| Number |
2023-0119 |
| Issued by |
 Europe |
| Issue date |
2023-06-12 |
| Effective date |
2023-06-26 |
| EASA approval number |
|
| ATA Chapter |
73 |
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
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce Alert NMSB TRENT 1000 73-AK733 original issue dated 23 July 2021, or Revision 1 dated 10 January 2022, or Revision 2 dated 03 March 2022, or Revision 3 dated 30 March 2023.
Rolls-Royce SB TRENT 1000 73-K891 original issue dated 07 December 2022.
Rolls-Royce Control Systems SB G5040HMU-73-02 original issue dated 13 July 2021, or Revision 1 dated 13 December 2021, or Revision 2 dated 28 March 2023.
Rolls-Royce Control Systems SB G5040HMU-73-8497 original issue dated 29 November 2022.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
23-051 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 24 April 2023 as PAD 23-051 for consultation until 22 May 2023. 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.
|
