BOMBARDIER LEARJET 40 Pilot's Manual page 2

Pilot's Manual
Trim Indications................................................................................... 5-23
Pitch Trim Indications.................................................................... 5-23
Aileron Trim Indications ............................................................... 5-24
Rudder Trim Indications ............................................................... 5-24
Mach Trim............................................................................................. 5-25
Stall Warning System .......................................................................... 5-26
Stall Warning Indications .............................................................. 5-26
Stall Warning Operation................................................................ 5-27
Stall Vane Anti-Ice .......................................................................... 5-27
Stall System Test ............................................................................. 5-28
Angle of Attack Indicators (Optional)......................................... 5-29
Instrument Panel Layout and AOA Indicator Position
(Figure 5-5)................................................................................... 5-29
Avionics .................................................................................................... 5-30
Honeywell Primus 1000 Avionics System ....................................... 5-30
Electronic Flight Instrument System (EFIS)................................ 5-30
IC-600 Power Source ...................................................................... 5-31
Avionics Master Switches................................................................... 5-32
Electrical Control Panel (Figure 5-6)............................................ 5-32
Air Data System (ADS)....................................................................... 5-33
Pitot-Static System.......................................................................... 5-33
Pitot-Static System Schematic (Figure 5-7).............................. 5-33
Standby Pitot-Static System Schematic (Figure 5-8) .............. 5-34
Air Data Computers (ADCs) ........................................................ 5-35
ADC Reversion ............................................................................... 5-35
Standby Instruments........................................................................... 5-36
Standby Instrument Group (Figure 5-9) ..................................... 5-36
Standby Altimeter .......................................................................... 5-36
Standby Airspeed/Mach Indicator.............................................. 5-36
Standby Attitude Indicator ........................................................... 5-37
Standby Compass........................................................................... 5-37
Attitude Heading Reference System (AHRS).................................. 5-38
Attitude and Heading Comparison Monitors............................ 5-39
AHRU Power Source & Cooling .................................................. 5-40
AHRS Reversion............................................................................. 5-40
Electronic Display System (EDS) ...................................................... 5-41
Primary Flight Displays (PFDs) ................................................... 5-42
Primary Flight Display and Bezel Controller
(Figure 5-10)................................................................................. 5-43
Bezel Controllers............................................................................. 5-43
Multi-Function Display (MFD) .................................................... 5-44
V-2
TABLE OF CONTENTS (Cont)
PM-132A