In view of the loading space fixed size of the traditional fuselage panel compression shear test-bed,a new generation fuselage panel compression and shear load test-bed was designed.It can adjust the loading space according to the length of fuselage panels,which is suitable for the compression load + shear load test of fuselage panels with different lengths.The design scheme of the test-bed was introduced,the key mechanism design method was proposed to realize the core function of the test-bed.Then the function of the test-bed was debugged.The function of key mechanism is normal,which can meet the use requirements.Using the test-bed to simulate the loading of the test dummy,the linearity of the loading process is good,which proves that the loading method of the test bench is reasonable.The uniformity of strain distribution of the test dummy is good,which proves that the accuracy of the test bench meets the requirements.