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Hendersonville, NC
REPORTEDLY, THE ENGINE POWER WAS NORMAL DURING THE ENGINE RUN-UP, GROUND ROLL AND LIFT-OFF. HOWEVER, SHORTLY AFTER TAKEOFF AT AN ALTITUDE OF ABOUT 250 FT AGL, THE ENGINE COUGHED, SPUTTERED AND LOST POWER. AT ABOUT THE SAME TIME, TWO WITNESSES NOTICED THAT THE AIRCRAFT SUDDENLY STARTED TO TRAIL BLACK SMOKE. THE INSTRUCTOR PILOT ASSUMED CONTROL OF THE AIRCRAFT AND ATTEMPTED TO TURN BACK AND LAND ON THE RUNWAY. HOWEVER, HE DID NOT HAVE ENOUGH ALTITUDE. THE AIRCRAFT CRASHED ABOUT .2 MI SHORT OF THE RUNWAY. DURING AN INVESTIGATION, AUTOMOTIVE TYPE FUEL WAS FOUND IN THE AIRCRAFT. THERE WAS SOME DAMAGE TO ONE SPARK PLUG, A ROCKER BOX COVER AND A MAGNETO HARNESS. THESE WERE REPLACED AND AN ENGINE RUN-UP WAS ACCOMPLISHED. THE RUN-UP WAS NORMAL EXCEPT FOR THE FUEL FLOW. AT 2665 RPM, THE FLOW WAS 61.5 PPH, BUT THE SPECIFICATION CALLED FOR 78 PPH.
REPORTEDLY, THE ENGINE POWER WAS NORMAL DURING THE ENGINE RUN-UP, GROUND ROLL AND LIFT-OFF. HOWEVER, SHORTLY AFTER TAKEOFF AT AN ALTITUDE OF ABOUT 250 FT AGL, THE ENGINE COUGHED, SPUTTERED AND LOST POWER. AT ABOUT THE SAME TIME, TWO WITNESSES NOTICED THAT THE AIRCRAFT SUDDENLY STARTED TO TRAIL BLACK SMOKE. THE INSTRUCTOR PILOT ASSUMED CONTROL OF THE AIRCRAFT AND ATTEMPTED TO TURN BACK AND LAND ON THE RUNWAY. HOWEVER, HE DID NOT HAVE ENOUGH ALTITUDE. THE AIRCRAFT CRASHED ABOUT .2 MI SHORT OF THE RUNWAY. DURING AN INVESTIGATION, AUTOMOTIVE TYPE FUEL WAS FOUND IN THE AIRCRAFT. THERE WAS SOME DAMAGE TO ONE SPARK PLUG, A ROCKER BOX COVER AND A MAGNETO HARNESS. THESE WERE REPLACED AND AN ENGINE RUN-UP WAS ACCOMPLISHED. THE RUN-UP WAS NORMAL EXCEPT FOR THE FUEL FLOW. AT 2665 RPM, THE FLOW WAS 61.5 PPH, BUT THE SPECIFICATION CALLED FOR 78 PPH.