During spin recovery, which control input is applied opposite to the spin direction to reduce yaw?

• A. Rudder opposite
• B. Ailerons opposite
• C. Elevator down
• D. Power full

Answer: (A)

In a spin, the aircraft rotates around the vertical axis due to the stalled wing producing a sustained yaw and roll. To reduce that yaw and stop the rotation, apply the rudder in the direction opposite to the spin. This opposite rudder creates a counteracting yaw moment, slows the rotation, and lets the nose drop so the wings can regain lift and recovery can proceed. Using ailerons affects roll and can worsen the spin if misapplied, the elevator mainly changes pitch rather than yaw, and increasing power can sustain or deepen the spin. So the opposite rudder is the input that directly reduces yaw during spin recovery.