Not much point in that test other than to see how it breaks.
If pilot does not react fast enough (usually within a couple of seconds) after loss of power, by lowering the collective lever to reduce blade pitch, the rotor speed will drop below a recoverable RPM and the rotors will stall. In that case it will end the same way as this demo.
As Frank said, in a real world scenario after loss of power, if pilot lowers collective pitch quickly, he can autorotate and with sufficient altitude and with a suitable flat landing spot available, it's completely survivable and may save machine without damage.

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