What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
On the morning of September 08, 2015 at 0845 an experimental amateur built, dragonfly ii departed Freeport/ Albertus airport from runway 24 with a destination of poplar grove airport, poplar grove, Illinois. The pilot stated at about 500 feet down the runway on takeoff roll, he noticed the engine was running rough, so he adjusted the mixture knob and noticed a puff of black smoke come from the engine exhaust pipe. He stated the engine seemed to run normal with the mixture adjustment. He stated once airborne he was only able to climb to approximately 200 feet AGL. Realizing he would not clear the trees off the end of the runway he elected to turn left and land the aircraft in a pasture. It was stated that a witness saw the aircraft porpoising through the air prior to hitting the ground. Upon impacting the ground the aircraft hit a barbed wire fence and post. Both main gear legs were torn from the aircraft along with the left canard and two of the three propeller blades. The fuselage was split apart at the instrument panel and the left side of the instrument panel was pushed forward about 6 to 8 inches. The pilots rudder pedals were pushed forward into the cabin side of the firewall. The pilot was able to open the canopy and exit the aircraft without assistance. There was no post crash fire. When the aircraft was being recovered, it was noted that fuel was leaking from the main fuel tank located under the pilot seat.
As the FAA filed it
ON THE MORNING OF SEPTEMBER 08, 2015 AT 0845 AN EXPERIMENTAL AMATEUR BUILT, DRAGONFLY II DEPARTED FREEPORT/ ALBERTUS AIRPORT FROM RUNWAY 24 WITH A DESTINATION OF POPLAR GROVE AIRPORT, POPLAR GROVE, ILLINOIS. THE PILOT STATED AT ABOUT 500 FEET DOWN THE RUNWAY ON TAKEOFF ROLL, HE NOTICED THE ENGINE WAS RUNNING ROUGH, SO HE ADJUSTED THE MIXTURE KNOB AND NOTICED A PUFF OF BLACK SMOKE COME FROM THE ENGINE EXHAUST PIPE. HE STATED THE ENGINE SEEMED TO RUN NORMAL WITH THE MIXTURE ADJUSTMENT. HE STATED ONCE AIRBORNE HE WAS ONLY ABLE TO CLIMB TO APPROXIMATELY 200 FEET AGL. REALIZING HE WOULD NOT CLEAR THE TREES OFF THE END OF THE RUNWAY HE ELECTED TO TURN LEFT AND LAND THE AIRCRAFT IN A PASTURE. IT WAS STATED THAT A WITNESS SAW THE AIRCRAFT PORPOISING THROUGH THE AIR PRIOR TO HITTING THE GROUND. UPON IMPACTING THE GROUND THE AIRCRAFT HIT A BARBED WIRE FENCE AND POST. BOTH MAIN GEAR LEGS WERE TORN FROM THE AIRCRAFT ALONG WITH THE LEFT CANARD AND TWO OF THE THREE PROPELLER BLADES. THE FUSELAGE WAS SPLIT APART AT THE INSTRUMENT PANEL AND THE LEFT SIDE OF THE INSTRUMENT PANEL WAS PUSHED FORWARD ABOUT 6 TO 8 INCHES. THE PILOTS RUDDER PEDALS WERE PUSHED FORWARD INTO THE CABIN SIDE OF THE FIREWALL. THE PILOT WAS ABLE TO OPEN THE CANOPY AND EXIT THE AIRCRAFT WITHOUT ASSISTANCE. THERE WAS NO POST CRASH FIRE. WHEN THE AIRCRAFT WAS BEING RECOVERED, IT WAS NOTED THAT FUEL WAS LEAKING FROM THE MAIN FUEL TANK LOCATED UNDER THE PILOT SEAT.
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 N24TL · 1
Matched to the same aircraft by N-number and date.