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Aiming at the advanced performance and variety of a helicopter"s airborne electronic system and the lack of fast and effective detection means for field support, a small combined multi-function in-situ inspection equipment is designed. The equipment is mainly composed of PIP and PMA. The PIP is used to provide the excitation and measurement resources needed for in-situ detection. It is the main component of the in-situ detection device. The PMA controls the PIP through the network interface. It is the main human-computer interaction carrier of the PIP. By running the corresponding test program on the PMA. Complete fault detection of the onboard electronic system. For in-situ detection of different onboard electronic systems, it is only necessary to replace the corresponding resource module in the PIP host and run the corresponding test program in the PMA. The designed in-situ inspection equipment provides an effective detection method for the outfield protection of a helicopter, which can improve the maintenance efficiency of the field, reduce the maintenance cost of the whole electromechanical subsystem, and meet the requirements of rapid protection in the field environment.