Hi all,
I’m trying to understand how to determine CofG of my DG-100. In the
maintenance manual there is such sentence which I do not understand:
“The fuselage must be leveled so that the top of the aft fuselage boom
has a tail-down slope of l00 : 3.67.“
I understood that I need to lift up the sailplane tail, but what does
100:3.67 means? To what height? Can you help me with that?

BR,
Artiom.