The invention discloses an aircraft horizontal wing test bracket, which comprises- a lifting mechanism, a driving mechanism, a bracket mechanism and a moving mechanism, wherein the lifting mechanism is positioned above the moving mechanism, the bracket mechanism is positioned above the lifting mechanism, and the driving mechanism is arranged on the lifting mechanism and used for driving the bracket mechanism. As that span of the wing is long in the installation proces of the wing, As that problem of large volume, large weight, inconvenient and flexible movement and low precision of crane hoisting height fine-tune, the installation angle of the wing recovery installation is ensured, and the problems of up-down fine-tune of the wing hoisting and the structural and functional damage of the fuselage or the wing caused by the inertial collision of the wing with the fuselage are effectively solved.