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situations. Indications
can be generated by the following:
· Crew alerting subsystem
within the Engine Indication and Crew Alerting System (EICAS).
· Enhanced Ground Proximity Warning System (EGPWS).
· Weather Radar (WX) system.
· Traffic alert and Collision Avoidance System (TCAS).
· Altitude alert portion of the Air Data Computer (ADC).
· Stick shaker portion of the Stall Protection System (SPS).
EICAS provides crew with the necessary displays for airplane engine control and monitoring, control
surface monitoring and all major subsystem
synoptic displays. During normal operation, the engine
and control surface information is displayed on the EICAS display unit (DU3) and the system
synoptic information is displayed on the SYSTEMS display (DU4).
GF0310_001
DU 1 DU 2 DU 3 DU 4 DU 5 DU 6
PFD 1 MFD 1 EICAS SYSTEMS MFD 2 PFD 2
VS 2000
TOC
3
KSRP
180
220
210
200
170
160
150
0.88
0.856 M
190
KPHX
WX SAT
GSPD
−56
TAT
TAS
−40
234
345
LX
HDG
330
ETE 1+36
KLAX
TOC KPHX
KDVT KSRP
4000 4000
FL180
FMS1
DTK
360
20
20
10
10
20
20
10
10
33
30
W
24
21 15
12
E
6
3
0
1
2
1
2
3
VAPP VNAV
HDG AP1 ASEL 10400
29.92 IN
H23.4NM
SRP
BARO
9500
10500
10000
HDG
330
3
12.5NM
KDVT
LUF
KDVT
1300 5
1000
N
5
360
S
N
TERR
OFF
30
6
33
185
6
4
TOTALFUEL(LBS) 41550
1.54 1.54
73.3 73.3
789 789
14600 10000 14600
2350 ND
STAB
NU
NL RUDDER
LWD
NR
TRIMS
7.2
N2
FF (PPH)
OIL TEMP
OIL PRESS
93.4
5750
115
81
93.4
5750
115
81
1.65 1.65
CRZ
EPR
SYNC
N1
ITT
OIL QTY (QTS)
ENG
APU
RES
RPM EGT
10.4
22
1300
85 %
0.00
20
100 400
4.5
5.0
10.4
CKPT (5C)
OXYGEN
CAB ALT
CAB RATE
P
FWD
APU
RWD
CABIN (5C)
AFT
CABIN (5C)
21
29
23
20
"1300
LDG ELEV 1000 TOC
3
KSRP
KPHX
WX SAT
GSPD
−56
TAT
TAS
−40
234
345
LX
HDG
330
ETE 1+36
KLAX
TOC KPHX
KDVT KSRP
4000 4000
FL180
12.5NM
KDVT
LUF
KDVT
5
N
5
360
TERR
OFF
30
6
33
VS 2000
180
220
210
200
170
160
150
0.88
0.856 M
190
FMS1
DTK
360
20
20
10
10
20
20
10
10
33
30
W
24
21 15
12
E
6
3
0
1
2
1
2
3
VAPP VNAV
HDG AP1 ASEL 10400
29.92 IN
H23.4NM
SRP
BARO
9500
10500
10000
HDG
330
3
1300
1000
S
N
185
6
4 0
1 2
13% 13 %
OPEN OPEN
OUTFLOW VALVES
EICAS provides display of:
· Primary engine parameters
· Fuel quantities
· Flaps/slats/spoilers positions
· Crew Alerting System (CAS) messages
· Secondary engine parameters
· Landing gear position
· Surface trim indication
SYSTEMS provides synoptics display of:
· Bleed/AntiIce
Air
· Hydraulics
· DC Electrical
· Flight Controls
· Air Conditioning
· AC Electrical
· Fuel
· Status
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
03−10−1
CENTRAL DISPLAY SYSTEM
The central display system provides crew with displays for aircraft control, navigation, engine control
and monitoring and systems synoptic. Other systems information provided for display are WX
display, TCAS, EGPWS and Lightning Sensor System (LSS) display.
Airplane data is transmitted from airplane systems to 4 dual channel, Data Acquisition Units (DAU),
　
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