You are correct about the lift differential associated with aileron, but I still disagree with you guys saying the right wing was stalled when the right tire never came off the ground, and also because of the fact that with full power and flaps, this airplane's stall deck angle is significantly higher than what is achieved in a 3-point or very slightly tail raised attitude. Could not have been stalled at such a low deck angle and AOA. The only way it could have reached critical AOA at this pitch attitude is if the airplane was descending, but of course the runway surface prevented this.