The present invention provides an airplane nose landing gear outer cylinder brace rod contact static test clamp. The clamp comprises a stand, an actuating cylinder, a connection module and an outer cylinder brace rod contact module, wherein the stand is a rectangular frame; the actuating cylinder is hung on a top beam of the stand; the connection module comprises a bilateral actuating cylinder connection support base being butted joint an actuating cylinder support base, a loading lever in bilateral hinging with the actuating cylinder connection support base, a connection support base having one end hinged with the loading lever and having the other end fixedly connected with a side beam of the stand, and a brace rod contact pulling-on piece having one end hinged with the middle position of the loading lever; and the outer cylinder brace rod contact module comprises a brace rod contact support base fixedly connected at a switching position of two beams of the stand, and an outer cylinder brace rod contact sleeving the brace rod contact support base through a pivot, wherein the outer cylinder brace rod contact hinged with the other end of the brace rod contact pulling-on piece through an binaural piece arranged on the outer cylinder brace rod contact. The test clamp can truly reflect a connection condition and a loaded state of a test piece on a landing gear and can bear a static force and fatigue test in large load.