BOMBARDIER LEARJET 40 Pilot's Manual page 3

EICAS Display................................................................................. 5-45
Display Controllers......................................................................... 5-46
EICAS Display and BL-871 Bezel Controller
(Figure 5-11).............................................................................. 5-46
Display Controller (Figure 5-12) ............................................... 5-47
Display Unit Reversion Panels ..................................................... 5-48
Display Unit Reversion Panels (Figure 5-13) .......................... 5-48
Data Acquisition Units (DAUs) ......................................................... 5-49
Reversionary Control Panel (Figure 5-14) ................................... 5-49
Radio Management Units (RMUs) .................................................... 5-51
Radio Management Unit (Figure 5-15) ........................................ 5-51
RMU Cross-Side Operation........................................................... 5-52
RMU Backup Pages ........................................................................ 5-52
VHF Com Tuning............................................................................ 5-53
FMS Tuning...................................................................................... 5-54
NAV Tuning..................................................................................... 5-54
ADF Tuning ..................................................................................... 5-55
Transponder/TCAS Tuning .......................................................... 5-56
TCAS...................................................................................................... 5-56
TCAS Operation.............................................................................. 5-57
System Controls and Displays ...................................................... 5-58
Traffic Display Symbols ................................................................. 5-58
Enhanced Ground Position Warning System (EGPWS)................. 5-59
Audio Control System......................................................................... 5-60
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
PM-132A
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Pilot's Manual
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