曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
N
START START
I
G
N
ND
STAB
1.54
1.65
73.3
T/O
N1
SYNC
73.3
789
ITT
SYNC
789
–TRIMS–
NL RUDDER NR
AIL
LWD RWD
7.2
NU
93.4
575O
115
81
23OO
L ENG FLAMEOUT
FUEL LO QTY
FUEL IMBALANCE
YD OFF
GLD MANUAL ARM
PARK/EMER BRAKE ON
<– FUEL XFER ON
TOTAL FUEL (LBS) 415OO
1.54
146OO 1OOOO 146OO
N2
FF (PPH)
OIL TEMP
OIL PRESS
93.4
575O
115
81
1.65
CRZ
EPR
I
G
N
START START
I
G
N
ND
STAB
1.54
1.65
73.3
T/O
N1
SYNC
73.3
789
ITT
SYNC
789 DN DN DN
OUT
3O
GEAR
–TRIMS–
NL RUDDER NR
AIL
LWD RWD
7.2
NU
93.4
575O
115
81
23OO
Crew Alerting System Window
14 message lines with Gear/Slats/Flaps popup
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 gear and
flaps indicate up, and no
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.
the
predetermined
TRIMS
Indications for Aileron, Rudder, and Stabilizer trim.
Crew Alerting System Window
24 message lines with Gear/Slats/Flaps
NOTE: Pop-up not displayed.
EICAS will automatically be displayed
when the airplane is powered up
(BATT MASTER ON).
Engine Indicating
Indications of EPR, N1, ITT, N2,
Fuel Flow, Oil temperature
and Pressure.
Fuel
Indications of total fuel quantity and
individual tank quantity.
GX_07_002
Aft tank not applicable to Global 5000
Aft tank not applicable to Global 5000
7-4 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
SYSTEMS SYNOPTICS
To view SYSTEMS synoptic displays, select the appropriate button on the EICAS
control panel.
STATUS PAGE
NOTE
STAT page will automatically be displayed when airplane is
powered up (BATT MASTER ON).
STAT
HYD
AC
ELEC
BLEED
AIR
COND
DC
ELEC
FUEL
FLT
CTRL
SCROLL
EICAS
SYSTEMS SELECT
NORM
MFD 1 MFD 2
CKPT/CABIN
Temperature
Indications of
cockpit, forward,
and Aft Cabin
selected (cyan)
and actual (green)
temperature.
OIL QTY
Indication of
engine, APU and
reservoir oil
quantity.
APU
Indication of APU
RPM and EGT.
Indication of APU
door position if
failed in other
than commanded
position.
DOORS
Indication of
passenger entry
door, overwing
emergency exit,
baggage door
and service
doors.
BRAKE TEMP
Indication of brake
temperatures.
OUTFLOW
VALVES
Indication of
outflow valves
position (manual
mode only).
OXYGEN
Indication of
oxygen quantity.
CAB ALT, P
and CAB RATE
Indications of
cabin altitude,
cabin differential
pressure and
cabin rate of
climb. Cabin rate
shown in manual
only.
GX_07_003
OIL QTY (QTS)
ENG
APU
RES
APU DOOR 11.2°
RPM EGT
BRAKE TEMP
12 . 3
1300
90%
13% 13%
0 . 00
100 650
03 06 03 03
12.3
5.2
3.2
20
19 20
22 22
20
CABIN (°C) CABIN (°C)
OXYGEN
CKPT (°C) AFT
OPEN OPEN
OUTFLOW VALVES
CAB ALT
CAB RATE
P
0 0
1 2
1 2
1 2
For Training Purposes Only
Sept 04
7-5
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
BLEED/ANTI-ICE SYNOPTIC PAGE
STAT
HYD
AC
ELEC
BLEED
AIR
COND
DC
ELEC
FUEL
FLT
CTRL
SCROLL
EICAS
SYSTEMS SELECT
NORM
MFD 1 MFD 2
GX_07_004
BLEED / ANTI-ICE
APU
LP
AIR
COND
HP
L
LP
HP 26
PSI
26
PSI
R
7-6 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
庞巴迪挑战者手册5(50)
