Cessna 310 Safety Record

the pilot's failure to lower the landing gear and to properly align the airplane with the runway. Factors associated with the accident were: the inoperative gear warning, degraded aircraft performance, the pilot's diverted attention, the pilot's decision to perform a go-around, the snow bank and the runway which the airplane traveled across.

The pilot's failure to maintain adequate airspeed, which resulted in a stall. A factor related to the accident was the pilot's inadequate preflight inspection, which failed to secure the right engine oil cap, resulting in oil exhaustion and the loss of engine power.

inadequate maintenance inspection of the landing gear system, following a prior incident, due to the mechanic's failure to follow the service manual instructions.

The pilot-in-command's improper fuel management and improper positioning of the fuel selector valve to the empty fuel tank. Factors in the accident were: the PIC's improper in-flight planning and decision, his failure to list an alternate airport, and his decision to allow the newly hired copilot to perform instrument approaches in marginal weather which led to numerous instrument approaches and missed approaches.

the pilot's inadequate compensation for wind conditions, and his failure to maintain directional control of the airplane during the landing roll. Related factors were: the pilot's misunderstanding of the wind conditions, and the resultant quartering tail wind.

The pilot's failure to maintain a climb following initiation of a missed approach in fog due to spatial disorientation, and his inadequate training by company personnel. Potential rescue was delayed due to the FAA radar controller's failure to follow established communication procedures for overdue aircraft.

water/ice contamination in the fuel system and/or fuel filters due to failure of the maintenance facility that performed the annual inspection to identify and replace four cracked and deteriorated fuel filler cap O-rings. A factor in this accident was the pilot's failure to identify, and recognize the contamination hazard with, the cracked and deteriorated fuel filler cap O-rings during the preflight of the aircraft.

the pilot's inadequate preflight planning/preparation and inadequate management of the airplane's fuel supply, which resulted in fuel exhaustion and a forced landing at night. Factors related to the accident were: an inaccurate fuel quantity indicating system, darkness, and trees in the emergency landing area.

the pilot's inadequate preflight planning/preparation and fuel consumption calculations resulting in fuel exhaustion. The pilot's failure to switch the fuel tanks to the auxiliary position and feather both propellers were factors.

loss of total engine power due to fuel exhaustion for undetermined reason(s). The lack of suitable terrain for the forced landing was a related factor. The worn and leaking fuel system components and inadequate maintenance by unknown personnel were possible factors.

failure of the pilot to maintain aircraft control due to spatial disorientation. Factors were clouds and dark night light conditions, and the pilot's diverted attention due to a landing gear problem.

the failure of the pilot of the PA-32R, N1030Q, to obtain identification of the Cessna 310R, N1835E, visually, and his inadequate visual outlook. A factor was the failure of both pilots to hear communications from each other.

The pilot's failure to maintain visual flight conditions which resulted in the loss of control and subsequent inflight breakup of the airplane when he exceeded the design stress limits of the airframe.

failure of the pilot to follow emergency procedure(s) and/or feather the respective propeller after loss of power in the left engine for an undetermined reason. The undetermined loss of power (left engine) was a related factor.