Number |
2018-0095R1 |
Issued by |
Europe |
Issue date |
2019-11-29 |
Effective date |
2019-12-06 |
EASA approval number |
|
Contributor |
EASA Environment and Propulsion Systems Department |
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 2018-0095 dated 24 April 2018.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Rolls-Royce NMSB TRENT 1000 72-J353 original issue dated 25 August 2016, or Revision 1 dated
24 November 2016, or Revision 2 dated 14 February 2018.
Rolls-Royce SB TRENT 1000 72-J704 original issue dated 23 June 2017.
Rolls-Royce Alert NMSB TRENT 1000 72-AJ929 original issue dated 23 November 2017.
Rolls-Royce SB TRENT 1000 72-K216 original issue dated 18 June 2019.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
19-201 |
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 07 March January 2018 as PAD 18-034 for consultation until 04 April 2018. 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. This revised AD was posted on 11 November 2019 as PAD 19-201 for consultation until 25 November 2019. No comments were received during the consultation period.
4. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
5. 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.
|