![]() Inertia of the propeller group has been specified. Engine altitude and max aircraft altitude have been refined (reduced). The radiator flaps on the automatic control mode supports now the temperatures on the normal operating mode better. The dependence of the engine cooling on speed has been configured. Critical angles and lifting force reducing throughout the entire speed range according to wing blowing has been implemented. ![]() By prolonged braking there is now the possibility of nosing over. Contact with the ground point of the fuselage has been recalculated. The rudder operation at low speeds has been clarified (improved), damping at the course has been increased.
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