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US-2003-10-01 : Engine - High Pressure Turbine Rotor Rear Shaft - Replacement (Cyclic Life Limit Reduction)

Number US-2003-10-01
Issued by United States of America  United States of America
Issue date 2003-05-13
Effective date 2003-06-17
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • GENERAL ELECTRIC
    • CF6-6
      • CF6-6D
      • CF6-6D1
      • CF6-6D1A
      • CF6-6K
      • CF6-6K2
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information General Electric Company CF6-6 Engine Shop Manual, GEK 9266. A copy may be obtained from General Electric Company via Lockheed Martin Technology Services, 10525 Chester Road, Suite C, Cincinnati, Ohio 45215, telephone (513) 672-8400, fax (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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