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Figure 17−10−43 Audio and Display Control Panel 17−10−46
Figure 17−10−44 Flight Control Panel Course Knobs 17−10−46
Figure 17−10−45 PFD Navigation Display 17−10−47
Figure 17−10−46 MFD Navigation Display 17−10−48
Figure 17−10−47 PFD − VHF NAV − Failure Displays 17−10−49
Figure 17−10−48 MFD − VOR/DME Status Page 17−10−51
NAVIGATION SYSTEMS
Table of Contents
Vol. 2 17−00−3
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
Page
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 17−10−49 DME Controls (RTU/Audio Control Panel) 17−10−53
Figure 17−10−50 DME Displays (PFD/MFD) 17−10−54
Figure 17−10−51 ADF Bearing Display (PFD) 17−10−57
Figure 17−10−52 ADF Bearing Display (MFD) 17−10−58
Figure 17−10−53 ADF Controls (RTU/Audio Control Panel) 17−10−59
Figure 17−10−54 Transponder Controls (RTU) 17−10−61
Figure 17−10−55 Transponder Controls (Reversionary/Inhibit Panel) 17−10−61
Figure 17−10−56 TCAS MFD Traffic Symbology Display 17−10−63
Figure 17−10−57 Examples of TCAS Vertical Speed Advisories 17−10−65
Figure 17−10−58 TCAS Controls (RTU) 17−10−68
Figure 17−10−59 MFD TCAS Displays 17−10−69
Figure 17−10−60 Display Control Panel 17−10−69
Figure 17−10−61 PFD TCAS Display 17−10−70
Figure 17−10−62 TCAS Test PFD and MFD Indications 17−10−71
Figure 17−10−63 MFD LRN STATUS (Page 2/2) 17−10−74
Figure 17−10−64 PFD RAIM Indications 17−10−74
Figure 17−10−65 FMS CDU RAIM Message 17−10−75
Figure 17−10−66 FMS GPS Control Page 17−10−76
Figure 17−10−67 FMS Control Display Unit (CDU) 17−10−79
Figure 17−10−68 Data Base Unit 17−10−81
Figure 17−10−69 FMS TUNE INHIB Switch/Light 17−10−83
Figure 17−10−70 FMS 3 Reversionary Selector 17−10−83
Figure 17−10−71 CDU Message Display 17−10−84
Figure 17−10−72 PFD Message Display 17−10−85
Figure 17−10−73 MFD Message Display 17−10−86
NAVIGATION SYSTEMS
Table of Contents
Vol. 2 17−00−4
REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
Page
GENERAL
The navigation systems calculate and display the attitude, altitude and position of the aircraft, based
on data from other aircraft systems, ground stations, and sensed environmental conditions around
the aircraft. The displayed information includes aircraft movement, distance, speed and direction of
travel about all three axes. The present position and computed future positions can also be
displayed.
This chapter will cover:
• Independent position determining systems
• Dependent position determining systems, and
• Flight management system (FMS)
Refer to the “Collins Pro Line 4 Avionics System For The Challenger 604” Pilot’s Guide for additional
information.
Independent Position Determining Systems
Operating independently of ground installations or orbital satellites, the independent position
determining systems establish accurate aircraft location in three dimensions. They are comprised
of the following avionics systems:
• Inertial reference system (IRS)
• Weather radar system
• Enhanced ground proximity warning system (EGPWS)
Dependent Position Determining Systems
The dependent position determining systems use ground installations, aircraft transponders, or
orbital satellites to determine the location of the aircraft, and include the following avionics
systems:
• VHF navigation system
• Automatic direction finder (ADF) system
• Distance measuring equipment (DME) system
• ATC transponder
• Traffic alert and collision avoidance system (TCAS II)
• Global positioning system (GPS)
Flight Management Systems (FMS)
The FMS is a fully integrated navigation and flight data system providing:
• Cockpit management – NAV sensor control, secondary radio tuning, and MFD control
menus;
• Flight management – lateral point-to-point navigation, vertical navigation (VNAV), flight
　
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