The present invention relates to an aircraft hydraulic pump testing apparatus, and more particularly, to check whether the aircraft hydraulic pump operates normally by complexly checking the rotational speed of the aircraft hydraulic pump, the degree of load, and the flow rate of the supplied inspection oil. It relates to an aircraft hydraulic pump testing device. In addition, the main tank containing the inspection oil, a supply unit for supplying the inspection oil of the main tank to the aircraft hydraulic pump, and a load control valve that applies a load to the inspection oil discharged through the aircraft hydraulic pump through the supply unit at a preset pressure; It characterized in that it comprises a control unit for controlling the operation of the supply unit, the load control valve, an aircraft hydraulic pump.
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