A t support system for connecting a vertical stabilize surface to a fuselage of an aircraft is provided, includes two symmetrical sets of bar systems, each of said groups of bars comprises a front bars, middle-front bar system, middle and rear bar systems, the front bar system of the two sets of bar systems, middle-front bar system, The arrangement of the aft and middle members corresponds to thejoint of the vertical stabilizer of the aircraft, A link plate is arrange at that joint of each group of rods and the vertical stabilize surface of the aircraft, bolt holes for connecting with the joint of the vertical stabilizer surface of the aircraft are arrange on the connecting plate, and the front rods comprise a first joint, a first vertical rod, a first vertical fixed ear seat, a first lateral rod and a second lateral rod, wherein the front rods comprise a first joint, a first vertical rod, a first vertical fixed ear seat, and a second lateral rod. The invention simulates the connection constraint condition between the vertical stabilizer and the fuselage of the aircraft, tests the ultimate bearing capacity and the failure mode of the connection joint, and provides the test basis for the structural strength analysis and calculation, thereby reducing the risk of full-scale test.