The utility model belongs to the field of aircraft structure testing, and particularly relates to an oil supply feeler lever static test loading simulation piece which is used for a certain type of aircraft static simulation test. An aircraft oil-supply feeler lever and mounting structure static test needs to apply an oil-supply feeler lever load. By simulating the working state of the oil-supplyfeeler lever, the load of the oil-supply feeler lever is applied, and the strength of front and rear supports of the oil-supply feeler lever and a fuselage connecting area is assessed. The load of theoil-supply feeler lever is convenient to apply; the test installation workload and the test cost are reduced; according to the static test loading simulation piece for the oil supply feeler lever, athreaded connector connected with the oil supply feeler lever is arranged at one end of a frame body of the simulation piece, an axial loading connector is arranged at the other end of the frame body,and radial loading connectors distributed in the circumferential direction are arranged at the rod portion of the frame body. The loading simulation piece of the oil supply feeler lever is verified by static tests of the oil supply feeler lever and an installation structure of an airplane, and has the characteristics of low manufacturing cost, simplicity and convenience in installation and loading implementation and the like.