The invention provides an integrated electronic injection/ignition system for an aviation fuel engine. The system structurally comprises a throttle valve assembly, an electric nozzle, a steering engine assembly, an air filter, a spark plug, a DD integrated circuit board and an oil supply system, wherein the throttle valve assembly comprises a throttle valve body, a throttle valve, a throttle valve shaft, a throttle valve return spring and a throttle pull bar, and the steering engine assembly comprises a steering engine, a steering engine rocking arm and a bulb pull bar; and the DD integrated circuit comprises an electronic control unit (ECU) and a capacitor discharge igniter (CDI). According to the invention, a miniaturized piston engine oil injection system is designed, the two major problems of mechanical spindle adjustment and low oil injection precision are avoided, a conventionally independent ignition system and an injection system are also integrated together, the structure is simplified, the space is saved, and redundancy design and self-check design also help to improve the flight safety and the maintenance efficiency.