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US-2002-10-04 : Engine - Low Pressure Turbine Rotor Shaft - Reduced Life Cycle Limit

Number US-2002-10-04
Issued by United States of America  United States of America
Issue date 2002-05-16
Effective date 2002-06-20
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • GENERAL ELECTRIC
    • CF6-80E1
      • CF6-80E1A2
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information GE CF6-80E1 Engine Manual, TR 05-0019, dated March 7, 2001; and TR 05-0030, dated February 28, 2002; or a later revision of the CF6-80E1 Engine Manual. For a copy of this service information, contact General Electric Company, GE Aviation, Room 285, 1 Neumann Way, Cincinnati, OH 45215; telephone: +1 513-552-3272; email: aviation.fleetsupport@ge.com.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu

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