What is the altitude loss per turn during a near steady-state spin?

In a near steady-state spin, the aircraft experiences a loss of altitude due to the dynamics of the spin itself. During each turn in a spin, the aircraft is not producing lift effectively, and the combination of a high angle of attack and rotational movement leads to a loss of altitude as the aircraft descends through the air.

The measured altitude loss during a near steady-state spin typically falls within the range of 400 to 500 feet per turn. This loss is significant and emphasizes the importance of understanding spin recovery techniques and actions to regain control of the aircraft. The data supporting this altitude loss comes from both training protocols and observational data gathered during flight maneuvers.

Recognizing this specific range is crucial for pilots as it informs them about the risks associated with spinning and the rapid altitude loss that can occur, aiding them in making informed decisions about recovery procedures.