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Mode 7 .......................................................................................................................17-01-26
Terrain Awareness Alerting ........................................................................................ 17-01-27
Terrain Clearance Floor (TCF)................................................................................... 17-01-29
Annunciations ............................................................................................................ 17-01-30
Weather Radar .................................................................................................................... 17-01-31
Description................................................................................................................. 17-01-31
Components and Operation....................................................................................... 17-01-31
Weather Radar Operational Modes ........................................................................... 17-01-31
Radar Antenna........................................................................................................... 17-01-32
REV 2
NAVIGATION
Table of Contents (Cont)
Volume 2 Flight Crew Operating Manual May 06/2005
17-00-02 CSP 100-6 REV 2
Flight Management System (FMS) ..................................................................................... 17-01-33
Description................................................................................................................. 17-01-33
Components and Operation....................................................................................... 17-01-34
Dead Reckoning (DR)................................................................................................ 17-01-34
FMS Calculated VSPEEDS .......................................................................................... 17-01-34
GPS Control............................................................................................................... 17-01-34
Global Positioning System (GPS) .............................................................................. 17-01-34
Predicted RAIM.......................................................................................................... 17-01-35
Required Navigation Performance (RNP).................................................................. 17-01-35
Satellite Deselect ....................................................................................................... 17-01-35
Controls and Indications...................................................................................................... 17-01-36
Navigation Components............................................................................................. 17-01-36
EICAS Messages ................................................................................................................ 17-01-37
NAVIGATION
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 17-01-01
INTRODUCTION
The Radio Navigation System contains the radios and controls used for navigation purposes. Included in these systems are
Terrain Awareness Warning System (TAWS), transponder, VHF navigation radios, weather radar, radio interface unit
(RIU), displays and controls with FMS, Radio Communication, GPS, and TCAS.
Two separate systems are provided for radio navigation. They are designed and installed so that the failure of one system
does not preclude the operation of the other system. Both are connected to the on-side and cross-side cockpit displays and
controls.
Equipment, controls and wiring are designed and installed so that the operation of any of the system components will not
adversely affect or will not be adversely affected by the simultaneous operation of any other radio or electronic unit
or system.
The Challenger 300 is equipped with conventional navigation systems as follows:
- Integrated Navigation Receivers
- Distance Measuring Equipment
- Automatic Direction Finder
RADIO INTERFACE UNIT (RIU)
The left and right Radio Interface Units are located on their respective equipment racks forward of the entry door.The RIUs
accommodate data concentration, communications and audio management, and control functions. The RIU provides an interface
between the radios and the rest of the aircraft systems and equipment. They receive inputs from TAWS and TCAS
and distribute digital audio signals from the audio control panels (ACPs).
REV 1
NAVIGATION
Volume 2 Flight Crew Operating Manual Sep 13/2004
17-01-02 CSP 100-6 REV 1
VHF NAVIGATION SYSTEM
DESCRIPTION
The standard VHF navigation system includes dual VOR/localizer receivers, dual glideslope receivers, dual marker beacons,
single distance measuring receiver (DME), and single automatic direction finder receiver (ADF). A second ADF and
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