Troubleshoot Wing Rib Errors - Ribs 15-108 too high vs. tapered spar - spar taper was set-up correctly (but is wrong) - notches for stringer-1 were problematic and tipped me off to issue
Solution: - when wing geometry was corrected to extend LE & TE tapers to fuselage centerline (vs. going straight across fuselage from WS12.25 to opposite) - Rib 12.25 LENGTH was extended automatically to match the new planform - HOWEVER the height of the NACA 0016 airfoil at WS 12.25 was NOT recalculated for the new chord length - THUS Rib 12.25 is TOO LOW - Spar taper starts at WS12.25 & is TOO LOW as well - when Rib 12.25 is corrected, spar taper starting point will be raised and taper will be correct
