When examining the earlier
SIM-X, it was observed that it had aerobatic characteristics, so the factory management decided to install a more powerful engine with a carburetor for inverted flights, reduce the lower wing struts, reduce the wing area and make the construction more flexible to give a more aerobatic aircraft. The renowned Yugoslav engineer
Sima Milutinović was consulted in 1937 to implement the necessary changes. The first test flight was by factory test pilot Captain Milan Bjelanović in January 1938. Starting 12 March 1938, tests were conducted by the
Yugoslav Royal Air Force. The plane got excellent grades and the YRAF bought the prototype SIM-XI. The SIM-XI was a monoplane with a single carbureted 150 hp
Siemens (Bram) Sh14a, engine. The plane was of mostly wooden structure, with an elliptical cross-section of fuselage made entirely of wood covered with plywood, and wooden wings covered with cloth, with rounded ends. On each side, the wings were supported by a pair of inclined struts attached to the fuselage. The aircraft had two fuel tanks, one located at the junction of the wings, the other in the fuselage. The fuselage tank was filled for aerobatics, and the wing tank was filled for normal flights. Both tanks were filled during flights when it was needed to travel greater distances. The landing gear was fixed, completely made of steel tubes, which were strong enough for the plane to be able to land on rugged terrain. ==Operational history==