| Number |
2019-0249R1 |
| Issued by |
 Europe |
| Issue date |
2025-01-30 |
| Effective date |
2025-02-06 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
TRENT 1000
-
Trent 1000-A
-
Trent 1000-AE
-
Trent 1000-C
-
Trent 1000-CE
-
Trent 1000-D
-
Trent 1000-E
-
Trent 1000-G
-
Trent 1000-H
|
| Revision |
This AD revises EASA AD 2019-0249 dated 09 October 2019.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2019-0075 dated 29 March 2019.
|
| Publication(s) and related information |
Rolls-Royce Alert NMSB TRENT 1000 72-AK130 original issue dated 11 June 2018, or Revision 1 dated 29 June 2018, or Revision 2 dated 26 July 2018, or Revision 3 dated 10 January 2019, or Revision 4 dated 04 March 2019, or Revision 5 dated 22 August 2019, or Revision 6 dated 17 October 2024.
Rolls-Royce NMSB TRENT 1000 72-K099 original issue dated 11 June 2018, or Revision 1 dated 03 July 2018, or Revision 2 dated 27 September 2018.
Rolls-Royce NMSB TRENT 1000 72-K100 original issue dated 11 June 2018, or Revision 1 dated 02 July 2019.
Rolls-Royce NMSB TRENT 1000 72-K129 original issue dated 11 June 2018, or Revision 1 dated 02 July 2018, or Revision 2 dated 27 September 2018, or Revision 3 dated 28 February 2019.
Rolls-Royce NMSB TRENT 1000 72-K132 original issue dated 29 June 2018, or Revision 1 dated 10 January 2019, or Revision 2 dated 26 March 2019.
Rolls-Royce SB TRENT 1000 72-K434 original issue dated 21 July 2021, or Revision 1 dated 25 November 2021.
The use of later approved revisions of the above-mentioned documents, is acceptable for compliance with the requirements of this AD. |
| PAD number |
19-168 |
| 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 as PAD 19-168 on 09 September 2019 for additional consultation until 23 September 2019. 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.
|
