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Digital Audio Control Panel (Figure 5-16) .................................. 5-61
Clearance Delivery Radio (CDR)....................................................... 5-63
Clearance Delivery Radio (Figure 5-17) ...................................... 5-64
Flight Guidance Control System ....................................................... 5-65
Flight Director ................................................................................. 5-65
Flight Guidance Controller (FGC)................................................ 5-66
Flight Guidance Controller (Figure 5-18)................................. 5-66
Autopilot/Yaw Damper ................................................................ 5-69
AP/YD Annunciation .................................................................... 5-70
Control Wheel Trim Switch ........................................................... 5-70
Control Wheel Master Switch (MSW).......................................... 5-70
Touch Control Steering (TCS) ....................................................... 5-71
Autopilot Engagement/Disengagement..................................... 5-71
Yaw Damper Engagement/Disengagement............................... 5-72
Mistrim Annunciation.................................................................... 5-72
Power Supply Configuration........................................................ 5-72
Go-Around (GA) Button..................................................................... 5-73
Pilot’s Manual
V-4 PM-132A
TABLE OF CONTENTS (Cont)
Flight Management System (FMS).................................................... 5-73
Control Display Unit (CDU) ......................................................... 5-74
UNS-1E FMS CDU (Figure 5-19) .............................................. 5-74
Data Transfer Unit (DTU).............................................................. 5-75
Configuration Module................................................................... 5-75
FMS Functions ................................................................................ 5-75
Weather Radar ..................................................................................... 5-77
WU-660 Weather Radar Control Panel (Figure 5-20) ................ 5-77
Avionics Cooling ................................................................................. 5-78
Instrument Panel Cooling ............................................................. 5-78
Miscellaneous .......................................................................................... 5-79
Cockpit Voice Recorder (CVR) .......................................................... 5-79
Clocks.................................................................................................... 5-80
Multi-Function Chronometer and Instrument Location
(Figure 5-21)................................................................................. 5-80
Hourmeter-Airplane (Optional)........................................................ 5-81
Flight Data Recorder (FDR) (Optional) ............................................ 5-81
Emergency Locator Transmitter (Optional)..................................... 5-81
Dorne & Margolin ELT14 ................................................................... 5-81
Transmitter and Antenna .............................................................. 5-81
Transmitter Switch (ARM/OFF/ON) ......................................... 5-81
Remote Control and Monitor Unit............................................... 5-82
Operation......................................................................................... 5-82
ARTEX ELT 110-406............................................................................. 5-83
Transmitter and Antenna .............................................................. 5-83
Transmitter Switch (ON-OFF) ...................................................... 5-83
Cockpit Switch and Indicator Light............................................. 5-84
Buzzer .............................................................................................. 5-84
Operation......................................................................................... 5-84
Pilot’s Manual
PM-132A 5-1
FLIGHT CONTROL SYSTEMS
The primary flight controls (ailerons, elevator, and rudder) are mechanically
operated through the control columns, control wheels, and rudder
pedals. The flaps and spoilers are hydraulically actuated and
electronically controlled. Airplane trim systems (pitch, roll, and yaw)
are electronically controlled.
AILERON
The aileron control system consists mainly of three control circuits, one
in the fuselage area and one in each of the left and right wing area. In
　
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