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FAA AD on General Electric Company CF6-80C2 and CF6-80E1 series turbofan engines (2009-07-03)

Washington, Usa - To prevent cracks from propagating to an uncontained failure of the disk and damage to the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 13092-13094] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-1025; Directorate Identifier 2008-NE-31-AD; Amendment 39-15862; AD 2009-07-03] RIN 2120-AA64 Airworthiness Directives; General Electric Company CF6-80C2 and CF6-80E1...

fra/pec - 1102863

AVIONEWS - World Aeronautical Press Agency
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