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EICAS
The Engine Indication and Crew Alerting System is controlled through a Central
Display System that processes airplane data and information. This system monitors all
vital information and displays the appropriate indications to the flight crew.
EPGDS
The Electrical Power Generation and Distribution System monitors and controls the
airplane electrical system.
FADEC
The Full Authority Digital Engine Control System interfaces with the various airplane
systems to provide total control over the two engines through their entire operating
regime.
EFIS
The Electronic Flight Instrument System provides flight instrument and navigation
information to the crew through two primary flight displays (PFDs) and two multifunction
displays (MFDs).
For Training Purposes Only
Sept 04
1-33
P I LOT T R A I N I N G GU I D E
AIRPLANE GENERAL
FMQGC
The Fuel Management Quantity Gauging Computer continuously monitors the various
fuel parameters for quantities and distribution. This system provides proper fuel
scheduling and fuel balance during the entire flight. The fuel system computer also
alerts the flight crew should a fault occur in the system.
IAMS
The Integrated Air Management System controls and monitors the airplane bleed-air,
environmental, cabin pressurization and anti-ice systems.
FMS
The Flight Management System allows the flight crew to select and display airplane
navigation both laterally and vertically. The system can also provide automatic tuning
of navigation receivers and manual tuning of communication transceivers.
AFCS
The Automatic Flight Control System is an integrated autopilot, flight director and
yaw damper. The system also controls various airplane flight modes and provides
airplane guidance.
EFCS
The Electronic Flight Control System controls the airplane multi-function spoilers,
ground spoilers, horizontal stabilizer trim, as well as the pitch feel control and the
rudder travel-limit control.
CAIMS
The Central Aircraft Information Maintenance System is a modifiable, distributed
maintenance system. This system provides means for maintenance and flight crew to
view history of individual airplane system faults, run LRU tests, and display and
download real-time data.
1-34 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
AIRPLANE GENERAL
FLIGHT COMPARTMENT GENERAL ARRANGEMENT (Global Express shown)
WARNING
PRESSURE DIFFERENTIAL
SHALL NOT EXCEED .1 PSI
DURING TAXI AND 1.0 PSI
UPON INITIAL LANDING
OFF
ON
CABIN PWR
O
WINDSHIELD HEAT
L
ON
OFF/
RESET
R
ON
OFF/
RESET
ELECTRICAL
EXT AC
AVAIL
ON
FAIL
OFF
GEN 1
FAIL
OFF
EXT DC
AVAIL
ON
GEN 3 GEN 4
FAIL
OFF
GEN 2
FAIL
OFF
PUSH OFF/RESET
PUSH
OFF/RESET
APU GEN
FAIL
OFF
RAT GEN
ON
OFF
BATT MASTER
EMS
OFF
ON
ASTE
E
OF
HYDRAULIC
R HYD SOV
CLOSED
L HYD SOV
CLOSED
AURAL WARNING
PUSH TO MUTE
IAC 1 IAC 2
MUTED MUTED
PASS SIGNS
NO SMKG SEAT BLTS
OFF
ON
AUTO
OFF
ON
AUTO
EMER LIGHTS
OFF
ON
O
ARM
O
AU
O
AU
LANDING
L WING NLG R WING
TAXI/RECOG
WINGTIP
NAV BEACON STROBE WING INSP LOGO
OFF
ON
OFF
PULSE
STEADY
OFF
PULSE
STEADY
OFF
PULSE
STEADY
OFF
WINGTIP
OFF
WHT
ON
OFF
ON
OFF
ON
OFF
ON
O
EXTERNAL LIGHTS
O
O
O
O
O
ST
O
ON
O
ST
O
ST
HYDRAULIC
1B 3A 3B 2B
OFF
AUTO
OFF
ON ON ON
ON
OFF
AUTO
OFF
AUTO
O
AU
O
AU
O
O
AU
APU
RUN
OFF START
ENGINE
ENG START
IGNITION
ON
AUTO
L CRANK R CRANK
FUEL
R
WING FEED
INHIBIT
L
WING FEED
INHIBIT
XFEED SOV
FAIL
OPEN
AUX PUMP
OFF
PRI PUMPS
OFF
L RECIRC
ON
AUX PUMP
OFF
PRI PUMPS
OFF
R RECIRC
ON
AFT XFER
AUTO
OFF ON
OFF
AUTO
WING XFER PACK CONTROL
L MAN
TEMP
R MAN
TEMP
BLEED/AIR COND
TEMPERATURE
　
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本文鏈接地址：Bombardier Global AIRPLANE GENERAL(10)