What control movement is required for elevator input during spin recovery?

In spin recovery, the proper control movement for the elevator is to push forward and then pull back to recover. When an aircraft enters a spin, the ailerons are generally ineffective, and the first step in recovery is to reduce the angle of attack by pushing the yoke or control stick forward. This action helps to break the stall condition and allows the wings to regain effective airflow over their surfaces, facilitating a return to controlled flight.

Once the aircraft has stabilized and the rotation has ceased, pulling back on the control stick or yoke gradually will help to bring the aircraft back to a normal flight attitude without re-entering a stall or spin condition. This sequence of pushing forward followed by pulling back is crucial for effective recovery from a spin since it helps manage the aircraft's aerodynamic state by controlling the angle of attack and ensuring that airflow is re-established across the wings.