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2020-0195R1 : Engine – Low Pressure Turbine Discs – Inspection

Number 2020-0195R1
Issued by Europe  Europe
Issue date 2024-05-15
Effective date 2024-05-22
EASA approval number
Contributor EASA Environment & 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 2020-0195 dated 08 September 2020.
Correction Not applicable
Supersedure None
Publication(s) and related information Rolls-Royce Trent 1000 Alert NMSB 72-AK416 original issue dated 29 June 2020, or Revision 1 dated 03 May 2024. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
PAD number 20-105R1
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 July 2020 as PAD 20-105 for consultation until 03 August 2020 and re-published on 12 August 2020 as PAD 20-105R1 for consultation until 26 August 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.