Cessna Safety Record

THE PILOT'S IMPROPER FLARE AND IMPROPER RECOVERY FROM A BOUNCED LANDING, WHICH RESULTED IN A PORPOISE AND LOSS OF AIRCRAFT CONTROL. FACTORS RELATED TO THE ACCIDENT WERE: THE GUSTY CROSSWIND, AND FAILURE OF THE PILOT TO MAINTAIN RUNWAY ALIGNMENT.

AN ENGINE FAILURE CAUSED BY A MALFUNCTIONING CARBURETOR AND THE PILOT'S MISJUDGING HIS OBSTACLE CLEARANCE WHICH RESULTED IN A WIRE STRIKE WHILE MANEUVERING TO LAND. FACTORS IN THE ACCIDENT WERE THE UNCOMMANDED DEPLOYMENT OF CARBURETOR HEAT ON BOTH ENGINES, AN INOPERATIVE GEAR RETRACTION SYSTEM, AND A PROPELLER SYSTEM WHICH COULD NOT BE FEATHERED.

IMPROPER USE OF CARBURETOR HEAT BY THE PILOT, WHICH RESULTED IN CARBURETOR ICE. FACTORS RELATED TO THE ACCIDENT WERE: CARBURETOR ICING CONDITIONS, AND SOFT TERRAIN.

THE PILOT IN COMMAND'S INACCURATE FUEL CONSUMPTION CALCULATIONS, WHICH RESULTED IN LOSS OF ENGINE POWER DUE TO FUEL EXHAUSTION. FACTORS IN THIS ACCIDENT WERE: THE DARK NIGHT, AND THE SOFT/WET TERRAIN.

FAILURE OF THE #4 CONNECTING ROD. FACTORS RELATED TO THE ACCIDENT WERE: THE ADVERSE WEATHER CONDITIONS AND LACK OF SUITABLE TERRAIN FOR A FORCED LANDING.

IMPROPER PLANNING/DECISION BY THE PILOT, WHICH RESULTED IN FUEL EXHAUSTION, DUE TO AN INADEQUATE SUPPLY OF FUEL. FACTORS RELATED TO THE ACCIDENT WERE: THE OBSTRUCTIONS (UTILITY POLE, POWER LINE & FENCE) IN THE EMERGENCY LANDING AREA.

LOSS OF POWER IN THE RIGHT ENGINE DUE TO A DISCONNECTED DUCT BETWEEN THE TURBOCHARGER AND THE PLENUM CHAMBER. THE REASON FOR THE LOSS OF POWER IN THE LEFT ENGINE WAS NOT DETERMINED.

THE PILOT MISJUDGED HIS DISTANCE AND ALTITUDE ON FINAL APPROACH, AND FAILED TO REACH THE PROPER TOUCHDOWN POINT FOR LANDING. THE GUSTY CROSSWIND CONDITION WAS A RELATED FACTOR.

POOR JUDGEMENT OF THE PILOT DUE TO CONSUMPTION OF ALCOHOL, AND HIS MISJUDGEMENT OF DISTANCE AND ALTITUDE TO THE RUNWAY, WHILE ON FINAL APPROACH, WHICH SUBSEQUENTLY RESULTED IN A TOUCHDOWN AND NOSE OVER SHORT OF THE RUNWAY.

PILOT IN COMMAND'S INITIATION AND CONTINUATION OF THE FLIGHT INTO AN AREA OF KNOWN IMC WEATHER CONDITIONS AND HIS SUBSEQUENT INABILITY TO LAND PRIOR TO RUNNING OUT OF FUEL. CONTRIBUTING FACTORS TO THE ACCIDENT WERE THE PILOT'S FAILURE TO EXERCISE GOOD JUDGEMENT AND HIS DISREGARD FOR THE FEDERAL AIR REGULATIONS.

THE PILOT'S IMPROPER USE OF CARBURETOR HEAT WHICH CAUSED A POWER LOSS AND A FORCED LANDING IN UNSUITABLE TERRAIN. FACTORS RELATED TO THE ACCIDENT WERE CARBURETOR ICING CONDITIONS AND THE PILOTS LACK OF TOTAL EXPERIENCE.

THE PILOT'S FAILURE TO MAINTAIN SUFFICIENT TERRAIN CLEARANCE ALTITUDE DURING A LOW ALTITUDE TURN. CONTRIBUTING TO THE ACCIDENT WAS THE PILOT'S POOR JUDGEMENT IN CONDUCTING TOUCH-AND-GO LANDINGS WITH A 700-FOOT CEILING.

THE STUDENT PILOT'S IMPROPER PRE-FLIGHT PLANNING/PREPARATION, WHICH DID NOT INCLUDE A PLAN TO REFUEL THE AIRCRAFT AS NECESSARY. THE STUDENT PILOT'S LACK OF TOTAL EXPERIENCE CONTRIBUTED TO THIS ACCIDENT, AS DID THE CFI'S INADEQUATE SUPERVISION OF THE STUDENT.

PHYSICAL IMPAIRMENT OF THE VEHICLE DRIVER, FROM CONSUMPTION OF ALCOHOL, WHICH RESULTED IN A COLLISION WITH THE AIRPLANE. THE VEHICLE AND DARK NIGHT WERE CONSIDERED TO BE RELATED FACTORS.

FAILURE OF THE MIXTURE CONTROL CABLE, WHICH RESULTED IN A LOSS OF POWER DUE TO FUEL STARVATION DURING A CLIMB AFTER TAKEOFF. A FACTOR RELATED TO THE ACCIDENT WAS: ROUGH TERRAIN IN THE EMERGENCY LANDING AREA.

IMPROPER PLANNING/DECISION BY THE PILOT, WHICH RESULTED IN FUEL EXHAUSTION FROM AN INADEQUATE SUPPLY OF FUEL. FACTORS RELATED TO THE ACCIDENT WERE: FALSE FUEL GAGE INDICATIONS, LACK OF A SUITABLE AREA FOR A FORCED LANDING, AND OBSTRUCTIONS (UTILITY POLE & VEHICLE(S) IN THE EMERGENCY LANDING AREA.