What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
The PIC said he departed North Plains glider port (1OR4) and climbed to 400 feet AGL before starting a left turn. During the left turn, the engine suddenly went to idle. The PIC said the engine surged two more times then quit. The PIC continued his turn 180 degrees from his take off direction and landed in a field. The aircraft landed perpendicular to the crop rows causing the main gear to collapse underneath the wings.
The FAA arrived 4 hours after the accident. The fuel selected was set to the right fuel tank. Visual inspection of the fuel tanks revealed there was approximately 1-2 inches of fuel in the left fuel tank and no visible fuel in the right fuel tank; however the sides and bottom of the fuel tank were moist. The left fuel tank was dripping fuel from the bottom of the tank near the fuselage. There was visible evidence that fuel had leaked out from right fuel tank. The leading edges of both wings had severe vertical creases causing a tear in the metal. Also, because the main gear is attached to the fuselage/fire wall area, it appeared the right main gear damaged the fuselage where the gear was attached.
The PIC said he checked his fuel before he departed and had approximately a half tank of fuel in the left tank and ¾ of fuel in the right fuel tank. The PIC also, indicated he recently worked on the carburetor and has flown the aircraft a few times with no problems since he worked on the carburetor.
As the FAA filed it
THE PIC SAID HE DEPARTED NORTH PLAINS GLIDER PORT (1OR4) AND CLIMBED TO 400 FEET AGL BEFORE STARTING A LEFT TURN. DURING THE LEFT TURN, THE ENGINE SUDDENLY WENT TO IDLE. THE PIC SAID THE ENGINE SURGED TWO MORE TIMES THEN QUIT. THE PIC CONTINUED HIS TURN 180 DEGREES FROM HIS TAKE OFF DIRECTION AND LANDED IN A FIELD. THE AIRCRAFT LANDED PERPENDICULAR TO THE CROP ROWS CAUSING THE MAIN GEAR TO COLLAPSE UNDERNEATH THE WINGS.
THE FAA ARRIVED 4 HOURS AFTER THE ACCIDENT. THE FUEL SELECTED WAS SET TO THE RIGHT FUEL TANK. VISUAL INSPECTION OF THE FUEL TANKS REVEALED THERE WAS APPROXIMATELY 1-2 INCHES OF FUEL IN THE LEFT FUEL TANK AND NO VISIBLE FUEL IN THE RIGHT FUEL TANK; HOWEVER THE SIDES AND BOTTOM OF THE FUEL TANK WERE MOIST. THE LEFT FUEL TANK WAS DRIPPING FUEL FROM THE BOTTOM OF THE TANK NEAR THE FUSELAGE. THERE WAS VISIBLE EVIDENCE THAT FUEL HAD LEAKED OUT FROM RIGHT FUEL TANK. THE LEADING EDGES OF BOTH WINGS HAD SEVERE VERTICAL CREASES CAUSING A TEAR IN THE METAL. ALSO, BECAUSE THE MAIN GEAR IS ATTACHED TO THE FUSELAGE/FIRE WALL AREA, IT APPEARED THE RIGHT MAIN GEAR DAMAGED THE FUSELAGE WHERE THE GEAR WAS ATTACHED.
THE PIC SAID HE CHECKED HIS FUEL BEFORE HE DEPARTED AND HAD APPROXIMATELY A HALF TANK OF FUEL IN THE LEFT TANK AND ¾ OF FUEL IN THE RIGHT FUEL TANK. THE PIC ALSO, INDICATED HE RECENTLY WORKED ON THE CARBURETOR AND HAS FLOWN THE AIRCRAFT A FEW TIMES WITH NO PROBLEMS SINCE HE WORKED ON THE CARBURETOR.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.