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2025-0061 : Engine – Low-Pressure Compressor Rotor Shaft – Inspection(s)

Number 2025-0061
Issued by Europe  Europe
Issue date 2025-03-18
Effective date 2025-04-01
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
    • RB211 TRENT 900
      • 970-84
      • 970B-84
      • 972-84
      • 972B-84
      • 972E-84
      • 977-84
      • 977B-84
      • 980-84
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Rolls-Royce NMSB RB211 72-AL186 original issue dated 27 January 2025. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
PAD number 25-018
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 29 January 2025 as PAD 25-018 for consultation until 26 February 2025. 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.