Cessna 414 Safety Record

the pilot misjudged distance and speed on final approach to land and failed to attain a proper touchdown point during the landing, which resulted in an overrun of the runway and collision with a fence. A related factor was the loss of engine power during flight.

failure of the pilot to maintain adequate airspeed, while maneuvering, which resulted in an advertent stall and collision with trees, vehicles, and the terrain.

the pilot's continued flight into known icing conditions with an inadequate windscreen deicing system and the diminished visual lookout. Factors were the icing weather conditions and the windscreen ice.

The pilot's inadequate inflight decision which resulted in VFR flight into instrument meteorological conditions and his failure to maintain adequate terrain clearance which resulted in an inflight collision with terrain. The low ceiling was a factor.

VFR flight by the pilot into instrument meteorological conditions (IMC), and his failure to maintain sufficient altitude/clearance from rising/mountainous terrain. Factors relating to the accident were: the terrain and weather conditions.

The pilot's continued VFR flight into obscured, rising mountainous terrain, and his failure to climb the airplane as conditions worsened. Factors included the rising terrain and the weather obscuration.

THE PILOT'S INACCURATE WEIGHT AND BALANCE CALCULATIONS WHICH RESULTED IN AN OVER MAXIMUM ALLOWABLE GROSS WEIGHT TAKEOFF. CONTRIBUTING TO THE ACCIDENT WAS THE WET, DOWNSLOPING CONDITION OF THE RUNWAY.

the pilot's inadequate compensation for wind conditions, which resulted in an undershoot of the proper touchdown point for landing. Factors relating to the accident were: the unfavorable wind conditions and the exposed runway lip.

THE PILOT'S DELAYED INITIATION OF THE MISSED APPROACH UNTIL WELL BELOW THE MINIMUM DESCENT ALTITUDE AND BEYOND THE PUBLISHED MISSED APPROACH POINT. FACTORS WERE THE DARK NIGHT AND THE LOW CEILING AND VISIBILITY.

THE LOSS OF POWER ON THE LEFT ENGINE FOR UNDETERMINED REASONS. A FACTOR WAS THE FAILURE OF THE RIGHT ENGINE DUE TO MAINTENANCE PERSONNEL'S FAILURE TO PROPERLY TORQUE THE CYLINDER THROUGH BOLTS.

THE PILOT'S INADEQUATE PREFLIGHT PLANNING/PREPARATION AND SELECTION OF THE WRONG RUNWAY FOR TAKEOFF. FACTORS RELATED TO THE ACCIDENT WERE: THE UPHILL SLOPE OF THE RUNWAY, TAILWIND, HIGH DENSITY ALTITUDE, AND FAILURE OF THE PILOT TO CORRECTLY CONFIGURE THE FLAPS FOR TAKEOFF.

THE FAILURE OF THE PILOT-IN-COMMMAND TO PROPERLY FLARE BEFORE TOUCHDOWN AND THE PILOT'S DECISION TO LAND WITH EXCESSIVE AIRSPEED. A CONTRIBUTING FACTOR WAS THE APREHENSION/ANXIETY OF THE PILOT DURING THE PRECAUTIONARY LANDING.

THE DISENGAGEMENT OF THE GEAR DOWN-LOCK MECHANISM DUE TO CORROSION AND THE PILOT'S INTENTIONAL OPERATION OF THE AIRCRAFT WITH KNOWN DEFICIENCIES IN EQUIPMENT.

INADEQUATE VISUAL LOOKOUT BY THE PILOTS OF BOTH AIRCRAFT. FACTORS RELATED TO THE ACCIDENT WERE: FAILURE OF THE PILOT OF N9317L TO ILLUMINATE HIS AIRCRAFT NAVIGATION LIGHTS, AND IMPROPER RADIO COMMUNICATIONS BY THE PILOT OF N47WD BY SELECTING THE WRONG UNICOM FREQUENCY TO MONITOR AND ANNOUNCE HIS LANDING INTENTIONS AND POSITION.

THE DECISION OF THE PILOT NOT TO FOLLOW INSTRUMENT FLIGHT RULE PROCEDURES DURING INSTRUMENT METEOROLOGICAL CONDITIONS AND POOR PREFLIGHT PLANNING WHICH RESULTED IN OPERATION OF THE AIRPLANE OVER THE MAXIMUM GROSS WEIGHT AND REDUCED PERFORMANCE. FACTORS IN THE ACCIDENT WERE THE FOGGY WEATHER CONDITIONS, AND HIGH TERRAIN.

THE FAILURE OF THE PILOT TO USE PITOT STATIC SYSTEM COVERS DURING ICING CONDITIONS WHICH RESULTED IN A BLOCKED PITOT TUBE AND SUBSEQUENT LOSS OF AIRSPEED INDICATIONS. THIS LED TO PILOT DISORIENTATION AND AN INVERTANT STALL. FACTORS TO THE ACCIDENT WERE IMPROPER SNOW REMOVAL AND ADVERSE WEATHER CONDITIONS.

THE PILOT'S POOR JUDGEMENT IN ATTEMPTING FLIGHT AFTER THE AIRPLANE'S FUSELAGE WAS DAMAGED DURING A LOADING OPERATION. FACTORS WHICH CONTRIBUTED TO THE ACCIDENT WERE: THE OPERATOR'S FAILURE TO PROVIDE PROPER WEIGHT AND BALANCE DATA FOR THE AIRPLANE, THE PILOT'S FAILURE TO SUPERVISE THE LOADING OPERATION, AND HIS FAILURE TO ACCEPT THE SERVICES OF A MECHANIC TO INSPECT THE DAMAGE.

THE PILOT'S FAILURE TO MAINTAIN AN ADEQUATE APPROACH SPEED WHICH RESULTED IN AN IMPROPER FLARE. FACTORS CONTRIBUTING TO THE ACCIDENT WERE THE INADEQUATE INFLIGHT DEICING OF THE AIRFRAME SURFACES AND IN ICING CONDITIONS ENCOUNTERED.

DIRECTIONAL CONTROL WAS NOT MAINTAINED BY THE PILOT. FACTORS RELATED TO THE ACCIDENT WERE: AIRPORT SNOW REMOVAL HAD NOT BEEN PERFORMED BY THE AIRPORT PERSONNEL, A DARK NIGHT WITH FALLING SNOW AND THE SNOWBANK ON THE RUNWAY.

THE PILOT'S IMPROPER EMERGENCY PROCEDURES BY NOT RETRACTING THE LANDING GEAR WHEN HE SHUT THE ENGINE DOWN AND HIS FAILURE TO MAINTAIN AIRSPEED. THE SCAVENGE PUMP FAILURE, SHUTTING DOWN THE ENGINE AND THE INADVERTENT STALL WERE FACTORS IN THE ACCIDENT.