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On the strength test of the aircraft Model FD-25 A. Ryotaro HIKIDA, Shun TAKEDA, Teruo ICHIKAWA, Tetsuo TANABE, Toshiharu BABA, Tokio HIYAMA, Kenjiro TOKUNO Abstract The aircraft Model FD-25 A is a trainer manufactured by the TOYO-KOKU-KOGYO Ltd., with the design of the Fletcher Aircraft Corp. To demonstrate the strength of this aircraft, the load was applied under a system of forces simulating as closely as possible those required in the regulation of C.A.A. of Japan. In this paper, the result of tests, the method of load calculation and the loading apparatus were reported and discussed.