Safety Publications Tool

2020-0010R3 : Engine – De-Pairing Limitation

Number 2020-0010R3
Issued by Europe  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 2020-0010R2 dated 04 March 2020.
Correction Not applicable
Supersedure None
Publication(s) and related information Rolls-Royce Trent 1000 Alert NMSB 72-AK468 original issue dated 09 December 2019, or Revision 1 dated 03 March 2020, or Revision 2 dated 07 April 2020, or Revision 3 dated 17 October 2024. Rolls-Royce Trent 1000 NMSB 72-K494 original issue dated 03 March 2020. 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 19-216
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 18 December 2019 as PAD 19-216 for consultation until 01 January 2020. 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.