Number |
2014-0152R2 |
Issued by |
Europe |
Issue date |
2023-11-23 |
Effective date |
2023-11-30 |
EASA approval number |
|
Contributor |
EASA Environment & Propulsion Systems Department |
ATA Chapter |
72 |
Approval Holder / Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 500
-
RB211 Trent 553-61
-
RB211 Trent 553A2-61
-
RB211 Trent 556-61
-
RB211 Trent 556A2-61
-
RB211 Trent 560A2-61
-
RB211 TRENT 800
-
875-17
-
877-17
-
884-17
-
884B-17
-
892-17
-
892B-17
-
895-17
-
RB211 TRENT 900
-
970-84
-
970B-84
-
972-84
-
972B-84
-
977-84
-
977B-84
-
980-84
|
Revision |
This AD revises EASA AD 2014-0152R1 dated 02 March 2018.
|
Correction |
Not applicable
|
Supersedure |
The original issue of this AD superseded EASA AD 2013-0002 dated 04 January 2013.
|
Publication(s) and related information |
Rolls-Royce NMSB RB.211-72-AG085 Revision 2 dated 07 July 2011.
Rolls-Royce NMSB RB.211-72-AG264 Revision 5 dated 21 March 2011.
Rolls-Royce NMSB RB.211-72-G448 Revision 3 dated 07 July 2011, or Revision 4 dated 21 August 2014, or Revision 4 dated 21 August 2014, or Revision 5 dated 03 October 2023.
Rolls-Royce SB RB.211-72-AG401 Revision 2 dated 05 July 2011, or Revision 3 dated 28 January 2014.
Rolls-Royce NMSB RB.211-72-AH058 original issued dated 13 December 2012, or Revision 1 dated 07 July 2014.
Rolls-Royce NMSB RB.211-72-AH059 original issue dated 11 December 2012, or Revision 1 dated 07 July 2014.
Rolls-Royce SB RB.211-72-AH555 original issue dated 18 October 2013, or Revision 1 dated 13 December 2013.
Rolls-Royce SB RB.211-72-AH561 original issue dated 21 October 2013, or Revision 1 dated 27 June 2014.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
14-019 |
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 23 January 2014 as PAD 14-019 for consultation until 20 February 2014. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.
|