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Big Spring, TX
THE AIRPLANE WAS CONDUCTING AERIAL PIPELINE SURVEY, WHEN AN EYEWITNESS OBSERVED THE AIRPLANE TO PULL UP INTO A STEEP CLIMB, EXECUTE A WING OVER TYPE MANEUVER, FOLLOWED BY A STEEP DIVE. THE AIRPLANE COLLIDED WITH THE GROUND IN A WINGS LEVEL, SLIGHTLY NOSE HIGH ATTITUDE. THE INITIAL IMPACT SCARS AND PROPELLER STRIKES INDICATED A HIGH VERTICAL SINK RATE. THE FORWARD VELOCITY WAS APPROXIMATELY 142 KNOTS BASED UPON THE PROPELLER SLASH MARKS. ADDITIONALLY, THE TOTAL GROUND TRAVEL WAS 285 FEET EXCLUDING THE MAIN WHEEL ASSEMBLIES.
THE PILOT'S FAILURE TO RECOVER FROM AN AEROBATIC MANEUVER DUE TO INSUFFICIENT ALTITUDE.
THE AIRPLANE WAS CONDUCTING AERIAL PIPELINE SURVEY, WHEN AN EYEWITNESS OBSERVED THE AIRPLANE TO PULL UP INTO A STEEP CLIMB, EXECUTE A WING OVER TYPE MANEUVER, FOLLOWED BY A STEEP DIVE. THE AIRPLANE COLLIDED WITH THE GROUND IN A WINGS LEVEL, SLIGHTLY NOSE HIGH ATTITUDE. THE INITIAL IMPACT SCARS AND PROPELLER STRIKES INDICATED A HIGH VERTICAL SINK RATE. THE FORWARD VELOCITY WAS APPROXIMATELY 142 KNOTS BASED UPON THE PROPELLER SLASH MARKS. ADDITIONALLY, THE TOTAL GROUND TRAVEL WAS 285 FEET EXCLUDING THE MAIN WHEEL ASSEMBLIES.