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EICAS DISPLAY
FGF0310_001
TOTALFUEL(LBS) 41550
1.54 1.54
73.3 73.3
789 789
14600 10000 14600 ND
STAB
NU
NL RUDDER
LWD
NR
TRIMS
N2
FF (PPH)
OIL TEMP
OIL PRESS
93.4
5750
115
81
93.4
5750
115
81
EPR
N1
ITT
AIL
GEAR
OUT
30
DN DN DN
1.65 1.65
7.2
RWD
TOTALFUEL(LBS) 41550
1.54 1.54
73.3 73.3
789 789
14600 10000 14600 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
Crew Alerting System Window
14 message lines with Gear/Slats/Flaps
pop up displayed.
Slats/Flaps, Spoilers and Gear Position Pop Up
The pop up display will be removed from the
primary page (in flight only) 30 seconds after
the gear and flaps indicate up, ans no
predetermined malfunctions exist, or flight
spoilers out.
The pop up display will appear with flap selection
greater than zero degrees, gear selected down
and/or if any predetermined malfunctions exist.
Trims
Indications for Aileron, Rudder and Stabilizer Trim.
For more information see Chapter 10, FLIGHT
CONTROLS.
NOTE
EICAS will automatically be displayed when
airplane is powered up (BATT MASTER ON)
Crew Alerting System Window
24 message lines with Gear/Slats/Flaps
pop up not displayed.
Engine Indicating
Indications of EPR, N1, ITT, N2, FF,
OIL TEMP and OIL PRESSURE. For more
information see Chapter 18, POWER PLANT.
Fuel
Indications of total fuel quantity and
individual tank quantity. For more
information see Chapter 12, FUEL.
AURAL AND VISUAL WARNINGS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
03−10−26
SYSTEMS DISPLAY (STAT PAGE)
NOTE
SYSTEM display will automatically be displayed when airplane is powered up (BATT MASTER ON).
GF0310_026a
OIL QTY (QTS)
ENG
APU
RES
RPM EGT
BRAKE TEMP
10.4
90
13% 13%
100 400
03 03 03 03
4.5
5.0
10.4
OXYGEN
OPEN OPEN
OUTFLOW VALVES
0 0
1 2
1 2
2
APU
%
1
CKPT (°C) AFT
CABIN (°C) CABIN (°C)
FWD
20
1300
20 0.00
CAB ALT
CAB RATE
23 P
19 21 22
CKPT/CABIN Temperature
Indications of cockpit, cabin forward and
cabin aft temperature. For more information
CAB ALT, P and CAB RATE
Indications of cabin altitude, cabin differential
and cabin rate of climb. For more information
see Chapter 2, AIR CONDITIONING
AND PRESSURIZATION.
see Chapter 2, AIR CONDITIONING
AND PRESSURIZATION.
OXYGEN
Indications of oxygen
quantity. For more
information see
Chapter 8, EMERGENCY
EQUIPMENT.
OUTFLOW VALVES
Indications of outflow
valves position (manual
mode only). For more
information see Chapter 2,
AIR CONDITIONING
BRAKE TEMP
Indications of brake
temperatures. For more
information see
Chapter 15, LANDING
GEAR.
AND PRESSURIZATION.
OIL QTY
Indications of engine, APU
and reservoir oil quantity.
For more information see
Chapter 5, APU, and
Chapter 18, POWER
PLANT.
APU
Indications of APU door
position (failure mode
only), APU RPM and EGT.
For more information see
Chapter 5, AUXILIARY
POWER UNIT.
DOORS
Indications of passenger entry
door, overwing emergency exit
baggage door. For more
information see Chapter 1,
AIRPLANE GENERAL.
AURAL AND VISUAL WARNINGS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
03−10−27
REVERSION CONTROL PANEL
The reversion panel, located on the pedestal, can be used to revert the EICAS display to alternate
display units, to revert IRS and ADCs and to revert SGs.
GF0310_027
PFD1 and PFD2 Knobs
Used to revert PFD 1 and PFD 2
displays to alternate display units.
EICAS Knob
Used to revert EICAS display
to alternate display units.
IRS and ADC Knobs
Used to revert IRS and ADCs.
For more information see
Chapter 11, FLIGHT
INSTRUMENTS.
SG1, SG2, SG3, Knobs
Used to revert applicable symbol
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