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COMPONENTS AND OPERATION
The MFD control panel provides for the selection of the terrain (TR/WX) display on the respective MFD, while the DCP is used to display TR/WX on the PFD. Graphical terrain data is automatically displayed on the MFD when a terrain hazard is encountered. Each time the TAWS computer commands a terrain popup, the MFD automatically commands terrain over-lay to be added to the current format if the onside PFD is not displaying terrain and if the MFD format is compatible with terrain. The PFD commands the normal range to 10 NM. If the current MFD format is incompatible with terrain, the format will be changed to PPOS with TR selected, with a 10nm range. Regardless of the current format, selecting TR/WX will automatically select terrain for display. Similarly, selection of WX or WX/LX automatically deselects terrain.
Terrain range is selectable from the on-side DCP RANGE knob. with selected ranges up to 300 nm. If the display range is at a value greater than 300 nm when the pilot selects terrain, the display range will automatically reduce to 300 nm. On the Challenger 300, range can be selected up to 600 nm when in plan map format. If terrain data has been selected for display, selection of display ranges greater than 300 nm will be inhibited.
The TAWS WARN control panel, located on the center instrument panel, provides for the inhibiting of GS, FLAPS, aural warnings and TERRAIN.
-GS
-A TAWS GS WARN OFF status message is displayed when the switch is set to OFF. This switch is used by
the pilot to mute nuisance “glideslope” warnings. This switch is normally selected when a backcourse ap-
proach is conducted
-FLAPS
-A TAWS FLAPS OFF status message is displayed when the switch is set to OFF. This switch is used by the pilot to mute related GPWS warnings when a landing will be attempted with flaps not at 30 degrees
-TERRAIN
-A TAWS TERR OFF status message is displayed when the switch is set to OFF. This switch is used by the pilot to deselect the terrain function of the TAWS
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
17-01-13 TERRAIN AWARENESS WARNING SYSTEM (TAWS) (Cont) MFD CONTROL PANEL (MCP)
Illustration of the MFD is shown with the optional 3D Map Display switches (refer to Chapter 11-1-24 for further description).
DISPLAY CONTROL PANEL (DCP)
CFO1101002_007
TAWS WARN PANEL
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
17-01-14
TAWS modes are as follows:
MODE 1
EXCESSIVE DESCENT RATE
"SINKRATE"
"PULL UPI"
MODE 2
EXCESSIVE TERRAIN CLOSURE RATE "TERRAIN..TERRAIN" "PULL UPI"
SINK AFTER TAKEOFF "DON'T SINKI" MODE 3 TOO CLOSE TO TERRAIN "TOO LOW-TERRAIN" "TOO LOW-GEAR" MODE 4 "TOO LOW-FLAPS" EXCESSIVE DEVIATION BELOW GLIDESLOPE "GLIDESLOPE" MODE 5
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