The embodiment of the invention discloses a semi-physical test method and system for an aircraft avionics system. The system comprises: a test management subsystem for managing test projects, models and data through preset test management; a real-time simulation subsystem performing real-time simulation calculation on n aircraft avionics system and states of the subsystems of an aircraft; and a signal acquisition and output subsystem which is used for data interaction between a simulation system and real airborne equipment, wherein the airborne equipment is real airborne equipment, simulationexcitation equipment is avionics equipment operation environment simulation equipment, and the real-time simulation subsystem comprises an aerodynamic model, a kinetic model, an undercarriage model, amass characteristic model, a motion equation, an atmospheric data model, a GPS model and an inertial navigation model. According to the embodiment of the invention, through closed-loop crosslinking of testing environments of hardware system excitation, the real-time simulation system and the real airborne equipment, various effective ways are provided for the aircraft avionics system testing, andthe invention is close to an external field test.