In the drawing for the AS5048 root airfoil, it shows a distance of 21.56"
between the main and aft center spars. Looking at my plans, there is a
10.75" bay behind the main spar, followed by another 10.25" bay before the
forward vertical member of the aft spar. Now that's 21" for the bays and
the vertical piece is 5/8" square (0.625") so the minimum distance between
the two should be 21.625", not 21.56" right. Upon further inspection there
should be a 1/32" gap between the main spar and the vertical member behind
it. Adding that to the total gives me 21.65625". I know its splitting
hairs, but it will change how much material comes off the aft spar. Has
anyone else noticed this, or did I just measure wrong?
