MELBOURNE, FL, USA
N81859
CESSNA T210L
THE ACFT WAS BEING FERRIED TO MELBOURNE BY A CONTRACTOR TO THE US MARSHALS SERVICE. BEFORE DEPARTURE INSPECTION AND ENGINE RUN-UP REVEALED A 500-600 RPM MAGNETO DROP; THE LEFT TANK WAS 3/4 FULL AND THE RIGHT TANK HAD APPROX 15 GALLONS OF FUEL, ACCORDING TO GAUGES. THE PLT HAD WORK DONE THAT REDUCED THE MAG DROP TO 200-250 RPM. THE PLT REPORTED THAT WHILE ON A 3-MILE FINAL TO RWY 4 AT MELBOURNE, THE ENGINE QUIT. HE SAID HE SWITCHED THE SELECTOR TO THE OTHER TANK. THE ACFT COLLIDED WITH TREES AND THE GROUND DURING A FORCED LANDING. THE FUEL SELECTOR WAS FOUND IN THE LEFT TANK POSITION. NO FUEL SYSTEM LEAKS WERE EVIDENT. FURTHER EXAMINATION REVEALED 3 OZ OF FUEL IN THE RT TANK; THE LEFT TANK CONTAINED 25 GALLONS BUT APPEARED TO BE 3/4 FULL. THE RT FUEL GAUGE WAS ACCURATE AND THE LEFT READ LOW WHEN TESTED. THE RT MAG DROP WAS 700 RPM DRG A TEST-RUN. THE RT MAG IMPULSE SPRING WAS BROKEN, ALLOWING INTERNAL TIMING TO VARY.
FAILURE OF THE PILOT TO ACCURATELY DETERMINE FUEL QUANTITY PRIOR TO DEPARTURE FOLLOWED BY HIS FAILURE TO OPERATE THE ENGINE ON THE FULLEST FUEL TANK RESULTING IN A FUEL TANK BEING RUN DRY RESULTING IN ENGINE FAILURE WHILE ON SHORT FINAL APPROACH AT HIS DESTINATION.
Source: NTSB Aviation Accident Database
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