From a thread posted in March:
The link in the quote discusses low rotor RPM, and the ‘line’ mentioned is this one:
LOW ROTOR RPM STALL CAN BE FATAL
<snip>
The resulting boom chop, however, is somewhat acedemic, as the aircraft and it occupants are already doomed by the stalled rotor before the chop occurs.
Yesterday a helicopter crashed in Spokane Valley, Washington. Link.
According to witness reports, the helicopter appeared to lose power to the main rotor, which caused the rotors to “droop down.” The tail rotor broke off from the rear wing, causing the craft to lose control. It was reportedly spinning “360s” before it crashed into a yard. The pilot died upon impact, witnesses said.
A 13-year-old witness said, ‘It was making a sound like a quarter in a washing machine, then there was a loud pop,” and the craft started spinning.’
Of course the cause of the crash will have to be determined by investigators, but it sounds like a classic low rotor RPM situation that occurred after a loss of power. The ‘quarter in a washing machine’ comment makes me suspect a blown jug. Perhaps there was a failure of a shaft, but I’m guessing that that would cause the spin before the boom chop. If the sequence is as the boy described, it sounds like the shaft was turning the tail rotor (and thus preventing the spin) until the chop. Having no other information other than there was a mechanical problem and a boom chop, my hypothesis is as follows: The aircraft suffered a loss of power. The student pilot did not lower the collective lever rapidly enough to maintain rotor RPM. The rotor stalled and severed the tail boom. The pilot was, as the Safety Notice states, ‘doomed’.
The R22 has a low-inertia rotor system. That is, it’s lightweight and doesn’t have the mass to keep turning for very long in the event of a power failure. It is critical to lower the collective immediately to reduce the pitch of the rotor and enter autorotation. You have like a second, so pilots are trained to the point where the response is automatic – or should be. Entering autorotation after a power failure also includes canceling inputs to the anti-torque rotor, as there is no longer any torque (except for friction) to counteract.