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FAA AD on General Electric Co. CF6-80A series turbofan engines
Washington, USA - To detect cracks in the bottoms of the dovetail slots that could propagate to failure of the disk and cause an uncontained engine failure
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-44-AD; Amendment 39-13016; AD 2003-01-05] RIN 2120-AA64 Airworthiness Directives; General Electric Co. CF6-80A Series Turbofan Engines PDF Copy (If Available): Preamble Information Regulatory Information 2003-01-05 General Electric...
AVIONEWS - World Aeronautical Press Agency - 38562
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency