Sterling City, TX, USA
N410MM
Robinson R22
The pilot exited the helicopter with the engine set to idle power. Subsequently, the collective/throttle increased due to the engine vibrations, and the helicopter became light on the skids. The helicopter rocked back on the tail, which separated the tail rotor from the helicopter and damaged the main rotor blades. The manufacturer had previously issued a safety notice, which stated to never exit the helicopter unattended with the engine running and the rotors turning because the collective can "creep up, increasing both pitch and throttle, allowing the helicopter to lift off or roll out of control," as occurred in this accident.
The pilot reported to the Federal Aviation Administration Inspector that he was working with the land owner to conduct cattle herding with the helicopter. He landed in the field and got out to speak with the land owner about the flight. The pilot left the helicopter at idle power when he exited. While speaking to the land owner, the collective/throttle increased and the helicopter rocked back on the tail, separating the tail rotor. The main rotor blades were then damaged when the helicopter settled back down.The helicopter received substantial damage to the tail rotor and main rotor blades. Robinson Helicopter's issued Safety Notice SN-17 in November 1984, revised June 1994, which stated: NEVER EXIT HELECOPTER WITH ENGINE RUNNING Several accidents have occurred when pilots momentarily left their helicopters unattended with the engine running and rotors turning. The collective can creep up, increasing both pitch and throttle, allowing the helicopter to lift off or roll out of control.
The pilot’s improper decision to exit the helicopter without shutting down the engine, which allowed the collective/throttle to increase and resulted in a loss of control of the unattended helicopter.
Source: NTSB Aviation Accident Database
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