| Number |
2018-0084R2 |
| Issued by |
 Europe |
| Issue date |
2019-01-17 |
| Effective date |
2019-01-17 |
| 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 2018-0084R1 dated 19 April 2018.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2018-0073 dated 30 March 2018.
|
| Publication(s) and related information |
Rolls-Royce Alert NMSB TRENT 1000 72-AJ814 original issue dated 17 August 2017, or Revision 1 dated 26 September 2017, or Revision 2 dated 12 April 2018.
Rolls-Royce Alert NMSB TRENT 1000 72-AJ819 original issue dated 17 August 2017, or Revision 1 dated 9 October 2017, or Revision 2 dated 12 April 2018, or Revision 3 dated 13 April 2018.
Rolls-Royce NMSB TRENT 1000 72-J744 original issue dated 20 June 2017, or Revision 1 dated 18 April 2018.
Rolls-Royce NMSB TRENT 1000 72-J871 original issue dated 19 October 2017, or Revision 1 dated 19 December 2017, or Revision 2 dated 10 April 2018, or Revision 3 dated 12 April 2018.
Rolls-Royce Alert NMSB TRENT 1000 72-AJ869 original issue dated 19 October 2017, and Revision 1 (supersedure) dated 12 April 2018.
Rolls-Royce Alert NMSB TRENT 1000 72-AK058 original issue dated 30 March 2018.
Rolls-Royce Alert NMSB TRENT 1000 72-AK060 original issue dated 13 April 2018.
Rolls-Royce SB TRENT 1000 72-J941 original issue date 06 December 2018.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication.
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 PAD, can be reported to the EU aviation safety reporting system.
|
