What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On August 24, 2003, at 10:00 am CDT, a Ayres S2-R, N5671X, was substantially damaged while executing a forced landing into a field with small pine trees 1/2 mile from the intended landing site. The commercial pilot reported that he was flying back to wards flying service (wfig) at or about 100 feet AGL when the engine quit. The pilot was not injured. Visual meteorological conditions prevailed. The aircraft sustained substantial damage to the right aileron, lower right wing tip, tail section, tail wheel, broken step, collapsed left landing gear, left elevator and undercarriage. It was observed by the iic, there was about 1/4 to 1/2 inch height of fuel in left fuel tank while the right had none due to the tilted right wing. The pilot who also holds an A&P, said that he experienced a rough running engine on the same aircraft, the day before the accident and he suspected a faulty fuel pump. A follow-up inspection has been implemented to determine if the fuel pump had failed during the return flight.
As the FAA filed it
(-23) ON AUGUST 24, 2003, AT 10:00 AM CDT, A AYRES S2-R, N5671X, WAS SUBSTANTIALLY DAMAGED WHILE EXECUTING A FORCED LANDING INTO A FIELD WITH SMALL PINE TREES 1/2 MILE FROM THE INTENDED LANDING SITE. THE COMMERCIAL PILOT REPORTED THAT HE WAS FLYING BACK TO WARDS FLYING SERVICE (WFIG) AT OR ABOUT 100 FEET AGL WHEN THE ENGINE QUIT. THE PILOT WAS NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE TO THE RIGHT AILERON, LOWER RIGHT WING TIP, TAIL SECTION, TAIL WHEEL, BROKEN STEP, COLLAPSED LEFT LANDING GEAR, LEFT ELEVATOR AND UNDERCARRIAGE. IT WAS OBSERVED BY THE IIC, THERE WAS ABOUT 1/4 TO 1/2 INCH HEIGHT OF FUEL IN LEFT FUEL TANK WHILE THE RIGHT HAD NONE DUE TO THE TILTED RIGHT WING. THE PILOT WHO ALSO HOLDS AN A&P, SAID THAT HE EXPERIENCED A ROUGH RUNNING ENGINE ON THE SAME AIRCRAFT, THE DAY BEFORE THE ACCIDENT AND HE SUSPECTED A FAULTY FUEL PUMP. A FOLLOW-UP INSPECTION HAS BEEN IMPLEMENTED TO DETERMINE IF THE FUEL PUMP HAD FAILED DURING THE RETURN FLIGHT.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N5671X · 1
Matched to the same aircraft by N-number and date.