FIELD: aviation; control systems and units for aircraft and its equipment. SUBSTANCE: proposed unit is provided with bracket having adjustable power stops; power control lever with handle is mounted on its axle; it is also provided with three-position mechanical switch and two microswitches connected with rudder trimmer electromechanism. Three-position mechanical switch is made in form of arm located on rear surface and mounted on leaf spring located in handle cavity; this arm is provided with two hold-down cams oriented into handle cavity and bearing projection on outer surface. EFFECT: extended functional capabilities of unit due to simultaneous control of engine power and rudder trimmer; enhanced human engineering. 3 dwg
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