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ADs [at] easa.europa [dot] eu
|
| Number |
23-051 |
| Issued by |
 Europe |
| Issue date |
2023-04-24 |
| EASA approval number |
|
| Contributor |
EASA Environment & Propulsion Systems Department |
| 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. |
| Remarks |
1. This Proposed AD will be closed for consultation on 22 May 2023.
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.
|
