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FAA AD on General Electric Company (GE) CF6-80C2 turbofan engines

Washington, Usa - To prevent cracks in the forward engine mount platform and forward engine mount yoke that could result in possible separation of the engine from the airplane

Airworthiness Directive Federal Register Information [Federal Register: March 5, 2007 (Volume 72, Number 42)] [Page 9662-9666] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-23871; Directorate Identifier 2006-NE-01-AD; Amendment 39-14975; AD 2007-05-14] RIN 2120-AA64 Airworthiness Directives; General...

fra/pec - 1070756
Rome, Italy, 03/07/2007 12:21
AVIONEWS - World Aeronautical Press Agency

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