CG out of AFT limit
Yesterday we received the final figures before take-off and we noticed a very strange cabin distribution. (Since we make our own loadsheets at dispatch, we assume average cabin distribution.)
We completed a manual loadsheet and it turned out that we were just out of our aft cg limit.
Off course we reseated pax to obtain good distribution and calculated a new mac and load&trim sheet.
We were discussing all possibilities had we not discovered this checkin error.
Tailstrike during rotation
Difficulties in attitude control (unable to control and reduce pitch)
I am wondering how dramatic things can turn out on those
a: aft cg (out of limits) and
b: trim set to average cabin distribution
Is there any (sim) experience?