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ADs [at] easa.europa [dot] eu
|
| Number |
26-071 |
| Issued by |
 Europe |
| Issue date |
2026-06-03 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
TRENT 1000
-
Trent 1000-AE3
-
Trent 1000-CE3
-
Trent 1000-D3
-
Trent 1000-G3
-
Trent 1000-H3
-
Trent 1000-J3
-
Trent 1000-K3
-
Trent 1000-L3
-
Trent 1000-M3
-
Trent 1000-N3
-
Trent 1000-P3
-
Trent 1000-Q3
-
Trent 1000-R3
-
TRENT 7000
-
Trent 7000-68
-
Trent 7000-70
-
Trent 7000-72D
-
Trent7000-72
-
Trent7000-72C
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2024-0178 dated 12 September 2024.
|
| Publication(s) and related information |
Rolls-Royce Alert NMSB Trent 1000 72-AL139 original issue dated 05 July 2024, or Rev. 1 dated
16 December 2025.
Rolls-Royce NMSB Trent 1000 72-K618 Rev. 2 dated 13 June 2024.
Rolls-Royce SB Trent 1000 72-K570 original issue dated 15 June 2021, or Rev. 1 dated
31 March 2023.
Rolls-Royce SB Trent 1000 72-K571 original issue dated 15 June 2021, or Rev. 1 dated
22 February 2022.
Rolls-Royce SB TRENT 1000 72-L197 original issue date 10 April 2025.
Rolls-Royce SB TRENT 1000 72-L198 Rev. 1 dated 03 October 2025.
Rolls-Royce SB TRENT 1000 72-L199 original issue dated 10 April 2025.
Rolls-Royce SB TRENT 1000 72-L200 Rev. 1 dated 17 October 2025.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| Remarks |
1. This Proposed AD will be closed for consultation on 01 July 2026.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred
on a product, part or appliance not affected by this PAD, 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 PAD 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.
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