LODI, CA, USA
N62421
HILLER UH-12E
WHILE ON AN AERIAL AGRICULTURAL SPRAYING FLIGHT THE ACFT ENGINE LOST TOTAL POWER. THE PLT EXECUTED AN IMMEDIATE AUTOROTATION LANDING. UPON GROUND CONTACT, THE ACFT SKID FOR ABOUT 8 FT UNTIL THE FRONT SKID CONTACTED THE GROUND FURROW AND NOSED OVER CAUSING THE MAIN ROTOR BLADE TO CONTACT THE GROUND AND TAIL BOOM ASSEMBLY. THE PILOT REPORTED THAT HE HAD ABOUT 10 - 12 GALLONS ABOARD FOR THE 5 MINUTE FLIGHT AND THAT HE BELIEVED THE FUEL PUMP BYPASS VALVE MALFUNCTIONED CAUSING THE FUEL TO BE 'DUMPED OVERBOARD' VIA THE SYSTEM DRAIN VALVE. INVESTIGATION REVEALED THAT THE ACFT CONTAINED LESS THAN 1/2 PT OF FUEL. THE ENGINE WAS FUNCTIONALLY TESTED AND IT OPERATED NORMALLY.
Source: NTSB Aviation Accident Database
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