On July 22, 2000, a Bell 206A-1 (registration N136C) was involved in an aviation accident near Bennettsville, SC. Investigators recorded the probable cause as: The pilot's failure to use proper remedial action to counteract a loss of tail rotor effectiveness resulting in collision with terrain during the subsequent uncontrolled descent. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.
A rotorcraft experienced a violent right spin after lifting off to a hover, resulting in the main rotor severing the tail boom and the aircraft rolling onto its side. The FAA found no evidence of mechanical failure.
Accident Sequence
According to the pilot and one passenger, the rotorcraft lifted off from the airstrip and rose to a hover at an altitude of about 2 to 3 feet. Immediately after reaching this hover, the rotorcraft began a violent spin to the right. The spin persisted until the landing skid and the nose section of the rotorcraft collided with the ground. The impact caused the main rotor to sever the tail boom, after which the main rotor itself collided with the terrain. The rotorcraft then rolled over onto its right side.
Investigation
The FAA examined the wreckage and reported no evidence of any mechanical failure. Furthermore, the rotorcraft was operating within its maximum takeoff weight and loading limits at the time of the accident. The density altitude at the location was recorded as 2,206 feet.
Frequently asked questions
What happened in the 22 Jul 2000 Bell 206A-1 accident near Bennettsville, SC?
A rotorcraft experienced a violent right spin after lifting off to a hover, resulting in the main rotor severing the tail boom and the aircraft rolling onto its side. The FAA found no evidence of mechanical failure.
What aircraft was involved and where did it happen?
The accident on 22 Jul 2000 involved a Bell 206A-1, registration N136C, at Bennettsville, SC.
What was the probable cause of the accident?
The pilot's failure to use proper remedial action to counteract a loss of tail rotor effectiveness resulting in collision with terrain during the subsequent uncontrolled descent.
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