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US-2004-22-07 : [Correction] High Pressure Turbine Stage 2 Nozzle Guide Vanes - Inspection

Number US-2004-22-07
Issued by United States of America  United States of America
Issue date 2005-03-04
Effective date 2004-12-01
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • GENERAL ELECTRIC
    • CF6-80C
      • CF6-80C2A1
      • CF6-80C2A2
      • CF6-80C2A3
      • CF6-80C2A5
      • CF6-80C2A5F
      • CF6-80C2A8
      • CF6-80C2B1
      • CF6-80C2B1F
      • CF6-80C2B2
      • CF6-80C2B2F
      • CF6-80C2B4
      • CF6-80C2B4F
      • CF6-80C2B5F
      • CF6-80C2B6
      • CF6-80C2B6F
      • CF6-80C2B6FA
      • CF6-80C2B7F
      • CF6-80C2B8F
      • CF6-80C2D1F
Revision Not applicable
Correction This AD was republished to correct the phrase ''5.0 or more cycles per flight leg'' in the Compliance section. In all other respects, the original AD remains the same.
Supersedure None
Publication(s) and related information General Electric Company CF6-80C2 SB No. 72-0952, Revision 6, dated May 5, 2003. For a copy of this service information, contact 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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