Once the flaps have been retracted one stage to say F2, auto thrust would limit the aircraft speed to 195 kts (200 -5). As the VFE speed is approached, say around 190 kts, the flap handle is moved to 1+F and the auto thrust will continue to accelerate the aircraft to 210 kts (215 - 5).
The whole premise is wrong so what follows can't be right.