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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 605” Pilot’s
Guide.
NAVIGATION SYSTEMS
Description
Vol. 2 17−10−83
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
FLIGHT MANAGEMENT SYSTEM (FMS) (CONT'D)
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 17−10−78
PFD Messages
FMS messages also appear on the PFD (when FMS is the NAV SOURCE). Additionally,
certain PFD messages may be displayed on the navigation information section of the PFD.
NAVIGATION SYSTEMS
Description
Vol. 2 17−10−84
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
FLIGHT MANAGEMENT SYSTEM (FMS) (CONT'D)
PFD Message Display
Figure 17−10−79
MFD Messages
FMS messages may be displayed in the FMS NAV status field, located in the lower window of
the MFD display area.
NAVIGATION SYSTEMS
Description
Vol. 2 17−10−85
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
FLIGHT MANAGEMENT SYSTEM (FMS) (CONT'D)
MFD Message Display
Figure 17−10−80
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.
AMBER
Cautions usually requiring timely pilot
intervention.
Cautions, cross-side NAV source, and active
leg “to waypoint”.
GREEN
Active selections, VNAV data on LEGS page,
availability status.
Safe/normal operation altitudes on map.
CYAN
Secondary information (e.g. from waypoint,
page titles).
Legends, pilot-selected values, secondary
map data.
MAGENTA Active leg (“to waypoint”).
Fly-to-references, flight director, airspeed bug,
preselect altitude, on-side data, active leg “to
waypoint”.
WHITE
Primary information (e.g. flight plan data,
down track waypoints, and FPLN and LEGS
MOD state).
Reference symbols, scales, NAV map,
alternate-source sensor, on-side FMS, AFDS
armed modes.
NAVIGATION SYSTEMS
Description
Vol. 2 17−10−86
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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
Transponder XPDR 1 DC ESS 4 D4
XPDR 2 DC BUS 2 2 H4
FMS FMS CDU 1 DC BATT 1 M3
FMS CDU 2 DC BUS 2 2 H9
FMS CDU 3 DC ESS 4 D9
FMS DATA LOAD DC BUS 1 1 H10
GPS GPS 1 DC BATT 1 N3
GPS 2 DC BUS 2 2 H11
Inertial Reference
System
IRU 1 DC ESS 4 D11
IRU 1 SEC DC BATT 1 Q8
IRU 2 DC BUS 2 2 H10
IRU 2 SEC BATT BUS 1 Q9
IRU 3 DC BATT 1 H13
IRU 3 SEC DC BATT 1 Q10
Radio Altimeter RAD ALT 1 DC BUS 1 1 H14
RAD ALT 2 DC BUS 2 2 H14
Lightning Sensor LDS DC BUS 2 2 H6
Weather Radar WEATHER RDR
R/T
DC BUS 1 1 K1
Traffic Collision
Avoidance System
TCAS AC ESS 3 C5
Terrain Collision
Avoidance System
TAWS AC BUS 1 1 B13
NAVIGATION SYSTEMS
Summary
Vol. 2 17−20−1
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
NAVIGATION SYSTEMS
Summary
Vol. 2 17−20−2
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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