What is the symmetric clean acceleration limit for the T-6A?

The symmetric clean acceleration limit for the T-6A is 7.0 g. This limit indicates the maximum load factor that the aircraft can safely withstand during a clean configuration maneuver, which is performed when the flaps and landing gear are retracted.

Understanding the importance of this limit is crucial for pilots, as exceeding the maximum allowable load factor can lead to structural damage to the aircraft. The ability to perform maneuvers up to this limit allows pilots to execute a variety of flight operations while ensuring safety and integrity of the aircraft structure.

The other values do not represent the maximum symmetric clean acceleration limit, as they are lower and do not reflect the aircraft's design specifications for structural strength during maneuvers in a clean configuration. This knowledge is vital for ensuring safe and effective flight operations within the designed performance parameters of the T-6A.