| Number |
2026-0143R1 |
| Issued by |
 Europe |
| Issue date |
2026-11-06 |
| Effective date |
2026-11-13 |
| 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 |
This AD revises EASA AD 2026-0143 dated 20 July 2026.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2024-0178 dated 12 September 2024.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 original issue dated 08 June 2025, or Rev. 1 dated 03 October
2025, or Rev. 2 dated 26 February 2026.
Rolls-Royce SB TRENT 1000 72-L199 original issue dated 10 April 2025.
Rolls-Royce SB TRENT 1000 72-L200 original issue dated 08 June 2025, or Rev. 1 dated 17 October
2025, or Rev. 2 dated 26 February 2026.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
26-071 |
| 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 03 June 2026 as PAD 26-071 for consultation until
01 July 2026. 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.
|
