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Pilot’s Manual PM-132A 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) .......................................................... 5-2 Elevator ................................................................................................... 5-2 Elevator Disconnect.......................................................................... 5-3 Elevator Disconnect (Figure 5-2)................................................. 5-3 Rudder..................................................................................................... 5-4 Rudder Pedal Adjustment Switch.................................................. 5-4 Rudder Boost .......................................................................................... 5-5 Controls Gust Lock................................................................................ 5-6 Controls Gust Lock (Figure 5-3) ..................................................... 5-6 Flaps......................................................................................................... 5-7 Flap Control Lever............................................................................ 5-8 Flap Position Indication................................................................... 5-8 Spoiler Systems ...................................................................................... 5-9 Normal Spoiler Mode..................................................................... 5-10 Autospoilers .................................................................................... 5-10 Spoileron Operation ....................................................................... 5-11 Spoileron (Roll Disconnect Mode of Operation) ........................ 5-12 Spoiler Indications .......................................................................... 5-13 Spoiler Monitor System ................................................................. 5-14 Pitch Trim.............................................................................................. 5-15 Pitch Trim Selector Switch............................................................. 5-15 Primary Pitch Trim ......................................................................... 5-16 Trim Switch Panel (Figure 5-4) .................................................. 5-16 Bypass Trim.................................................................................. 5-17 Secondary Pitch Trim ..................................................................... 5-18 Autopilot Pitch Trim....................................................................... 5-19 Trim-In-Motion Indication............................................................. 5-19 Pitch Trim Bias................................................................................. 5-20 Configuration Trim......................................................................... 5-20 Aileron Trim.......................................................................................... 5-21 Rudder Trim ......................................................................................... 5-22 SECTION V FLIGHT CONTROL SYSTEMS & AVIONICS Pilot’s Manual V-2 PM-132A TABLE OF CONTENTS (Cont) 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 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：BOMBARDIER_Learjet_0-Flight_Controls_and_Avionics
