Recovery from a spin requires a pilot to use the flight controls to overcome the pro-spin moments resulting from aerodynamic and inertial forces involved in spins. # PARE method Most general aviation manufacturers recommend some variant of the "PARE" method to recover from a spin: - P - power idle - A - ailerons neutral - R - rudder opposite - E - elevator forward # Power [[Pitch and Power Coupling]] results in a nose-up pitching moment, deepening the stall and flattening the spin. # Ailerons In the case of normally directed flow over the wings, ailerons applied opposite the direction of the spin rotation will increase the effective camber of the inner (more stalled) wing, stalling it further and worsening the spin. ### Reversed flow in the case of reversed flow... # Rudder Opposite the direction of the spin to overcome yaw inertial forces # Elevator unstall bro # Additional Concerns NASA loading, moment of inertia, pic different article? blanketing: If the pilot attempts to resist this rolling moment with opposite aileron, wing loading and lift coefficient are increased on that wing, placing it at a higher angle of attack.