Cessna Safety Record

The failure of the pilot under instruction to maintain directional control during the landing roll and the inadequate supervision of the flight instructor, which resulted in a collision with a runway light, overload failure of the wheel axle, and the airplane nosing over inverted.

The pilot's inability to maintain the correct approach airspeed (Vref) on final due to incorrect airspeed indications resulting from a partial blockage of the pitot line. Factors include a quartering tailwind, a wet runway, and the pilot's decision not to lower the flaps during the landing.

The failure of the turbocharger scavenging pump resulting in the total failure of the engine, and the pilot's failure to compensate for wind conditions that led him to over fly the runway during his forced landing. Factors were the pilot's diverted attention due to smoke in the cockpit, and the tailwind weather condition.

the pilot exceeded the proper touchdown point during the landing. Factors associated with the accident were the fence and the ditch which the airplane contacted.

The failure of the left magneto, which resulted in a partial loss of engine power. Factors were the fouled number 3, 4, and 5 rear spark plugs and the lack of suitable terrain for the precautionary landing.

The pilot's failure to maintain clearance from the rising terrain. Factors include his poor decision to depart without assurance that he could clear the surrounding terrain under the ambient conditions, his failure to adhere to the accepted procedure of leaning the fuel mixture for high-altitude takeoff, high density altitude, downdrafts, mountainous terrain, and tress along his departure path.

The pilot's improper remedial action and his failure to maintain directional control of the airplane during landing. A factor in the accident was the pilot's excessive use of the airplane brakes.

The pilot's inadequate compensation for a crosswind and his failure to maintain directional control during landing, resulting in the airplane veering off the runway and the subsequent collision with a culvert.

The pilot's inadequate compensation for wind conditions and his delayed go-around, which resulted in the loss of aircraft control. A factor was the turbulent weather conditions.

The pilot's improper recovery from a bounced landing. A factor in the accident was the pilot's decision to operate the airplane over the maximum gross weight and his improper landing flare.

the total loss of engine power while in cruise flight due to the fatigue failure of the engine's anti-ice bleed air line, which resulted in the pilot's inability to utilize the engine anti-ice system. Contributing factors were the icing conditions and the lack of suitable terrain for the forced landing.

the pilot failed to maintain altitude after inadvertently flying to instrument meteorological conditions. Factors associated with the accident were the low ceilings and visibility, the pilot became disoriented after inadvertently flying into IMC, and the pilot was not instrument rated.

The pilot's failure to follow aircraft operating procedures by not raising the flaps during the go-around maneuver. Contributing factors were the pilot's failure to adhere to the balked landing checklist (FLAPS to 20) resulting in degraded climb performance, and the power lines in his flight path.

The pilot's failure to attain proper alignment with the landing runway, and her failure to maintain proper glide path for the landing runway, resulting in an encounter with vortex turbulence from a preceding heavy aircraft landing on a parallel runway and subsequent loss of aircraft control. Factors included the pilot's lack of total flying experience, and crosswind conditions conducive to a vortex turbulence encounter.

The pilot's incorrect positioning of the fuel selector which resulted in fuel starvation. Factors were the pilot's lack of familiarity with the fuel system due to an inadequate checkout by a flight instructor, and the lack of suitable terrain for the forced landing.