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Bombardier Learjet-Flight Control Systems and Avionics

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Pilot’s Manual PM-126A V-1 TABLE OF CONTENTS Flight Control Systems ............................................................................. 5-1 Aileron..................................................................................................... 5-1 Roll Disconnect ................................................................................. 5-1 Control Wheel ................................................................................... 5-2 Control Wheel (Figure 5-1) .....
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  Pilot’s Manual PM-126A V - 1 TABLE OF CONTENTS Flight Control Systems.............................................................................5-1Aileron.....................................................................................................5-1Roll Disconnect.................................................................................5-1Control Wheel...................................................................................5-2Control Wheel (Figure 5-1)..........................................................5-2Elevator...................................................................................................5-2Elevator Disconnect..........................................................................5-3Elevator Disconnect (Figure 5-2).................................................5-3Rudder.....................................................................................................5-4Rudder Pedal Adjustment Switches..............................................5-4Rudder Boost..........................................................................................5-5Controls Gust Lock................................................................................5-6Controls Gust Lock (Figure 5-3).....................................................5-6Flaps.........................................................................................................5-7Flap Control Lever............................................................................5-8Flap Position Indication...................................................................5-8Spoiler Systems......................................................................................5-9Normal Spoiler Mode.....................................................................5-10Autospoilers....................................................................................5-10Spoileron Operation.......................................................................5-11Spoileron (Roll Disconnect Mode of Operation)........................5-12Spoiler Indications..........................................................................5-13Spoiler Monitor System.................................................................5-14Pitch Trim..............................................................................................5-15Pitch Trim Selector Switch.............................................................5-15Primary Pitch Trim.........................................................................5-16Trim Switch Panel (Figure 5-4)..................................................5-16Bypass Trim..................................................................................5-17Secondary Pitch Trim.....................................................................5-18Autopilot Pitch Trim.......................................................................5-19Trim-In-Motion Indication.............................................................5-19Pitch Trim Bias.................................................................................5-20Configuration Trim.........................................................................5-20Aileron Trim..........................................................................................5-21Rudder Trim.........................................................................................5-22 SECTION V FLIGHT CONTROL SYSTEMS & AVIONICS   Pilot’s Manual V-2 PM-126A TABLE OF CONTENTS (Cont) Trim Indications...................................................................................5-23Pitch Trim Indications....................................................................5-23Aileron Trim Indications...............................................................5-24Rudder Trim Indications...............................................................5-24Mach Trim.............................................................................................5-25Stall Warning System..........................................................................5-26Stall Warning Indications..............................................................5-26Stall Warning Operation................................................................5-27Stall Vane Anti-Ice..........................................................................5-27Stall System Test.............................................................................5-28Angle of Attack Indicators (Optional).........................................5-29Instrument Panel Layout and AOA Indicator Position(Figure 5-5)...................................................................................5-29Avionics....................................................................................................5-30Honeywell Primus 1000 Avionics System.......................................5-30Electronic Flight Instrument System (EFIS)................................5-30IC-600 Power Source......................................................................5-31Avionics Master Switches...................................................................5-32Electrical Control Panel (Figure 5-6)............................................5-32Air Data System (ADS).......................................................................5-33Pitot-Static System..........................................................................5-33Pitot-Static System Schematic (Figure 5-7)..............................5-33Standby Pitot-Static System Schematic (Figure 5-8)..............5-34Air Data Computers (ADCs)........................................................5-35ADC Reversion...............................................................................5-35Standby Instruments...........................................................................5-36Standby Instrument Group (Figure 5-9).....................................5-36Standby Altimeter..........................................................................5-36Standby Airspeed/Mach Indicator..............................................5-36Standby Attitude Indicator...........................................................5-37Standby Compass...........................................................................5-37Attitude Heading Reference System (AHRS)..................................5-38Attitude and Heading Comparison