What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Aircraft was involved in skydiving activities; accident occurred on 9th flight of the day; aircraft refueled immediately prior to takeoff. Pilot reported normal takeoff; at approximately 200 feet altitude the pilot observed loss of airspeed; noticed RPM was slowly decreasing and manifold pressure remained constant. Pilot turned left and attempted an emergency landing in a grass field; left wing clipped a utility pole on descent; aircraft became entangled in utility wires; aircraft landed; nose gear sheared off; aircraft spun approximately 180 degrees and traveled approximately 50 feet and came to a full stop; pilot and passengers exited aircraft. Fuel samples were taken from the aircraft and fueling source; visual inspecton of aircraft fueling source reveal a very small amount of water. Visual inspection of sample taken from refueling source nozzle appeared normal; fuel vender checked api gravity weight and found it to be normal. Aircraft engine was not maintained iaw oem recommended overhaul schedule. Aircraft exceed allowable gross weight on takeoff by as much as 150 pounds.
As the FAA filed it
(-23) AIRCRAFT WAS INVOLVED IN SKYDIVING ACTIVITIES; ACCIDENT OCCURRED ON 9TH FLIGHT OF THE DAY; AIRCRAFT REFUELED IMMEDIATELY PRIOR TO TAKEOFF. PILOT REPORTED NORMAL TAKEOFF; AT APPROXIMATELY 200 FEET ALTITUDE THE PILOT OBSERVED LOSS OF AIRSPEED; NOTICED RPM WAS SLOWLY DECREASING AND MANIFOLD PRESSURE REMAINED CONSTANT. PILOT TURNED LEFT AND ATTEMPTED AN EMERGENCY LANDING IN A GRASS FIELD; LEFT WING CLIPPED A UTILITY POLE ON DESCENT; AIRCRAFT BECAME ENTANGLED IN UTILITY WIRES; AIRCRAFT LANDED; NOSE GEAR SHEARED OFF; AIRCRAFT SPUN APPROXIMATELY 180 DEGREES AND TRAVELED APPROXIMATELY 50 FEET AND CAME TO A FULL STOP; PILOT AND PASSENGERS EXITED AIRCRAFT. FUEL SAMPLES WERE TAKEN FROM THE AIRCRAFT AND FUELING SOURCE; VISUAL INSPECTON OF AIRCRAFT FUELING SOURCE REVEAL A VERY SMALL AMOUNT OF WATER. VISUAL INSPECTION OF SAMPLE TAKEN FROM REFUELING SOURCE NOZZLE APPEARED NORMAL; FUEL VENDER CHECKED API GRAVITY WEIGHT AND FOUND IT TO BE NORMAL. AIRCRAFT ENGINE WAS NOT MAINTAINED IAW OEM RECOMMENDED OVERHAUL SCHEDULE. AIRCRAFT EXCEED ALLOWABLE GROSS WEIGHT ON TAKEOFF BY AS MUCH AS 150 POUNDS.
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 N4892D · 1
Matched to the same aircraft by N-number and date.