What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Agricultural operator had just received a 30-40 gallon fuel load and had taken on a 50 gallon load of pesticide. After taking off and leveling at approximately 3 feet, the pilot while traveling horizontal, accelerated in an attempt to gain altitude. But the aircraft lost altitude and hit the muddy ground with his left skid. At that time the aircraft immediately stopped causing the main rotor to flex. The rotor flexed to the point that it struck and cut off the tail rotor and boom assembly. (.4) the pilot had been spraying the field for about 3 hours. He attempted to take off at or over gross weight and the rotor RPM began to decay. The helicopter was positioned perpendicular to the furrowed rows in the field and when the pilot attempted to land the left skid dug into the mud. The aircraft bounced forward and the main rotor blades flexed downward and severed the tailboom. The pilot reported that he had not experienced any mechanical discrepancies with the aircraft prior to the accident. He further stated that he had not experienced any problems with the engine during the accident.
As the FAA filed it
(-23) AGRICULTURAL OPERATOR HAD JUST RECEIVED A 30-40 GALLON FUEL LOAD AND HAD TAKEN ON A 50 GALLON LOAD OF PESTICIDE. AFTER TAKING OFF AND LEVELING AT APPROXIMATELY 3 FEET, THE PILOT WHILE TRAVELING HORIZONTAL, ACCELERATED IN AN ATTEMPT TO GAIN ALTITUDE. BUT THE AIRCRAFT LOST ALTITUDE AND HIT THE MUDDY GROUND WITH HIS LEFT SKID. AT THAT TIME THE AIRCRAFT IMMEDIATELY STOPPED CAUSING THE MAIN ROTOR TO FLEX. THE ROTOR FLEXED TO THE POINT THAT IT STRUCK AND CUT OFF THE TAIL ROTOR AND BOOM ASSEMBLY. (.4) THE PILOT HAD BEEN SPRAYING THE FIELD FOR ABOUT 3 HOURS. HE ATTEMPTED TO TAKE OFF AT OR OVER GROSS WEIGHT AND THE ROTOR RPM BEGAN TO DECAY. THE HELICOPTER WAS POSITIONED PERPENDICULAR TO THE FURROWED ROWS IN THE FIELD AND WHEN THE PILOT ATTEMPTED TO LAND THE LEFT SKID DUG INTO THE MUD. THE AIRCRAFT BOUNCED FORWARD AND THE MAIN ROTOR BLADES FLEXED DOWNWARD AND SEVERED THE TAILBOOM. THE PILOT REPORTED THAT HE HAD NOT EXPERIENCED ANY MECHANICAL DISCREPANCIES WITH THE AIRCRAFT PRIOR TO THE ACCIDENT. HE FURTHER STATED THAT HE HAD NOT EXPERIENCED ANY PROBLEMS WITH THE ENGINE DURING THE ACCIDENT.
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 N3084G · 3
Matched to the same aircraft by N-number and date.