Cessna 310 Safety Record

THE CFI'S FAILURE TO MAINTAIN AIRSPEED ABOVE VMC, RESULTING IN A LOSS OF CONTROL DURING THE SINGLE ENGINE G0-AROUND. FACTORS WERE NOT ATTAINING RUNWAY ALIGNMENT AND THE CFI'S FAILURE TO RETRACT THE LANDING GEAR FOR THE GO-AROUND PROCEDURE.

WAS THE LOSS OF CONTROL DUE TO THE PILOT'S SPATIAL DISORIENTATION FOLLOWING A COMPLETE ELECTRICAL SYSTEM FAILURE. FACTORS WERE THE DARK NIGHT AND THE ELECTRICAL FAILURE AS RESULT OF BURNED OUT WIRING TERMINAL.

the pilot's failure to maintain control of the airplane. Factors in the accident were the dark night lighting conditions, moderate to severe turbulence, and heavy rain.

LOSS OF AIRCRAFT CONTROL FOR AN UNDETERMINED REASON, AND SUBSEQUENT FLIGHT THAT RESULTED IN THE STRESS LIMITS OF THE AIRPLANE BEING EXCEEDED AND AIRFRAME FAILURE.

the pilot's improper in-flight planning/decision and his failure to maintain the minimum control airspeed which progressed to an inadverent stall/spin. Factors relating to this accident were fuel exhaustion and the pilot's lack of experience in the accident airplane.

THE PILOT'S FAILURE TO MAINTAIN AIRCRAFT CONTROL DUE TO ALCOHOL IMPAIRMENT. FACTORS WHICH CONTRIBUTED TO THE ACCIDENT WERE: THE PILOT'S INTENTIONAL FLIGHT INTO ADVERSE WEATHER, FOG, AND THE DARK NIGHT.

THE PILOT-IN-COMMAND'S FAILURE TO MAINTAIN AN ADEQUATE TERRAIN AVOIDANCE ALTITUDE. FACTORS WHICH CONTRIBUTED TO THE ACCIDENT WERE THE DARK NIGHT AND FEATURELESS SNOW COVERED TERRAIN, BOTH WHICH CREATED A 'FEATURELESS TERRAIN ILLUSION' WHICH PROBABLY LED THE PILOT TO VISUALLY OVERESTIMATE HIS ALTITUDE.

THE PILOT'S INADEQUATE ALTITUDE (OR CLEARANCE) FROM MOUNTAINOUS HILLY TERRAIN. FACTORS RELATED TO THE ACCIDENT WERE DARKNESS, LOW CLOUDS, AND LIGHT SNOW.

THE PILOT NOT FOLLOWING WAKE TURBULENCE (VOTEX) AVOIDANCE PROCEDURES, WHICH ARE DETAILED IN FAA PUBLICATIONS, RESULTING IN THE AIRPLANE ENCOUNTERING WAKE TURBULENCE. FACTORS IN THIS ACCIDENT WERE: 1) THE PILOT'S INABILITY TO CONTROL THE AIRPLANE AFTER ENCOUNTERING WAKE TURBULENCE, AND 2) INADEQUATE ALTITUDE TO EFFECT A RECOVERY FROM THE UNCONTROLLED DESCENT.

LOSS OF AIRCRAFT CONTROL FOR AN UNDETERMINED REASON AFTER THE PILOT TOOK OFF AT NIGHT AND FLEW THE AIRCRAFT INTO THE AREA OF A THUNDERSTORM AND LIGHTNING.

LOSS OF ENGINE POWER ON INITIAL TAKEOFF CLIMB ON ALL ENGINES FOR UNDETERMINED REASONS. THIS RESULTED IN A FORCED LANDING, IN FLIGHT COLLISION WITH TREES, TERRAIN, AND POSTCRASH FIRE.

THE PILOT'S CONTINUED VFR FLIGHT INTO IMC, AND HIS FAILURE TO ATTAIN A PROPER ALTITUDE OVER HIGH, MOUNTAINOUS TERRAIN. FACTORS WERE THE HIGH TERRAIN, AND THE FOG, CLOUDS, AND OBSCURATION AT THE ACCIDENT SITE.

INADEQUATE AIRSPEED, WHICH RESULTED IN AN INADVERTENT STALL/SPIN, AND FAILURE OF THE INSTRUCTOR PILOT TO TAKE SUFFICIENT REMEDIAL ACTION TO PREVENT THE LOSS OF CONTROL.

THE PILOT DID NOT FOLLOW THE PUBLISHED IFR PROCEDURES AND ALLOWED THE AIRPLANE TO DESCEND TO AN ALTITUDE INSUFFICIENT TO CLEAR THE TERRAIN. FACTORS WHICH CONTRIBUTED TO THE ACCIDENT WERE: THE PILOT'S APPREHENSION DUE TO THE LOW FUEL STATE, THE DARK NIGHT, ADVERSE WEATHER, AND THE MOUNTAINOUS TERRAIN.

THE PILOT'S CONTINUATION OF VFR FLIGHT INTO INSTRUMENT METEOROLOGICAL CONDITIONS RESULTING IN SPATIAL DISORIENTATION AND LOSS OF AIRCRAFT CONTROL. FACTORS WHICH CONTRIBUTED TO THE ACCIDENT WERE: THE ADVERSE WEATHER CONDITIONS AND THE PILOT'S FAILURE TO OBTAIN AN ADEQUATE WEATHER BRIEFING BEFORE FLIGHT.

THE LOSS OF DIRECTIONAL CONTROL AS RESULT OF THE VELOCITY MINIMUM CONTROL AIRSPEED NOT BEING MAINTAINED. A FACTOR WAS THAT THE MANEUVER WAS INITIATED AT AN INADEQUATE ALTITUDE TOO LOW FOR THE PILOT TO RECOVER.

IMPROPER PLANNING/DECISION BY THE PILOTS OF BOTH AIRCRAFT, AND THE MITSUBISHI PILOT'S MISJUDGMENT OF HIS POSITION, WHILE ATTEMPTING TO FLY FORMATION AT NIGHT WITH AN AIRCRAFT THAT DID NOT HAVE ALL NAVIGATION LIGHTS OPERATIVE. FACTORS RELATED TO THE ACCIDENT WERE: BOTH PILOT'S LACK OF TRAINING IN THE TYPE OF OPERATION, DARKNESS, INOPERATIVE NAVITGATION (TAIL) LIGHT ON THE CESSNA 310, AND THE LACK OF VISUAL PERCEPTION THAT WOULD HAVE BEEN AVAILABLE TO THE MITSUBISHI PILOT.

THE CESSNA PILOT MISJUDGE HIS ALTITUDE ABOVE THE WATER. CONTRIBUTING FACTORS WERE: THE PILOT ALLOWING HIS ATTENTION TO BE DIVERTED AND HIS LACK OF VISUAL/DEPTH PERCEPTION OVER THE CALM (GLASSY) WATER.

THE PILOT-IN-COMMAND'S INTENTIONAL VFR FLIGHT INTO INSTRUMENT METEOROLOGICAL WEATHER CONDITIONS, AND HIS FAILURE TO MAINTAIN ADEQUATE ALTITUDE TO PROVIDE TERRAIN CLEARANCE. CONTRIBUTING FACTORS WERE: THE MOUNTAINOUS TERRAIN, ADVERSE WEATHER CONDITIONS, AND THE SECOND PILOT'S POSSIBLE REDUCED VISION DUE TO HIS VISION PROBLEM AND MEDICATION.