How does an aircraft respond during an accelerated stall in a steep turn?

In an accelerated stall during a steep turn, the correct understanding is that both wings stall at the same time. This phenomenon occurs because the aircraft is experiencing increased load factor and reduced airspeed as it maneuvers in a steep turn. When the angle of attack of the wings exceeds the critical angle during this higher load factor, the wings can reach the stall condition simultaneously.

In steep turns, the greater the bank angle, the more lift is required to maintain altitude. Consequently, pilots may inadvertently exceed the critical angle of attack for both wings, especially if they are not managing airspeed appropriately. This simultaneous stall can lead to a loss of control and uncoordinated flight, often resulting in a dramatic loss of altitude and an adverse yaw condition.

Understanding this behavior is crucial for pilots, as it emphasizes the importance of maintaining proper speed and control input during steep turns to avoid entering a stall condition.