What is the maximum normal load factor for T-6?

The maximum normal load factor for the T-6 is defined as +4.0 to -2.0 G's. This value indicates the aircraft's ability to withstand forces during maneuvers, both positive and negative. The positive load factor, +4.0 G's, means the aircraft can experience forces equivalent to four times its weight during a pull-up or similar maneuver without structural failure. On the other hand, a negative load factor of -2.0 G's allows for some downward force but indicates the limits of what the aircraft can safely experience in terms of negative loading, such as during a push-over maneuver. These limits are crucial for pilots to understand, as they directly impact aircraft performance, safety, and the ability to execute various flight maneuvers while mitigating the risk of exceeding structural limits.

The other options present higher maximum load factors that are beyond what the T-6 is designed to handle within normal operational limits, potentially leading to structural failure or loss of control if those limits are exceeded. Understanding the appropriate load factors helps ensure safe and effective flying practices.