The utility model provides an aircraft control
assembly rapid
troubleshooting test device, comprising a test host computer and a test circuit board, the test host computer sends a test control instruction to the test circuit board, and the test circuit board outputs a discrete
signal for the test of a to-be-tested device to the to-be-tested device after receiving the test control instruction. And after the to-be-tested device receives the test discrete
signal, test feedback information is transmitted to the test circuit board, and the test circuit board sends the test feedback information to the test upper computer, so that the test upper computer processes the test feedback information to judge whether the function of the to-be-tested device is normal or not. Compared with a traditional
test bench test method, the method has the advantages that functions which cannot be realized by a traditional
test bench can be realized by using existing
software and hardware, the time for completing the test of a single aircraft control
assembly is shorter, the
test efficiency is higher, a more efficient and effective
test program is realized, and the overall quality and reliability of the aircraft control
assembly are improved.