Cessna T210 Safety Record

The pilot's inability to maintain aircraft control, which resulted in a loss of airspeed and a stall/spin. The inability of the pilot to maintain control of the airplane was likely due to an incapacitating cardiac event.

A loss of engine power due to fuel starvation as a result of the pilot's improper in-flight decision not to use the before landing checklist. A factor which contributed to the accident was the improper position of the mixture control.

the loss of engine power due to fuel exhaustion. Contributing factors were the pilot's inadequate preflight planning and lack of suitable terrain for the forced landing.

the pilot's failure to verify the current local wind condition that resulted in his selection of the wrong runway and an inadvertent downwind landing, a runway overrun and a ground collision with objects. A factor in the accident was the short runway and its dirt surface, which reduced brake effectiveness.

Failure of the Piper airplane pilot to obtain visual separation from the Cessna airplane rolling out after landing on the intersecting runway resulting in a collision between the two aircraft. A contributing factor was the evasive maneuver attempted be the pilot of the Cessna.

the pilot's inadvertent flight into adverse weather conditions, loss of control, and resulting exceedence of the design stress limits of the aircraft. which led to an in-flight structural failure. Factors in the accident included the pilot's inadequate preflight and in-flight planning and decision making, the severe turbulence, and the mountain wave.

An airborne fire which was fueled by leaking hydraulic fluid (the ignition source for the fire was undetermined) from the landing gear hydraulic system located under the cockpit instrument panel due to inadequate maintenance from other maintenance personnel. Contributing factors were the hydraulic fluid and the pilot's hard landing due the airplane's control not being possible subsequent to the loss of external visibility caused by smoke in the cockpit.

the pilot's in-flight loss of control due to spatial disorientation and a likely accumulation of airframe ice that led to a high speed descent and a structural breakup once the aerodynamic forces exceeded the strength limits of the structure. A factor in the accident was the pilot's lack of experience and training in instrument flight conditions.

the pilot's inadequate preflight preparation and failure to verify the fuel supply, which resulted in fuel exhaustion and subsequent loss of engine power.

The loss of engine power for undetermined reasons. Also causal was the pilot's improper in-flight emergency planning when he misjudged his available altitude and made a 360 degree turn away from the airport instead of proceeding directly to it, which resulted in him landing over a mile short of the runway in heavily wooded terrain. A factor was the prevailing high wind.

The total loss of engine power which was initiated by fretting of the crankcase halves for undetermined reasons, causing rotation of several of the main bearings, oil starvation, and subsequent failure of several of the connecting rods. A contributing factor was the rough terrain.

The pilot's failure to follow published procedures/directives (inducing excessive fuel flow to the engine), and the subsequent loss of engine power for nonmechanical reasons while on final approach. Contributing factors were the utility pole and the ditch.

The loss of engine power due to the failure of the number one connecting rod. A contributing factor was the lack of suitable terrain for the forced landing.

The lack of engine oil due to the mechanic's improper maintenance in not securing the loose "B" nut for the oil pressure line to the turbocharger leading to the loss of engine power while maneuvering. An additional cause was the unsuitable terrain the pilot encountered during the forced landing. A factor was the terrace the nose wheel impacted and subsequently nosed over.

The pilot's inadequate preflight inspection by his failure to secure the oil cap, which resulted in oil leakage on the windscreen, obstructing his vision, and his failure to maintain adequate airspeed.