庞巴迪挑战者605公务机机组操作手册 CL605-NAVIGATION_SYSTEMS.pdf94页

NAVIGATION SYSTEMS
Table of Contents

Vol. 2

17−00−1 Oct 05/06

CHAPTER 17 - NAVIGATION SYSTEMS
TABLE OF CONTENTS Page TABLE OF CONTENTS DESCRIPTION General Inertial Reference System (IRS) Description Alignment In-Flight Alignment IRS Reversionary Function (Dual IRS Configuration) IRS Reversionary Function (Triple IRS Configuration) EICAS Messages Weather Radar System Description Weather Radar Controls RADAR Modes Path Attenuation Correction (PAC) Alert Indication Target/Turbulence Alert Function Sector Scan Function Ground Clutter Suppression Function Gain Function Weather Radar Automatic Stabilization Lightning Detection System (LDS) (Optional) Terrain Awareness Warning System (TAWS) Description Components and Operation Controls and Indicators EICAS Messages VHF Navigation System Description Components and Operation VHF Navigation Indications Distance Measuring Equipment (DME) System Description Components and Operation Automatic Direction Finding System Description Components and Operation 17−10−1 17−10−1 17−10−1 17−10−1 17−10−2 17−10−3 17−10−4 17−10−5 17−10−5 17−10−5 17−10−5 17−10−8 17−10−11 17−10−12 17−10−13 17−10−13 17−10−13 17−10−13 17−10−13 17−10−14 17−10−14 17−10−16 17−10−30 17−10−32 17−10−34 17−10−34 17−10−34 17−10−42 17−10−48 17−10−48 17−10−48 17−10−51 17−10−51 17−10−51 17−00−1

CL−605 Flight Crew Operating Manual PSP 605−6


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