Dubious logic - Nick
Two attitudes here:
Fuselage attitude
Disc attitude
Disc must run at an attitude to cancel translating tendancy
Fuselage attitude will be such that cg is directly below thrust unless modified by t/r thrust not being in the same horizontal plane as the disc (in which case a cg/thrust couple is required).
Rotor head matters (a bit)
In Rigid and Fully Articulated cases another (much over debated) couple also modifies the fuselage attitude - which does not apply in the pendulous type rotor heads.
Incidentally Nick is the only person I have seen correctly qualifying CW and CCW with "when viewed from above/below" - they are meaningless terms without. - Similar to: "captain the left hand engine is on fire"