The stall originates at the stall strips, which are about 30 inches outboard from the fuselage. I tested stall speed at forward and aft CG, in this case no difference, although usually there is about a one knot difference (slower at aft CG). This airplane has very benign stall characteristics, less than 5 deg of roll, and very little aileron input is needed to keep the wings level.
We measured incidence of wing and tail and everything is within type design tolerance.