AC 61-67 C pertains to stalls and spins and states that if you enter a spin with flaps extended( down) to leave flaps in the extended position until rotation stops . For reference, I found this statement at the end of this AC. Question: Assume you enter a spin with flaps extended ( you forget to retract flaps at the onset of the spin due to being distracted) how would a airplane respond if you retracted the flaps during the developed phase of a spin? ( For those of you that respond, I am asking this question assuming the airplane is within the normal CG range and I realize that not all aircraft behave the same way during spins.) Thank you for the feedback.