| Number |
2021-0114 |
| Issued by |
 Europe |
| Issue date |
2021-04-23 |
| Effective date |
2021-05-07 |
| EASA approval number |
|
| ATA Chapter |
72 |
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 |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce Alert NMSB RB.211-72-AG774 original issue dated 20 March 2021, or Revision 1 dated 31 July 2013, or Revision 2 dated 23 December 2014, or Revision 3 dated 24 September 2015, or Revision 4 dated 13 October 2020.
Rolls-Royce Alert NMSB RB.211-72-AJ032 original issue dated 24 September 2015.
Rolls-Royce SB RB211-72-G581 original issue dated 20 March 2012.
Rolls-Royce SB RB.211-72-G634 original issue dated 20 March 2012, or Revision 1 dated 03 July 2012.
Rolls-Royce SB RB.211-72-G856 original issue dated 26 July 2013, or Revision 1 dated 27 August 2014.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
21-032 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 25 February 2021 as PAD 21-032 for consultation until 25 March 2021.
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.
|
