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• Fix entries
• Deselection of navaids
• Performance mode selection
• MAG/TRU display mode
• Thrust management
Parameters that are not synchronized include:
• FMC position initialization
• Selection of left/right sensors
When the FMSs are operated in INDEP mode, all parameters must be manually entered in each
FMS.
For additional information about SYNC/INDEP operation, see the “Collins FMS-6000 for the
Challenger 604” Pilot’s Guide.
NAVIGATION SYSTEMS
Description
Vol. 2 17−10−82
REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
FLIGHT MANAGEMENT SYSTEM (FMS) (CONT'D)
Controls and Indicators
FMS Tune Inhibit
The FMS may be inhibited from tuning the radios by selection of the FMS TUNE INHIB
switch/light, located on the reversionary/inhibit panel.
FMS TUNE INHIB Switch/Light
Figure 17−10−69
FMS 3 Reversionary Selector
FMS 3 may be selected using the FMS 3 reversionary selector switch on the center pedestal.
FMS 3 replaces FMS 1 or FMS 2 when the rotary selector switch is moved to the position 1 or 2
respectively.
FMS 3 Reversionary Selector
Figure 17−10−70
NAVIGATION SYSTEMS
Description
Vol. 2 17−10−83
REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
FLIGHT MANAGEMENT SYSTEM (FMS) (CONT'D)
FMS Message Displays
The FMS messages are displayed in several locations. Typically, a message remains displayed
as long as the condition that generated the message persists. For a complete description of
messages and message categories, see the “Collins FMS-6000 for the Challenger 604” Pilot’s
Guide.
CDU Messages
Messages may appear in the scratchpad, or in the message line immediately below the
scratchpad. Selection of the MSG function key cycles the CDU display to a dedicated message
page, where new and old messages may be reviewed.
CDU Message Display
Figure 17−10−71
NAVIGATION SYSTEMS
Description
Vol. 2 17−10−84
REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
FLIGHT MANAGEMENT SYSTEM (FMS) (CONT'D)
PFD Messages
FMS messages also appear on the PFD, immediately under the NAV SOURCE display (when
FMS is the NAV SOURCE). Additionally, certain PFD messages may be displayed in the
center of the HSI.
PFD Message Display
Figure 17−10−72
NAVIGATION SYSTEMS
Description
Vol. 2 17−10−85
REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
FLIGHT MANAGEMENT SYSTEM (FMS) (CONT'D)
MFD Messages
FMS messages may be displayed on the lower portion of the MFD display area.
MFD Message Display
Figure 17−10−73
FMS Color Conventions
The FMS color conventions are outlined in the following table. The EFIS FMS colors have been
included for reference only.
FMS Color Conventions Table
COLOR FMS CDU USE EFIS USE (REFERENCE ONLY)
RED Not used. Warnings.
YELLOW
Cautions usually requiring timely pilot
intervention.
Cautions.
GREEN
Active selections VNAV data on legs
page.
Safe/normal operation altitudes on map.
CYAN
Secondary information (e.g. from
waypoint, page titles, and route plan
legs).
Legends, pilot-selected values,
secondary map data.
MAGENTA Active leg (“to waypoint”).
“To waypoint”, fly-to-reference flight
director, airspeed bug, preselect altitude.
WHITE
Primary information (e.g. flight plan data,
down track waypoints, and FPLN and
legs ACT or MOD state).
Reference symbols, scale NAV MAP,
alternate source sensor, on-side FMS,
AFDS armed modes.
NAVIGATION SYSTEMS
Description
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REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
POWER SUPPLY AND CIRCUIT BREAKER SUMMARY
SYSTEM SUB-SYSTEM CB NAME BUS BAR
CB
PANEL
CB
LOCATION
NOTES
Navigation
Systems
Navigation Receiver
VHF NAV 1 DC ESS 4 D13
VHF NAV 2 DC BUS 2 2 H15
Distance Measuring
Equipment
DME 1 DC BUS 1 1 H12
DME 2 DC BUS 2 2 H12
Automatic Direction
Finder
ADF 1 DC ESS 4 D11
ADF 2 DC BUS 2 2 H13
Transponder
XPDR 1 DC ESS 4 D4
XPDR 2 DC BUS 2 2 H4
FMS
FMS CDU 1
DC BATT
1
M3 5387 and subs
& POST SB
604–24–002
FMS 1 BCK/UP
PWR
M2
　
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