| Number |
2025-0002 |
| Issued by |
 Europe |
| Issue date |
2025-01-07 |
| Effective date |
2025-01-21 |
| EASA approval number |
|
| Contributor |
EASA Environment & Propulsion Systems Department |
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
TRENT 1000
-
Trent 1000-A2
-
Trent 1000-AE2
-
Trent 1000-C2
-
Trent 1000-CE2
-
Trent 1000-D2
-
Trent 1000-E2
-
Trent 1000-G2
-
Trent 1000-H2
-
Trent 1000-J2
-
Trent 1000-K2
-
Trent 1000-L2
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce NMSB TRENT 1000-72-K841 original issue dated 23 May 2022, or Revision 1 dated 30 June 2022, Revision 2 dated 08 August 2023, or Alert NMSB TRENT1000-72-AK841 Revision 3 dated 07 October 2024.
Rolls-Royce Cleaning, Inspection and Repair Manual CIR-TRENT-10RRC Revision 88 dated 12 August 2024.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
24-131 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 31 October 2024 as PAD 24-131 for consultation until 28 November
2024. 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.
|
