| Number |
2018-0291R1 |
| Issued by |
 Europe |
| Issue date |
2025-02-24 |
| Effective date |
2025-03-03 |
| 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 2018-0291 dated 21 December 2018.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce Trent 700 Alert NMSB RB.211-72-AK165 original issue dated 26 November 2018, or Revision 1 dated 11 September 2019, or Revision 2 dated 25 November 2020, or Revision 3 dated 09 March 2022, or Revision 4 dated 31 January 2024.
Rolls-Royce Trent 700 Engine Manual E-Trent-1RR, dated 10 September 2018.
Rolls-Royce Trent 700 SB RB211 72-K414 original issue dated 21 July 2021, or Revision 1 dated 21 June 2024.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
18-161 |
| 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 27 November 2018 as PAD 18-161 for consultation until 11 December 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.
|
