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· Altitude (barometric/radio)
· Ground Speed
· Airspeed (MACH/KIAS)
· Vertical Speed
· Airspeed and Vertical Speed Trend
· True Airspeed
· Temperature Data
· Airplane Attitude
· Navigation Information
· Heading Information
Each primary flight display (PFD) and multifunction
display (MFD) receives altitude, heading,
airspeed and attitude data from the onside
sensors. Flight crew access to display format and display
controls is provided at PFD control panel, (located on the glareshield), the reversion control panel
and MFD control panel, (located on the pedestal).
PRIMARY FLIGHT DISPLAYS
MULTIFUNCTION DISPLAYS
Reversion Control Panel
PFD Control Panel
MFD Control Panel
ADC
GF1110_001
0.88
FMS1 SRP
23.4NM
BARO
3
6
E
12
15
21 S
24
W
30
33 N DTK
360
LIM
0.856M
0.88
FMS1 SRP
23.4NM
BARO
3
6
E
12
15
21 S
24
W
30
33 N DTK
360
LIM
0.856M
CKPT (°C) FWD
CABIN (°C)
AFT
CABIN (°C)
20
90
22
20
22
20
1300
0.00
500
OXYGEN
CAB ALT
P
20 CAB RATE
%
OIL QTY (QTS)
ENG
APU
RES
12.3
4.5
5.0
12.3
APU
RPM 100 EGT 650
BRAKE TEMP
04 05 04 04
TOTAL FUEL (LBS) 41550
1.54 1.54
73.3 73.3
789 789
14600 10000 14600
2350 ND
STAB
NU
NL RUDDER
LWD RWD
NR
TRIMS
7.2
N2
FF (PPH)
OIL TEMP
OIL PRESS
93.4
5750
115
81
93.4
5750
115
81
EPR
N1
ITT
AIL
1.65 1.65
CRZ
1
0
13 %
OPEN
13
OPEN
OUTFLOW VALVES
1 2 0
% 1 2
2
KPHX
4000
KDVT
50 50
KLAX
KPHX
FL180
KSRP
KDVT
4000
TOC SAT
TAT
ETE
TAS
NM
GSPD
KSRP
ET
TOC
KLAX
−56
−40
234
LX
345
00:10
WX
T5.0%
LUF
1+36
12.5
KDVT
TRU
N
FMS1
KPHX
4000
KDVT
50 50
KLAX
KPHX
FL180
KSRP
KDVT
4000
TOC SAT
TAT
ETE
TAS
NM
GSPD
KSRP
ET
TOC
KLAX
−56
−40
234
LX
345
00:10
WX
T5.0%
LUF
1+36
12.5
KDVT
TRU
N
FMS1
RAD BARO
MINIMUMS NAV SCR BARO SET
PUSH STD
IN HPa
NORM
ALTN
PFD1
NORM
ALTN1
EICAS
NORM
ALTN
PFD2
ALTN2
ALTN3
PFD1 PFD2
NORM
ALTN
SG1
NORM
ALTN
SG3
NORM
ALTN
SG2
IRS ADC ADC IRS
In the event of a PFD failure, the PFD format may be displayed on the adjacent MFD by actuation of
the reversionary mode switch (PFD1 or PFD2) on the reversion control panel. MFD format can also
be replaced by EICAS page and/or SYSTEMS page. For more information, see Chapter 3.
PFD format can be changed by actuation of HSI button on the PFD control panel. MFD format can be
changed by actuation of the MAP/PLAN button, MENU button and/or checklist buttons (NORM, ABN
and EMER) on the MFD control panel.
FLIGHT INSTRUMENTS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
11−10−1
EFIS NETWORK
EICAS CONTROLLER
MFD
CONTROLLER
REVERSION
CONTROLLER
TO IAC 1,2,3
IAC 1 IAC 3 IAC 2
WX RADAR
CONTROLLER 2
RX/TX ANTENNA
IRS MODE SELECTOR
NAVIGATION TO IRU 1,2,3
DISPLAY
UNIT
MFD
CONTROLLER
1
ADC 1 ADC 2
DAU 3 DAU 4 ADC 3
THROTTLE
QUADRANT
ASSEMBLY
SYSTEMS
AND
SENSORS
SYSTEMS
AND
SENSORS
YAW
DAMPERS
DAU 1 DAU 2
1 2
PFD
CONTROLLER
#1
PFD
CONTROLLER
#2
IRU 2
IRU 3
IRU 1
GUIDANCE PANEL
ELEVATOR
DUAL SERVO’S
AILERON
EGPWS
GF1110_002
2 FMS 1 FMS 2
WX RADAR
CONTROLLER 1
0.88
FMS1 SRP
23.4NM
BARO
3
6
E
12
15
21 S
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Bombardier_Global_000-Flight_Instruments(3)
