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NAVIGATION SYSTEMS Table of Contents Vol. 2 17.00.1
Oct 05/06
CHAPTER 17 - NAVIGATION SYSTEMS
TABLE OF CONTENTS
Page
TABLE OF CONTENTS 17.00.1
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 17.00.2
Oct 05/06
Page
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
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本文链接地址:庞巴迪挑战者605公务机机组操作手册 CL605-CHAPTER 17 -导航系统 NAVIGATION SYSTEMS
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