Shy Torque:
Your post mirrored my thinking. I remember when I was flying 330s; the aircraft was on the ground and the engines at ground idle when something sheared on the TR pitch assembly and the tail rotor went to full pitch setting cant remember which way. The force was sufficient to yaw the fuselage, even though on the ground at a low power setting.
Many discussions in the crew room on how to cope with that failure in the air and no positive answer, particularly if the aircraft was at low airspeed at the time.
Only way to stop the yaw is autorotation and pull collective to slow the NR
.?