Is it normal to have to take considerable material off the RV-7 QB wing rear spar tab to properly interface it to the same RV-7 QB fuselage?
I installed the wings initially using 7/16 bolts. When I clecoed in the wing root fairing in place the gap got considerably wider moving aft on the forward surface. Using the leading edge plumb bob technique described in the plans, the wings seemed to have a slight forward sweep.
I installed the wings initially using 7/16 bolts. When I clecoed in the wing root fairing in place the gap got considerably wider moving aft on the forward surface. Using the leading edge plumb bob technique described in the plans, the wings seemed to have a slight forward sweep.