Load factor equals lift divided by weight so the doubling of the lift force to maintain altitude in a 60 degree bank constitutes a doubling of load factor.
This does not however mean that the occupants of the aircraft are under 2g. They will simply be supported by the sides of their seets.
Hmm, on the contrary I
do hope that the acceleration (including load factor) affecting the self-loading cargo and the airframe will be more or less the same at all times. People tend to react poorly to being thrown into walls (or, to be exact, have walls thrown at them). Cases where the load factor and g load on passengers differ significantly (although only very briefly) would be when encountering severe CAT...
Isn't it annoying when you're thinking one thing and end up typing something different.
Cheers,
/ft