Cessna 310 Safety Record

The pilot's inattentiveness to the fuel flow and fuel selector valve position resulting in fuel starvation. Contributing factors were the pilot's failure to follow proper engine failure procedures, and the pilot's improper in-flight planning and decision making.

Improper maintenance performed on the airplane by maintenance personnel, and the failure of the mechanic with an inspection authorization (IA) to verify the maintenance work performed, which resulted in a reverse elevator trim system, and subsequent loss of control and collision with trees during the initial climb from takeoff.

The pilot's failure to maintain sufficient airspeed to avoid a stall during the instrument landing approach, which resulted in an inadvertent stall and collision with terrain. Also causal was the pilot's impairment due to prohibited drugs. Factors associated with the accident are an inadvertent stall, a low ceiling, dark night, and the pilot's lack of currency in instrument flight rules.

Separation of the left main landing gear torque link during landing resulting in a loss of control and runway excursion. Contributing factors were a failure to comply with the airframe manufacturer's service bulletin, and the pilot's inability to maintain directional control after the torque link separation.

The pilot's failure to maintain sufficient airspeed during takeoff-initial climb to avoid a stall/mush. A factor associated with the accident was the inadvertent stall/mush.

The mechanic's improper maintenance that resulted in the right main landing gear's separation from the airplane and an inadvertent loss of control during landing.

The down limit switch, which operates the landing gear mechanical stop, was bent in the up position and allowed the gear motor to continued to run, causing the gearbox to over-travel, pull on the landing gear rods, and retract the landing gear.

The in-flight collision with a duck during cruise flight resulting in a ruptured fuel tank and the strobe/light assembly electrical short resulting in a fire to the right wing tip tank. Contributing factors were the dusk light conditions.

The pilot's failure to maintain control of the airplane during the landing roll due to the icy runway. Factors were the compacted snow and ice along the edges of the runway and at the taxiway intersection, and the snow banks adjacent to the runway and taxiway.

The pilot misjudged his altitude and airspeed while landing which resulted in the airplane stalling 20 feet above the runway. A factor associated with the accident was the pilot's execution of the approach when reported weather conditions were below the minimums required for the approach.

The pilot's misjudged distance/altitude which resulted in an undershoot. A related factor was the pilot's diverted attention due to the open cabin door.

The loss of engine power as a result of a fatigue fracture in one of the crankshaft gear teeth for undetermined reasons. Also causal was the pilot's failure to maintain control of the twin-engine airplane after the power loss, which resulted in an inadvertent stall and subsequent collision with terrain.

The collapse of the nose landing gear as a result of the pilot performing improper maintenance on the airplane due to his failure to properly safety the nose landing gear door.