20100514033939A

Accident · Destroyed

FAA accident report · Piper PA-24-250 · Redmond, OR · May 14, 2010

Date
May 14, 2010 · 07:09 local
Place
Redmond, OR
Airport
Roberts Field
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N6967P
NTSB investigation
NTSBWPR10FA239
Reported as
Piper PA-24-250
Reported engine
Lycoming 0-540 series
People aboard
1
Fatal injuries
1
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
0 total0 in this make and model0 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Aircraft took off normally with retracted gear and flaps. Between 200 and 400 ft. altitude, aircraft pitched nose up at approximately 90 degrees, climbed approx. 200 ft., entered a stall/spin, reversed direction 180 degrees and came to rest north of the approach end of runway 28. Flight control continuity was confirmed fuel confirmed in both wing tanks. Cockpit controls indicate the fuel boost pump was on, fuel tank selector was on the RH tank, auto pilot was off, the gear handle was in the up position and the flap handle was in the up position. Engine was running at point of impact. Propeller control high RPM (pushed forward), throttle in idle position (pulled out). Damage on the elevator trim indicator suggests the elevator trim was in the neutral position. The pilot was ejected from the aircraft, lying 10-15 feet behind the main wreckage. The pilot seat had a seat rail stop installed on the inboard track. Aircraft total time and pilot flight hours unavailable at this time.

As the FAA filed it

AIRCRAFT TOOK OFF NORMALLY WITH RETRACTED GEAR AND FLAPS. BETWEEN 200 AND 400 FT. ALTITUDE, AIRCRAFT PITCHED NOSE UP AT APPROXIMATELY 90 DEGREES, CLIMBED APPROX. 200 FT., ENTERED A STALL/SPIN, REVERSED DIRECTION 180 DEGREES AND CAME TO REST NORTH OF THE APPROACH END OF RUNWAY 28. FLIGHT CONTROL CONTINUITY WAS CONFIRMED FUEL CONFIRMED IN BOTH WING TANKS. COCKPIT CONTROLS INDICATE THE FUEL BOOST PUMP WAS ON, FUEL TANK SELECTOR WAS ON THE RH TANK, AUTO PILOT WAS OFF, THE GEAR HANDLE WAS IN THE UP POSITION AND THE FLAP HANDLE WAS IN THE UP POSITION. ENGINE WAS RUNNING AT POINT OF IMPACT. PROPELLER CONTROL HIGH RPM (PUSHED FORWARD), THROTTLE IN IDLE POSITION (PULLED OUT). DAMAGE ON THE ELEVATOR TRIM INDICATOR SUGGESTS THE ELEVATOR TRIM WAS IN THE NEUTRAL POSITION. THE PILOT WAS EJECTED FROM THE AIRCRAFT, LYING 10-15 FEET BEHIND THE MAIN WRECKAGE. THE PILOT SEAT HAD A SEAT RAIL STOP INSTALLED ON THE INBOARD TRACK. AIRCRAFT TOTAL TIME AND PILOT FLIGHT HOURS UNAVAILABLE AT THIS TIME.

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 N6967P · 1

Matched to the same aircraft by N-number and date.