Commercial Pilot License (CPL) 2025 – 400 Free Practice Questions to Pass the Exam

During a spin, the load factor of an airplane is slightly above 1G. This occurs because, during the rotation of the spin, the aircraft is subject to both the vertical lift and the centrifugal force acting outward due to the turning motion. The combination of these forces results in a greater load factor than what is typically experienced in straight and level flight.

When an aircraft is in a spin, it experiences increased aerodynamic forces that can lead to a higher load factor than the normal 1G experienced during level flight. This is influenced by various factors, including the aircraft’s speed and the angle of bank during the spin. The pilot must be aware of this increase because it affects the structural integrity of the aircraft and can lead to additional stresses on the airframe.

In summary, the load factor during a spin reflects the impact of both the lift generated and the centrifugal forces acting on the aircraft, resulting in a load factor that can be slightly above 1G.