Aeroengine cable test system

The invention provides an aeroengine cable test system. The aeroengine cable test system comprises a liquid crystal display screen, a mouse and keyboard box, a printer, a controller, a digital multimeter, a chassis, a gathering area, a switch, mini sound equipment, a megger, a current matrix switch, a voltage matrix switch, a direct current power supply, an adapter socket, a power supply socket and a universal wheel. When a person carries out successive measurement, efficiency is low and intensity is high. By using the test system of the invention, the above disadvantages are effectively solved; under the condition that an engine is not disassembled, fault test and positioning are performed on an electrical line of the engine in a ground parking state; test efficiency and test precision are greatly increased; and a lot of manpower and time cost are saved. An enough large test capacity is possessed; through one-time wiring, all test projects can be completed, and simultaneously enough allowance is left for fur