| Number |
2018-0049R2 |
| Issued by |
 Europe |
| Issue date |
2021-09-13 |
| Effective date |
2021-09-20 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 700
-
768-60
-
772-60
-
772B-60
-
772C-60
|
| Revision |
This AD revises EASA AD 2018-0049R1 dated 07 March 201
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce NMSB RB.211-72-AG085 Revision 2 dated 07 July 2011, or Revision 3 dated 27 August
2021.
Rolls-Royce NMSB RB.211-72-AG270 original issue dated 02 September 2009, or Revision 1 dated
14 December 2009, or Revision 2 dated 21 December 2010, or Revision 3 dated 25 February 2011,
or Revision 4 dated 21 March 2011, or Revision 5 dated 8 November 2017.
Rolls-Royce SB RB.211-72-AG402 original issue dated 30 September 2010, or Revision 1 dated
11 January 2011, or Revision 2 dated 07 July 2011, or Revision 3 dated 08 July 2014.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD.
|
| PAD number |
18-010 |
| 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 26 January 2018 as PAD 18-010 for consultation
until 23 February 2018. 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.
|
