N1241X

Safety history

• April 12, 2005Accident

  The fracture of multiple compressor turbine blades while the airplane was in a cruise flight configuration resulting in a loss of engine power. Sulphidation type corrosion was a factor in failure of the blades.

  Cessna 208B

  The fracture of multiple compressor turbine blades while the airplane was in a cruise flight configuration resulting in a loss of engine power. Sulphidation type corrosion was a factor in failure of the blades. Full accident record

• November 9, 1966Accident

  Improper In-Flight Decisions Or Planning; Fuel Exhaustion. Factors: Miscalculated Fuel Consumption; Continued Vfr Flight Into Adverse Weather Conditions; Low Ceiling

  Mooney M20E