"SYNOPSIS: Wing spar manufacturing tolerances and the diameter of the F-1204M Rollers may misalign the wing and fuselage spar pin attach bushings. This may make insertion of the wing spar pins difficult. A reduction of the spar pin roller diameters will insure that worst case manufacturing tolerances will not inhibit insertion of the wing spar pins."
Anybody had issues with this? Have seen previous posts on difficulty inserting wing pins. Anybody tried the revised rollers and if so, did it have any measurable effect?