| Number |
2024-0118R1 |
| Issued by |
 Europe |
| Issue date |
2024-07-29 |
| Effective date |
2024-08-05 |
| 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
|
| Revision |
This AD revises EASA AD 2024-0118 dated 25 June 2024.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2019-0099R2 dated 06 September 2019.
|
| Publication(s) and related information |
Rolls-Royce Alert NMSB TRENT 1000 72-AK316 original issue dated 09 April 2019, or Revision 1 dated 18 April 2019, or Revision 2 dated 30 April 2019, or Revision 3 dated 16 July 2019, or Revision 4 dated 10 May 2024.
Rolls-Royce SB TRENT 1000 72-J550 original issue dated 21 November 2017.
Rolls-Royce SB TRENT 1000 72-L042 original issue dated 24 January 2024.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
24-065 |
| 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 06 June 2024 as PAD 24-065 for consultation until 20 June 2024. 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.
|
