |
Issue date |
2015-02-23 |
Effective date |
2015-02-23 |
EASA approval number |
|
Contributor |
EASA Propulsion Section |
ATA Chapter |
73 |
Approval Holder / Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 800
-
875-17
-
877-17
-
884-17
-
884B-17
-
892-17
-
892B-17
-
895-17
|
Revision |
This AD revises EASA AD 2010-0188 dated 20 September 2010, including the Correction dated 22 February 2011.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Rolls-Royce NMSB RB211-73-D685 Revision 3 dated 18 August 2009, or Revision 4 dated 20 January 2010, or Revision 5 dated 18 August 2010, or Revision 6 dated 21 February 2011.
Rolls-Royce SB RB211-73-H814 dated 19 March 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
10-013 |
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 issued as PAD 10-013 on 21 January 2010 for consultation until 18 February 2010. 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.
|