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DESCRIPTION General 17−10−1 Inertial Reference System (IRS) 17−10−1 Description 17−10−1 Alignment 17−10−1 In-Flight Alignment 17−10−2 IRS Reversionary Function (Dual IRS Configuration) 17−10−3 IRS Reversionary Function (Triple IRS Configuration) 17−10−4 EICAS Messages 17−10−5 Weather Radar System 17−10−5 Description 17−10−5 Weather Radar Controls 17−10−5 RADAR Modes 17−10−8 Path Attenuation Correction (PAC) Alert Indication 17−10−11 Target/Turbulence Alert Function 17−10−12 Sector Scan Function 17−10−13 Ground Clutter Suppression Function 17−10−13 Gain Function 17−10−13 Weather Radar Automatic Stabilization 17−10−13 Lightning Detection System (LDS) (Optional) 17−10−13 Terrain Awareness Warning System (TAWS) 17−10−14 Description 17−10−14 Components and Operation 17−10−16 Controls and Indicators 17−10−30 EICAS Messages 17−10−32 VHF Navigation System 17−10−34 Description 17−10−34 Components and Operation 17−10−34 VHF Navigation Indications 17−10−42 Distance Measuring Equipment (DME) System 17−10−48 Description 17−10−48 Components and Operation 17−10−48 Automatic Direction Finding System 17−10−51 Description 17−10−51 Components and Operation 17−10−51 NAVIGATION SYSTEMS Table of Contents Vol. 2 17−00−1 Oct 05/06 CHAPTER 17 - NAVIGATION SYSTEMS 17−00−1 CL−605 Flight Crew Operating Manual PSP 605−6 TABLE OF CONTENTS Page TABLE OF CONTENTS DESCRIPTION Air Traffic Control (ATC) Transponder System 17−10−56 Description 17−10−56 Components and Operation 17−10−56 Traffic Alert and Collision Avoidance System (TCAS) 17−10−62 Description 17−10−62 TCAS Controls 17−10−63 TCAS Traffic Symbology 17−10−66 TCAS Resolution Advisory (RA) Inhibits 17−10−71 Self-Test 17−10−71 Global Positioning System (GPS) 17−10−72 Description 17−10−72 Components and Operation 17−10−73 Controls and Indicators 17−10−77 Flight Management System (FMS) 17−10−78 Description 17−10−78 Components and Operation 17−10−79 Controls and Indicators 17−10−82 SUMMARY Power Supply and Circuit Breaker Summary 17−20−1 LIST OF ILLUSTRATIONS DESCRIPTION Figure 17−10−1 PFD IRS Aligning Annunciations 17−10−3 Figure 17−10−2 IRS Reversionary Annunciation (Dual IRS Configuration) 17−10−3 Figure 17−10−3 IRS Reversionary Annunciation (Triple IRS Configuration) 17−10−4 Figure 17−10−4 Display Control Panel (DCP) − Weather Radar Controls 17−10−6 Figure 17−10−5 DCP & CCP TR/WX Direct Access Pushbuttons Menu 17−10−6 Figure 17−10−6 PFD Weather Radar Menu 17−10−7 Figure 17−10−7 Weather Radar Test Display 17−10−9 Figure 17−10−8 Weather Radar Display Levels 17−10−10 Figure 17−10−9 Weather Radar Operational Modes 17−10−11 Figure 17−10−10 Weather Radar PAC Alert 17−10−12 Figure 17−10−11 TAWS Functional Schematic 17−10−15 Figure 17−10−12 TAWS Mode 1 17−10−16 Figure 17−10−13 TAWS Mode 2A 17−10−17 NAVIGATION SYSTEMS Table of Contents Vol. 2 17−00−2 Oct 05/06 CL−605 Flight Crew Operating Manual PSP 605−6 Page LIST OF ILLUSTRATIONS DESCRIPTION Figure 17−10−14 TAWS Mode 2B 17−10−17 Figure 17−10−15 TAWS Mode 3 17−10−18 Figure 17−10−16 TAWS Mode 4A 17−10−19 Figure 17−10−17 TAWS Mode 4B 17−10−19 Figure 17−10−18 TAWS WARNING Panel & Locator 17−10−20 Figure 17−10−19 TAWS Mode 4C 17−10−20 Figure 17−10−20 TAWS Mode 5 17−10−21 Figure 17−10−21 TAWS WARNING Panel 17−10−22 Figure 17−10−22 TAWS Mode 6 Bank Angle 17−10−23 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：庞巴迪挑战者605机组操作手册 CL605-NAVIGATION_SYSTEMS
