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· Operating Mode.
· Satellites Tracked.
RAIM and FOM indicate current uncertainty of position expressed in nautical miles. HDOP and
VDOP are numbers that rate current satellite geometry in the horizontal and vertical axis with 1
being the best geometry. Normally HDOP and VDOP numbers are below 10.
To view the GPS STATUS 2/2 on the FMS CDU, proceed as follows:
GF1710_178
1 Press NEXT function key.
NOTE
For more information, refer to the Flight Management System Pilot’s Guide.
GPS 1 STATUS 1/2
GPS POSITION
GRD SPD = 310 GPS ALT
MILES FR FMS POS
POS SENSORS PRED RAIM
N34 ° 02 . 6 W112 ° 02 . 3
N302 KT E68 KT 14999
NO . 1 W 4 . 4 TOTAL 4 . 4
GPS 1 STATUS 2/2
RAIM = 0 . 10 NM
POS SENSORS PRED RAIM
FOM = 0 . 05 NM
MODE = NAVIGATION
HDOP = 2 UTC 1730
VDOP = 2 DATE 20APR97
SATELLITES TRACKED = 7
NAVIGATION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
17−10−81
GPS SCHEMATIC
GF1710_179
GNSSU
ADC 1 ADC 2
FMS 1
FMS 3
IAC 1
IAC 2
IAC 3
GPWS
GPS
ANTENNA
FMS 1 FMS 2 FMS 3
(IF INSTALLED)
(IF INSTALLED)
FMS 2
NAVIGATION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
17−10−82
NAVIGATION SYSTEM EICAS MESSAGES
GF1710_180
FMS 1−2−3 FAIL
Indicates that respective
FMS has failed. GPWS SYSTEM FAIL
Indicates GPWS computer
has failed.
TERR FAIL
Indicates terrain alerting
function has failed.
WINDSHEAR FAIL
Indicates that
windshear alerting
function has failed.
GND PROX FAIL
Indicates that GPWS
is inoperative. GND
PROX FAIL will also
be annunciated when
the FLAP OVERRIDE
switch is OVRD and
IAS > 250 knots.
GPWS FLAP OVRD
Indicates that FLAP
OVRD switch has been
selected and flap aural
warning has been
muted.
GPWS G/S OVRD
Indicates that G/S
WARN switch has been
selected and glideslope
aural has been muted.
LSTRK FAIL
Indicates that Lasertrack
is inoperative, or has
been turned OFF.
FMS 1 FAIL
FMS 2 FAIL
FMS 3 FAIL
GPWS SYSTEM FAIL
GND PROX FAIL
LSTRK FAIL
TERR FAIL
WINDSHEAR FAIL
GPWS FLAP OVRD
GPWS G/S MUTED
NAVIGATION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
17−10−83
NAVIGATION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
17−10−84
THIS PAGE INTENTIONALLY LEFT BLANK
CB - NAV SYSTEM
GF1720_001
STAT SYS BUS PREV CNTL TEST
PAGE
NEXT
PAGE
EMER
CNTL
CIRCUIT BREAKER SYSTEM BUS
BRT
CIRCUIT BREAKER − SYSTEM 2/2
THRUST REV
OXYGEN
HYD
ICE
IND/RECORD
LDG GEAR
LIGHTS
OIL
NAV
DC ESS
CB − NAV SYSTEM 1/6
ADF 2
DME 1
FMS 1 CDU
FMS 2 CDU
ADF 1 IN
IN
IN
IN
IN
DC 1
DC ESS
DC 2
DME 2
BATT
DC 2
IN
DC 1
CB − NAV SYSTEM 2/6
GPS 1
GPS 2
HUD
IRS 1 FAN
FMS 3 CDU IN
IN
IN
IN
IN
DC 1
DC 1
DC 2
GPWS
DC 2
DC ESS
IN
IRS 3 PWR A
IRS 3 PWR B
LIGHTNING SENSOR
MFD 1 CTLR
MFD 2 CTLR
IN
IN
IN
IN
DC 1
DC ESS
DC 1
BATT
DC 2 IN
4/6
RAD ALT 2
STBY ADI
STBY ALT/ASI
TCAS
VOR/ILS 1
RAD ALT 1 IN
IN
IN
IN
IN
DC 1
DC 2
AV BATT
DC ESS
DC ESS
DC 2
CB − NAV SYSTEM
IN
5/6
DC 2
CB − NAV SYSTEM 3/6
IRS 1 PWR B
IRS 2 FAN
IRS 2 PWR B
IRS 3 FAN
IRS 1 PWR A IN
IN
IN
IN
IN
DC ESS
BATT
DC 2
IRS 2 PWR A
DC ESS
DC 1
IN
VOR/ILS 3 (OPT)
WX RADAR
WX RADAR CTLR 1
WX RADAR CTLR 2
VOR/ILS 2 IN
IN
IN
IN
IN
DC ESS
DC 1
DC 1
DC 1
DC 1
CB − NAV SYSTEM 6/6
CB − NAV SYSTEM
CCBP
NAVIGATION
EMS CIRCUIT PROTECTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
17−20−1
CB - NAV SYSTEM (CONT'D)
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