During an approach to a stall, an increased load factor will result in the airplane:

When an airplane experiences an increased load factor, it essentially means that the aircraft is subjected to greater aerodynamic forces due to factors such as bank angles or increased weight. This increased load factor raises the stall speed of the aircraft.

Stall speed is defined as the minimum speed at which the aircraft can maintain level flight without stalling. When the load factor increases, the wings must generate more lift to counteract the added weight from the increased load. Since lift is dependent on the square of the airspeed and the angle of attack, a greater load factor will result in requiring a higher airspeed to achieve the necessary lift.

As a result, the stall speed increases, meaning the airplane will stall at a higher airspeed when the load factor is elevated. Understanding this relationship is crucial for pilots, as it directly impacts their approach and recovery maneuvers, especially when conducting turns or maneuvers that increase the load on the aircraft.