Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов, Страница: 161 / 923

Page 6-6
P/N 140-590032-0007
Revision A4: Sep, 2010
Section III Sub-section 6
FLIGHT CONTROLS
Pilot’s Operating Manual
RUDDER CONTROL SYSTEM (Figure 2)
The rudder is hinged from the rear of the vertical stabilizer and extends upwards from the rear cone of
the fuselage to just below the under-surface of the horizontal stabilizer.
Movement of the rudder pedals is transmitted by connecting rods and a bell crank to a pulley drum
under the flight compartment floor. Cables transmit the movement of the pulley drum to a quadrant
installed at the bottom of the rudder torque tube. A spring strut connected to the lower portion of the
rudder torque tube provides a centering force at the extreme travel. An autopilot servo motor is also
connected to the base of the torque tube.
Primary stops are located at the rudder lower hinge to determine the range of movement in both
directions. Secondary stops are located at each rudder pedal assembly.
Figure 2
Rudder Control System