The susceptibility of a helicopter to a lateral rolling tendency.
Pivot point, rolling motion, exceeding the critical angle
The angle which if exceeded, recovery is impossible
Smooth moderate collective application
An uncommented rapid right yaw that does not subside of its own accord, and if not quickly reacted to will cause loss of aircraft control.
Pilot must anticipate the variations, concentrate on flying the aircraft and not allow yaw rates to build

Class 2
Weight and CG will readily be exceeded