What is the maximum negative G limit for the T-6A?

The maximum negative G limit for the T-6A is -1.5 Gs. This limit is established to ensure the structural integrity of the aircraft during maneuvering and to prevent excessive loads that could lead to structural failures. Operating outside this limit, especially at higher negative Gs, can result in adverse effects such as loss of control or the risk of overstressing and damaging the airframe. Understanding this limitation is crucial for pilots when performing maneuvers, particularly during aerobatics or any flight activities that involve sudden changes in load factors. Additionally, training and operational procedures are designed with these limits in mind to maintain safety and airworthiness during flight.