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Scranton, SC
The helicopter pilot stated that he had just completed the first leg of a three-stop cross country flight. After landing, and hover-taxied toward the runway and performed a left pedal turn to observe the windsock. The pilot lost control of the helicopter, the tail rotor struck an embankment parallel to the runway, "which resulted in a 180-degree spin to the left and dynamic rollover." The helicopter came to rest on its left side, and incurred substantial damage to the fuselage, tail boom, and rotor blades. The pilot reported there were no mechanical malfunctions with the helicopter prior to the accident. He further stated that the accident could have been avoided by performance of the clearing turn farther from the embankment.
Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
The helicopter pilot stated that he had just completed the first leg of a three-stop cross country flight. After landing, he hover-taxied toward the runway and performed a left pedal turn to observe the windsock. The pilot lost control of the helicopter, the tail rotor struck an embankment parallel to the runway, "which resulted in a 180-degree spin to the left and dynamic rollover." The helicopter came to rest on its left side, and incurred substantial damage to the fuselage, tail boom, and rotor blades. The pilot reported there were no mechanical malfunctions with the helicopter prior to the accident. He further stated that the accident could have been avoided by performance of the clearing turn farther from the embankment.