Jd Boggs, assuming you're still checking on this thread you started you need to stop and realize a few things.

1- the wing makes the lift it does from the airfoil, the size of the wing (area), the speed the wing is flying at and finally the angle of attack that the stabilizer and elevator hold it at.
2- in level flight at a steady speed the lift from the wing is exactly equal to the weight of the airplane. If it were even a fraction of a percent different the plane would either climb or descend. And even then the new speed caused by the climb or steady descent would then shift to where the lift of the wing was exactly equal to the weight of the airplane.
3- Where the wing gets called on to generate extra or less lift is during pitching maneuvers. Examples are looping or during banked turns. In those cases the need to accelerate the plane through some degree of pitch change causes a vector addition of the effects of centrifugal forces and gravity to increase the load on the wing and require that some excess lift above that needed to match the airplane's weight is required.

And as mentioned this has nothing to do with stability. At least not in as the term is used for describing an airplane in flight. Stability in aerodynamics refers to the degree that an airplane will try to return to some previous trim state when disturbed.