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During an normal spin recovery:
  • A
    the control stick is moved side ways, against the angle of bank.
  • B
    the ailerons are held in the neutral position.
  • C
    the control stick is moved side ways, in the direction of the angle of bank.
  • D
    the control stick is pulled to the most aft position.
During a spin, the aircraft should be recovered by holding ailerons neutral and rudder in the opposite direction to the spin direction. When the aircraft has stopped spinning, angle of attack is to be increased (if sufficient airspeed is present) for minimum descent rate, level flight or climb (if possible).

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