Trying to convert Trim Limitations to CoG, Lever Arms etc. I the manual it gives;-

C. of G. Datum point 2.54" forward of centre line of main landing wheels.

C. of G. Forward limit 11.4" aft of datum.

C. of G. Aft limit 22.8" aft of datum.

Moment of Pilot and passenger 21.65".

Moment of front fuel -5.1".

Moment of rear fuel 43.3"

Moment of luggage shelf 43.3"

Max weight on luggage shelf 58lbs???? my copy is indistinct

Max all up weight Can't read a thing at this point!

I want sufficient info to complete the weight and balances section if anyone can help.

Thanks