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US-2002-02-09 : Engine - Low Pressure Turbine Rotor Stage 2 Disks - Replacement [Life Limit]

Number US-2002-02-09
Issued by United States of America  United States of America
Issue date 2002-02-08
Effective date 2002-03-15
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • GENERAL ELECTRIC
    • CF6-45
      • CF6-45A
      • CF6-45A2
    • CF6-50
      • CF6-50A
      • CF6-50C
      • CF6-50C1
      • CF6-50C2
      • CF6-50C2B
      • CF6-50C2D
      • CF6-50CA
      • CF6-50E
      • CF6-50E1
      • CF6-50E2
      • CF6-50E2B
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Chapter 05-10-00 of CF6-45 and CF6-50 Engine Shop Manual, GEK 50481. Copies may be obtained from General Electric Company via Lockheed Martin Technology Services,10525 Chester Road, Suite C, Cincinnati, Ohio 45215, telephone +1 (513) 672-8400, fax +1 (513) 672-8422.
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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