N919AC is a 1988 Bell Helicopter Textron 206B. It is a rotorcraft with 5 seats, powered by a Rolls-Royc 250-C20B rated at 420 horsepower. The registration is active, with the registrant based in Darlington, IN. Its multiple airworthiness certificate was issued in Dec 2014. It has been registered to its current owner since Jan 2024. This page also carries 2 NTSB events.
- 38 years old
- 1 of 31 Bell Helicopter Textron 206B
2024
2014
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N919AC's record changes.
The pilot stated that while conducting agricultural spraying operations, he flew back to the fuel truck for fuel. He radioed his spotter and asked if the area was clear, and the spotter told him it was. He was attempting to land on a trailer when the tail rotor came into contact with some tree limbs and several tail rotor blades separated from the helicopter. The helicopter immediately lost tail rotor authority and began to yaw. The pilot then tried to move the helicopter away from the trailer and land on the ground. The tail rotor and gearbox separated from the helicopter before the pilot landed the helicopter on the ground. The helicopter’s empennage was substantially damaged during the accident sequence. The pilot reported that there were no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation.
The pilot was performing aerial application flights during which he returned to the landing zone five times to receive additional product. He recalled spending the majority of his time troubleshooting a spray rate system issue and was not paying attention to the fuel level while ground personnel were loading the product. During climb out on the final spray, the engine lost all power. During the subsequent autorotation and hard landing on a gravel road, the tail boom and tail rotor drive shaft sustained substantial damage.
The pilot reported that there were no preimpact mechanical malfunctions or failures with the helicopter and that upon landing he noticed that the fuel gauge showed empty.
Examination of the helicopter by a Federal Aviation Administration inspector found that a total of 2.5 gallons of uncontaminated Jet A fuel was able to be sumped from the helicopter’s fuel system. Residual and trace amounts of fuel were discovered in the engine driven fuel pump and fuel filters. The helicopter was not equipped with an optional low fuel light.
The helicopter flight manual advised to avoid uncoordinated turns and maneuvers with fewer than 20 gallons.
It is likely that while the pilot maneuvered out of the field following his final spray, the engine was starved of fuel, which resulted in the loss of engine power.
The operator following the accident amended their ground personnel training manual to require that both the ground personnel and the pilot ‘confirm fuel quantity OK’ prior to each takeoff.
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