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Daytona Beach, FL
FLT EXPERIENCED ENGINE FAILURE WHILE DESCENDING FOR LANDING. WHILE APPROACHING A FIELD FOR A FORCED LANDING THE AIRCRAFT STRUCK ELECTRICAL POWER LINES AND THEN CRASHED INTO THE FIELD. THE ENGINE WAS OPERATED TO FULL POWER AFTER THE ACCIDENT WITH NO EVIDENCE OF PRECRASH MECHANICAL FAILURE OR MALFUNCTION. POST CRASH CALCULATIONS REVEALED THE AIRCRAFT SHOULD HAVE HAD 12 GALLONS OF FUEL ONBOARD AT THE TIME OF THE ACCIDENT. THE AIRCRAFT WAS OPERATION UNDER CONDITIONS CONDUCIVE TO SERIOUS CARBURETOR ICING AT GLIDE POWER HOWEVER THE PILOT STATED CARBURETOR HEAT WAS USED THROUGHOUT THE DESCENT. POST CRASH EXAMINATION OF THE CARBURETOR HEAT SYSTEM REVEALED IT TO BE INTACT WITH NO EVIDENCE OF MALFUNCTION.
FLT EXPERIENCED ENGINE FAILURE WHILE DESCENDING FOR LANDING. WHILE APPROACHING A FIELD FOR A FORCED LANDING THE AIRCRAFT STRUCK ELECTRICAL POWER LINES AND THEN CRASHED INTO THE FIELD. THE ENGINE WAS OPERATED TO FULL POWER AFTER THE ACCIDENT WITH NO EVIDENCE OF PRECRASH MECHANICAL FAILURE OR MALFUNCTION. POST CRASH CALCULATIONS REVEALED THE AIRCRAFT SHOULD HAVE HAD 12 GALLONS OF FUEL ONBOARD AT THE TIME OF THE ACCIDENT. THE AIRCRAFT WAS OPERATION UNDER CONDITIONS CONDUCIVE TO SERIOUS CARBURETOR ICING AT GLIDE POWER HOWEVER THE PILOT STATED CARBURETOR HEAT WAS USED THROUGHOUT THE DESCENT. POST CRASH EXAMINATION OF THE CARBURETOR HEAT SYSTEM REVEALED IT TO BE INTACT WITH NO EVIDENCE OF MALFUNCTION.