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Left Air Conditioning Unit
DME (1)
Smoke detector
Passenger signs
Overboard shutoff Valve
Pilots Wiper (motor and control)
Anti-Skid
GPS (1) <0027><0047>
Hydraulic System (AC pump
control 2 and 3B, fan control,
Indicator 2)
DC BUS 2 (CBP--2)
Horizontal Stabilizer Trim Control
Unit (CH 1)
Spoiler Electronic Unit (2A)
Spoiler Electronic Control
System (PWR 2)
Clock 2
Cabin Temperature Controller
and Manual Controller
Right Windshield and Window
Heater Controller
14th--Stage Bleed Air Isolation
and Shutoff Valve (R)
10th--Stage Bleed Air Isolation
and Shutoff Valve (R)
Anti--ice Automatic NORM (2)
Fuel Pump Control (R)
Proximity Sensor (Landing Gear
Control/Door 2)
(Weight--on--wheels 2)
Avionics Cooling (controller 2,
cockpit shutoff valve, overboard
shutoff valve
IAPS (AFCS) (right fan)
EFIS Control Panel 2
DCU 3 (CH A,B) <0019>.
Audio Control Panel (observers)
ADF 2
DME 2
VHF Nav radio 2
VHF Comm radio 2
PFD 2
MFD 2
RTU 2
Air Data Computer (2)
ATC Transponder 2
GPS 2 <0027>
Brake Pressure Indicator
Anti-Skid
Copilots Wiper (motor and
control)
Hydraulic System (AC pump
control 1 and 3A, Indicator 1)
DC Tie Control
Bus 2 Feed Tie and Utility
DC 2 power Sensing
TRU 1 Power Sensing
AC Utility Bus Control
Right Air Conditioning Unit
Flap Control (CH 2)
Nose Wheel Steering
Clock 2
Lights (copilot map and wing
anti--collision)
REV 56, Jan 31/03
Vol. 1 07--30--10
ELECTRICAL
DC Electrical System
Flight Crew Operating Manual MASTER
CSP A--013
DC ESSENTIAL BUS (CBP--4)
Horizontal Stabilizer Trim Control
Unit (CH--2)
Spoiler Electronic Unit (1A, 2B)
Spoiler Electronic Control
System 1--2 (PWR 3)
Heater, Static and ADS Heater
Control (L)
Cabin Pressure Controllers (1
and 2) and Control Panel
Left Window Heater Control
10th--stage Bleed air Isolation
Valve
Bleed Air Leak Test
Anti--ice Manual (L) STBY
Thrust Reverser (Auto, stow, 1
and 2)
Fuel (Transfer shutoff valve and
control)
Oil Pressure (R)
Passenger Door Control
Proximity Sensor (Landing Gear
Control)
Pilot’s Floodlights
Emergency Lights
EFIS, CRT, Dimming Panel 1
Avionic Cooling Controller (1)
Stall Protection (CH--R)
DCU 1 (CH A, B)
EFIS Panel 1
Audio Control Panel (copilot’s)
ADC 1
ADF 1
VHF Nav Radio (1)
Cockpit Voice Recorder
PFD 1
MFD 1
RTU 1
Clock 1
ATC Transponder 1
Head--up Guidance System
<0026>
IAPS (AFCS) (left fan)
BATTERY BUS (CBP--1) BATTERY BUS (CBP--2)
Passenger Oxygen (manual deploy and left
passengers)
Fuel System Control
Left Fuel Pump (Control and Power)
Fuel X--Feed Control
Left Engine oil Pressure
Passenger Address
Lights (Standby instrument and compass, map
dome,chart holder,overhead and copilot flood)
Fire Detector (A, B, Test)
Passenger Signs
EICAS/RTU Dimming
Stall Protection (stick pusher CH 1)
Audio Control Panel (pilot’s)
Air Data Computer(1 and 2) Alternate power
supply
VHF Comm Radio 1
Emergency Tuning Unit
IDG Disconnect (1 and 2)
Essential AC Transfer Control
GCU (1, 2 and 3)
DC Emergency bus Feed
Engine Ignition (A & B) Control
Engine Start (L and R)
Transfer/APU (manual x--flow, fuel pump,
controller, ECU)
Clock 1
Ram Air Shutoff Valve
CPAM
Crew Oxygen Monitor
Passenger Oxygen (auto deploy and right
passengers)
Anti--ice Valves (L and R manual 2)
Proximity Sensor (Landing Gear Control/Door 1
and 2) (Weight--on--wheels 1 and 2)
EICAS Control Panel
DCU 1 and 2 (CH A and B)
Standby Horizon Indicator
EICAS Display 1 (ED1)
EICAS Display 2 (ED2)
Lamp Driver Unit
Bright/Dim Power Supply Unit
Hyd System 3 (Gauges)
ADG Controller (auto and manual)
Essential TRU (power 1 and 2 sensing)
Feed 1 (battery and DC essential)
Feed 2 (battery and DC essential)
Battery Bus (power sensing)
RCCB Control (Main and APU battery)
FMS (CDU 2) <0024>
Overheat Detector (Main landing gear bay)
Vol. 1 07--30--11
REV 56, Jan 31/03
ELECTRICAL
DC Electrical System
Flight Crew Operating Manual
CSP A--013
MASTER
MAIN BATTERY DIRECT BUS
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航空翻译 www.aviation.cn
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Bombardier_CRJ_00-Electrical(10)
