Full aircraft structure fatigue test, as a part of civil aircraft structure airworthiness verification test, is the most complicated, the most expensive and the most time-consuming. Improving the efficiency of full aircraft structure fatigue test and shortening the fatigue test cycle have always been pursued， especially for fatigue test management technique. This paper introduces concurrent engineering which is applied to full aircraft fatigue tests such as MA600, ARJ21-700, Y12F tests. The traditional serial working mode is transformed into the parallel working mode. Concurrent test management technique is summarized and proposed creatively. This paper describes the basic content and method of concurrent test management technique. It analyzes different requirements of the technique in different stages in a single test. At the same time it raises the management methods in multiple tests in the same factory. The practice shows that concurrent test management technique plays an important role in accelerating the cycle of full aircraft fatigue test. What’s more the technique is potential for further research and it has application prospects.