| Number |
2026-0117R1 |
| Issued by |
 Europe |
| Issue date |
2026-08-12 |
| Effective date |
2026-08-19 |
| EASA approval number |
|
| 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 |
This AD revises EASA AD 2026-0117 dated 19 June 2026.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2020-0195R1 dated 15 May 2024
|
| Publication(s) and related information |
Rolls-Royce Alert NMSB TRENT 1000 72-AK416 original issue dated 29 June 2020, or Revision 1
dated 03 May 2024, or Revision 2 dated 24 March 2026.
Rolls-Royce SB Trent 1000 72-K771 original issue dated 24 May 2022.
Rolls-Royce SB Trent 1000 72-K937 original issue dated 16 August 2024, or Revision 1 dated 05
October 2024.
Rolls-Royce SB Trent 1000 72-L305 original issue dated 04 December 2025.
Rolls-Royce SB Trent 1000 72-L306 original issue dated 04 December 2025.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
26-065 |
| 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 13 May 2026 as PAD 26-065 for consultation until 10
June 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.
|
