CONTROL OF THE AEROPLANE

The aeroplane is equipped by dual stick control. Elevator and ailerons are controlled by a system of rods whereas the rudder is cable controlled. The wing flaps are controlled by the lever and rod and through the countershaft is threaded into aileron-flapperon circuit. Trim control is mounted as a standard. All engine controls are placed on the instrument board.

Rudder control - pedals of foot control are situated on the floor in front part of cockpit . Moving of pedals is transmitted on the rudder through steel cable.

Wing flaps - handle of wing flaps is situated in middle part of cockpit.