What is the asymmetrical load factor range for clean configuration in the T-6?

The asymmetrical load factor range for a clean configuration in the T-6 is critical for understanding the aircraft's structural integrity and performance capabilities during various maneuvers. In the clean configuration, which indicates that the aircraft is free of external stores or configuration changes that could affect drag and stability, the recommended load factor range is -1.0 to 4.7.

This range signifies the aircraft's ability to withstand a variety of forces during operations, such as during steep turns, pull-ups, or other high-stress flight situations without exceeding structural limits. The negative load factor indicates the aircraft’s capacity to handle loads during inverted flight or negative G maneuvers, whereas the positive load factor reflects how many times the gravitational force the aircraft can handle in positive maneuvers.

In contrast, the other ranges presented do not accurately represent the T-6’s operational limits for a clean configuration. Understanding this range is essential for safe and effective aircraft operation, especially in performance and aerobatic scenarios.