Monitors............................5-39AHRU Power Source & Cooling..................................................5-40AHRS Reversion.............................................................................5-40Electronic Display System (EDS)......................................................5-41Primary Flight Display (PFD).......................................................5-42Primary Flight Display and Bezel Controller (Figure 5-10).................................................................................5-43Bezel Controllers.............................................................................5-43Multi-Function Display (MFD)....................................................5-44  Pilot’s Manual PM-126A V - 3 TABLE OF CONTENTS (Cont) EICAS Display.................................................................................5-45Display Controllers.........................................................................5-46EICAS Display and BL-871 Bezel Controller (Figure 5-11)..............................................................................5-46Display Controller (Figure 5-12)...............................................5-47Display Unit Reversion Panels.....................................................5-48Display Unit Reversion Panels (Figure 5-13)..........................5-48Data Acquisition Units (DAUs).........................................................5-49Reversionary Control Panel (Figure 5-14)...................................5-49Radio Management Units (RMUs)....................................................5-51Radio Management Unit (Figure 5-15)........................................5-51RMU Cross-Side Operation...........................................................5-52RMU Backup Pages........................................................................5-52VHF Com Tuning............................................................................5-53FMS Tuning......................................................................................5-54NAV Tuning.....................................................................................5-54ADF Tuning.....................................................................................5-55Transponder/TCAS Tuning..........................................................5-56TCAS (Optional)..................................................................................5-56TCAS Operation..............................................................................5-57System Controls and Displays......................................................5-58Traffic Display Symbols.................................................................5-58Enhanced Ground Proximity Warning System (EGPWS)..............5-59Audio Control System.........................................................................5-60Digital Audio Control Panel (Figure 5-16)..................................5-61Clearance Delivery Radio (CDR).......................................................5-63Clearance Delivery Radio (Figure 5-17)......................................5-64Flight Guidance Control System.......................................................5-65Flight Director.................................................................................5-65Flight Guidance Controller (FGC)................................................5-66Flight Guidance Controller (Figure 5-18).................................5-66Autopilot/Yaw Damper................................................................5-69AP/YD Annunciation....................................................................5-70Control Wheel Trim Switch...........................................................5-70Control Wheel Master Switch (MSW)..........................................5-70Touch Control Steering (TCS).......................................................5-71Autopilot Engagement/Disengagement.....................................5-71Yaw Damper Engagement/Disengagement...............................5-72Mistrim Annunciation....................................................................5-72Power Supply Configuration........................................................5-72Go-Around (GA) Button.....................................................................5-73  Pilot’s Manual V-4 PM-126A TABLE OF CONTENTS (Cont) Flight Management System (FMS)....................................................5-73Control Display Unit (CDU).........................................................5-74UNS-1E FMS CDU (Figure 5-19)..............................................5-74Data Transfer Unit (DTU)..............................................................5-75Configuration Module...................................................................5-75FMS Functions................................................................................5-75Weather Radar.....................................................................................5-77WU-650 Weather Radar Control Panel (Figure 5-20)................5-77Avionics Cooling.................................................................................5-78Instrument Panel Cooling.............................................................5-78Miscellaneous..........................................................................................5-79Cockpit Voice Recorder (CVR)..........................................................5-79Clocks....................................................................................................5-80Multi-Function Chronometer and Instrument Location (Figure 5-21).................................................................................5-80Hourmeter-Aircraft (Optional)..........................................................5-81Flight Data Recorder (FDR) (Optional)............................................5-81Emergency Locator Transmitter (Optional).....................................5-81Dorne & Margolin ELT14...................................................................5-81Transmitter and Antenna..............................................................5-81Transmitter Switch (ARM/OFF/ON).........................................5-81Remote Control and Monitor Unit...............................................5-82Operation.........................................................................................5-82ARTEX ELT 110-406.............................................................................5-83Transmitter and Antenna..............................................................5-83Transmitter Switch (ON-OFF)......................................................5-83Cockpit Switch and Indicator Light.............................................5-84Buzzer..............................................................................................5-84Operation.........................................................................................5-84

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Jul 30, 2017

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Jul 30, 2017
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