What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On October 17, 2004 michael foley, the pilot, attempted to take off from his Private airstrip. The airstrip is approximately 2500 feet in length at an altitude of 4600 with an estimated 7% to 8% gradient on the south 2/3 of the runway. The pilot estimated the wind from the south at 30 knots. He elected to take off into the wind going uphill. The aircraft became airborne but made slight contact with the ground just past the end of the runway and proceeded through a barbed wire fence. The pilot indicated while he was attempting to return to land the engine was running roughly and eventually failed. The pilot completed approximately 150 degrees of a right turn when he contacted the top of the ridge. This contact crater had parts of the right main gearbox and right step. The aircraft came to rest 375 feet from the first indications of impact along a 300" magnetic course. The aircraft was roughly pointed in the opposite direction the aircraft had been traveling. The tail assembly was torn from the fuselage with only the control cables attached. There was no post accident fire.
As the FAA filed it
(-23) ON OCTOBER 17, 2004 MICHAEL FOLEY, THE PILOT, ATTEMPTED TO TAKE OFF FROM HIS PRIVATE AIRSTRIP. THE AIRSTRIP IS APPROXIMATELY 2500 FEET IN LENGTH AT AN ALTITUDE OF 4600 WITH AN ESTIMATED 7% TO 8% GRADIENT ON THE SOUTH 2/3 OF THE RUNWAY. THE PILOT ESTIMATED THE WIND FROM THE SOUTH AT 30 KNOTS. HE ELECTED TO TAKE OFF INTO THE WIND GOING UPHILL. THE AIRCRAFT BECAME AIRBORNE BUT MADE SLIGHT CONTACT WITH THE GROUND JUST PAST THE END OF THE RUNWAY AND PROCEEDED THROUGH A BARBED WIRE FENCE. THE PILOT INDICATED WHILE HE WAS ATTEMPTING TO RETURN TO LAND THE ENGINE WAS RUNNING ROUGHLY AND EVENTUALLY FAILED. THE PILOT COMPLETED APPROXIMATELY 150 DEGREES OF A RIGHT TURN WHEN HE CONTACTED THE TOP OF THE RIDGE. THIS CONTACT CRATER HAD PARTS OF THE RIGHT MAIN GEARBOX AND RIGHT STEP. THE AIRCRAFT CAME TO REST 375 FEET FROM THE FIRST INDICATIONS OF IMPACT ALONG A 300" MAGNETIC COURSE. THE AIRCRAFT WAS ROUGHLY POINTED IN THE OPPOSITE DIRECTION THE AIRCRAFT HAD BEEN TRAVELING. THE TAIL ASSEMBLY WAS TORN FROM THE FUSELAGE WITH ONLY THE CONTROL CABLES ATTACHED. THERE WAS NO POST ACCIDENT FIRE.
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 N101AM · 1
Matched to the same aircraft by N-number and date.