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AUTO
XFER
OFF
GEN
1
AUTO
XFER
FAIL
APU
BUS 1
UTIL BUS 2
0
0
0
KVA
V
HZ
GEN
0
0
V
HZ
ADG
ESS BUS
15
115
400
KVA
V
HZ
0
0
0
KVA
V
HZ
BUS 2
AC ELECTRICAL
BRT BRT
Advisory EICAS
Messages
Oxygen
Pressure
Cabin
Altitude
Cabin Rate
Cabin Diff.
Spoiler
Deployment
Indication
L and R 10th-
Stage Bleed
Air Pressure
Fuel
Temperature
Flight Spoiler
Indicator
Indicates
relative spoiler
position
Ground Spoiler
Indicator
Cabin
Temperature
WING A/ICE OK
T/O CONFIG OK
L FUEL PUMP ON
R FUEL PUMP ON
HYD SOV1 CLSD
HYD SOV2 CLSD
PARKING BRAKE ON
AC UTIL 1 OFF
FUEL CH 1 FAIL
YD 1 INOP
CABIN TEMP
BLEED PRESS
FUEL TEMP
ENGINE
BULK
OXY
C ALT
RATE
P
50
20
50
40 30
-20
1850
200
0
SPOILERS -0.5
APU
95 430
RPM EGT
P604_03_007
FLIGHT CONTROLS
FLAPS 30
FLAPS MOTOR OVERHEAT
AIL AIL
RUDDER
YAW DAMPER
STAB TRIM CH1 INOP
ELEV ELEV
FLIGHT CONTROLS
DC ELECTRICAL
TRU 1
V
A
28
18
TRU 2
V
A
28
18
27
11
V
A
V
A
27
11
24
0
V
A
24
0
V
A
ESS
TRU 2
APU
BATT
MAIN
BATT
ESS
TRU 1
BUS 1
BUS 2
UTIL BUS 1
UTIL BUS 2
EMER BUS
APU BATT
DIR BUS
MAIN BATT
DIR BUS
AC BUS 1 AC BUS 2
AC ESS
BUS
CHGR OFF
TIE
ESS BUS
BATT BUS
DC ELECTRICAL
1B 3A 3B 2B
3050
PSI
3000
PSI
2950
PSI
INBD
BRAKES
3000 PSI
OUTBD
BRAKES
3000 PSI
80 °C 15 °C
RUDDER
L ELEVATOR
L AILERON
FLT SPLR
GND SPLR
RUDDER
L ELEVATOR R
L AILERON R
LNDG GEAR
N/W STEER
NOSE DOOR
RUDDER
ELEVATOR R
AILERON R
FLT SPLR
MLG AUX ACT
1A 2A
49%
HYDRAULIC
95 °C
82% 76%
HYDRAULIC
Status EICAS
Messages
APU RPM and
EGT Indicators
AURAL/VISUAL WARNING
For Training Purposes Only
May 03
3-13
P I LOT T R A I N I N G GU I D E
EICAS Status Page
The status page is the default display of ED 2.
Crew Alerting System Messages
Advisory and status messages are presented only on the EICAS status page.
Flight Spoilers
When deployed, the flight spoilers’ extension will be presented at the bottom left-hand
corner of the EICAS status page. When retracted, the display disappears.
Auxiliary Power Unit
The APU RPM and EGT gauges are displayed on the EICAS status page when the
APU PWR FUEL switch is selected.
Cabin Temperature
The cabin temperature is displayed in degrees Celsius.
Bleed Air Pressure
The bleed air pressure of the left and right 10th-stage manifold is indicated in pounds
per square inch (psi).
Fuel Temperature
The fuel temperatures at the engines and in the left main tank (bulk) is provided in
degrees Celsius.
Oxygen Pressure
The gaseous oxygen pressure is continuously displayed on the status page. Green
indicates normal pressure and amber identifies pressure below 800 psi.
Cabin Pressurization
Cabin pressurization is displayed on the status page. The information includes:
• cabin altitude in feet
• rate of climb or descent in feet/minute
• differential pressure in psi
AURAL/VISUAL WARNING
3-14 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
Synoptic Pages
Synoptic pages are normally displayed on ED 2. In cases of ED 2 failure or crew
preference, they can also be displayed on ED 1 or on a MFD.
The synoptic pages provide the pilot with real-time interpretation of aircraft hydraulic,
electrical and flight controls system operation. Color logic is used to depict normal,
precautionary and maximum system limit as follows:
• normal range, indication is green
• precautionary range, the system indicator turns amber
• exceeds the limits, the indicator turns red
Flow lines are used on a number of synoptic pages. Although not all pages will display
　
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