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Penetration of the alert envelope activates the GND PROX lights and generates a TOO
LOW TERRAIN aural. The aural will occur once upon initial envelope penetration and
one time thereafter for each 20% degradation in altitude. The GND PROX lights remain
on until the aircraft exits the alert envelope.
Vol. 1 18--80--9
NAVIGATION SYSTEMS
Ground Proximity Warning System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Ground Proximity Warning System Terrain Display <2040>
Figure 18---80---4
TERRAIN DISPLAY FAIL (amber)
Terrain has been selected for display
and the required data is either failed,
missing, or invalid.
TERRAIN RANGE XXX NM (amber)
Terrain range disagrees with display
control panel range.
TAT --15 C
ADF 1
ADF 2
TERRAIN
CRS 350
CID
VOR1
UTC 11:42
TGT
30.0NM
TTG 1:59
270\30
FMS1 DTK 030
YUL 9999 NM
TTG :13
TAS 250 GS 254 SAT 12 C
200
30
33 N
3
ALO
CID
340
DBQ
100
TERRAIN DISPLAY FAIL
Vol. 1 18--80--10
NAVIGATION SYSTEMS
Ground Proximity Warning System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Ground Proximity Warning System Status Page <2040>
Figure 18---80---5
GS CANCEL status (white)
Indicates that glideslope Mode 5
alerts have been inhibited.
TERRAIN FAIL status (white)
Indicates a failure in the terrain
map display.
TERRAIN NOT AVAIL status (white)
Indicates that the terrain map display is
not available due to position inaccuracy.
GPWS FAIL status (white)
Indicates a failure in the basic
ground proximity warning modes.
TERRAIN OFF status (white)
Indicates that the terrain map display
has been selected and the terrain
functions have been inhibited.
WINDSHEAR FAIL status (white)
Indicates a failure in the windshear
detection system.
Status Page
Vol. 1 18--80--11
NAVIGATION SYSTEMS
Ground Proximity Warning System Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
J. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
Ground
Proximity
Warning
System
Computer GND PROX
WARN AC BUS 1 1 B14
Vol. 1 18--80--12
NAVIGATION SYSTEMS
Ground Proximity Warning System Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
THIS PAGE INTENTIONALLY LEFT BLANK
Vol. 1 18--90--1
NAVIGATION SYSTEMS
Weather Radar System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. WEATHER RADAR SYSTEM
The weather radar system provides the flight crew with a color-coded display of radar
detectable precipitation and ground mapping along the airplane’s flight path. System range
is up to 320 nautical miles and up to 60 degrees on either side of the airplane’s flight path.
The display control panel is used to select the weather radar format on the multifunctional
displays (MFDs). Weather radar data can also be overlaid in navaid sector, present position
map and TCAS modes. Control is provided using the weather radar control panel.
Vol. 1 18--90--2
NAVIGATION SYSTEMS
Weather Radar System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Weather Radar System <1025, 2040>
Figure 18---90---1
MODES
RANGE
FORMAT
RTA UNIT
MODES
RADAR CONTROL PANEL 1
DISPLAY
CONTROL PANEL 1
MULTI--
FUNCTION
DISPLAY 1
RADAR
VIDEO
REMOTE
ON/OFF
ATT
IAPS
BRT BRT
MODES
RANGE
FORMAT
MULTI--
FUNCTION
DISPLAY 2
DISPLAY
CONTROL PANEL 2
IRS 1 IRS 2
CB1--K2
DC BUS
1
WEATHER RADAR
CONT 1
CB1--K1
DC BUS
1
WEATHER
RADAR
R/T
Vol. 1 18--90--3
NAVIGATION SYSTEMS
Weather Radar System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Weather Radar System Control Panel
Figure 18---90---2
SEC XFR STAB
TILT
OFF
TEST
WX
MAP
GAIN
--1
--2
--3
+1
+2
+3
NORM
XFR
Used to transfer control of display range to
opposite side display control panel.
Controlling side range values are displayed
in white and non--controlling side values are
displayed in yellow.
Weather Radar Control Panel
Center Pedestal
STAB
Used to deselect radar stabilization
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