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Hydraulic System 1 Indication
Hydraulic Pump 1 and 3A
Control
Right T2 Heater
Copilot Windshield Wiper
Right Windshield Heater Control
Right EFIS CRT Dimming
Right Window Heater Control
PSEU Channel B
Nose Wheel Steering
Brake Pressure Indication
Anti-Skid
Chart Holder Lights
Copilot Map Light
Wing Anti-Collision Lights
ADF 2
Transponder 2
VHF Navigation 2
DME 2
AHRS Fan 2
GPS 2 <1027>
EMERGENCY BUS SERVICE BUS UTILITY BUS
APU Battery Direct Bus Feed
FIREX
Engine and APU Fuel SOVs
Hydraulic SOVs
Service Lights
Boarding Lights
Navigation Lights
Toilet Lights
Galley Area Lights
Beacon Lights
Water System
Right Cabin Reading Lights
Vol. 1 07--30--10
ELECTRICAL
DC Electrical System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
ESSENTIAL BUS
EICAS DCU 1
RTU 1
Pilot Audio
Cockpit Voice Recorder
Door Indication 1 and 2
ACS Control 2 Channel B
Left ACS Manual
Display Fan Control
Right ACS Pressure Sensors
Flap and Slat Control Channel 1
SSCU 2
Pitch Feel 2 Rudder Travel Limit
Stall Protection Right Channel
Left EFIS CRT Dimming
EFIS Control Panel 1
Air Data Computer 1
Primary Flight Director 1
Multifunctional Display 1
Crossflow Pump Control
Fuel System Control
Left Static Heater
ADS Heater Control 1
ADS Standby Heater Control
Left Window Heater Control
Anti-Ice Control Channel B
Instrument Flood Lights
Emergency Lights
ADF 1
Transponder 1
VHF Navigation 1
Attitude Heading 1
AHRS Fan 1
Bleed Air SOVs
Thrust Reversers
Right Engine Oil Pressure
Left T2 Heater
BATTERY BUS
EICAS DCU 1 and 2
EICAS Primary Display
EICAS Secondary Display
EICAS Control Panel
Right Lamp Driver Unit
EICAS Dimming
Left AFCS
MDC
Left IAPS Fan
APU Control
APU ECU Primary
VHF Communication 1
Emergency Tuning
Pilot, Copilot and Observer Audio
Cabin Interphone
Passenger Address
Emergency Bus Feed
IDG Disconnect
Generator Control Units
ACPC Control 3
ADG Deployment
ACS Control 1 Channel A
Ram Air SOV
Manual Cabin Pressure Control
Passenger Oxygen Deployment
Crew Oxygen Monitor
Cargo Smoke Detection
Fire Detection
MLG Bay Overheat Detection
Flap and Slat Control Channel 2
Aileron and Rudder Trim Indication
Stall Protection Stick Pusher
Stall Protection Left Channel
Standby Instrument
Clock 1
Left Fuel Pump and Control
Fuel System Control
Right T2 Heater
Gravity Fuel Crossflow
Fuel Transfer SOVs
APU Fuel Pump
Hydraulic System 3 Indication
Cowl Anti-Ice Valves
Wing Anti-ice Isolation Valve
PSEU Channel A and B
Weight-On-Wheels
Passenger Signs
Wing Landing Lights
Map Lights
Cabin Utility Lights
Overhead Panel Lights
EICAS and RTU Dimming
Left Engine Oil Pressure
Engine Starting
FADEC
Engine Ignition B
MAIN BATTERY DIRECT BUS APU BATTERY DIRECT BUS
Main Battery Power Sensors
Main Battery Control
External AC Power
DCPC 2
Main Battery Charger Output
Clocks
Cockpit Dome Lights
APU ECU Secondary
APU Door Actuator
APU Battery Power Sensors
APU Battery Control
DCPC 1
External AC Power
Service Bus Feed
Emergency Bus Feed
Refuel/Defuel Control
Emergency Refuel
Engine Oil Indication
Engine Oil Replenishment
<1213>
Vol. 1 07--30--11
ELECTRICAL
DC Electrical System Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
E. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
TRU 1 AC BUS 1 B5
T f
ESS TRU 1 AC
1 T2
Transformer
Rectifier Units
ESS TRU 2B
ESSENTIAL T5
TRU 2
AC BUS 2 2
B5
ESS TRU 2A
C5
DC 1 FEED
DC BUS 1
D6
DC Bus 1 PWR SENS
1 D14
RCCB DC 1 D3
DC 2 FEED
DC BUS 2 2
L8
DC Bus 2 PWR SENS
L10
RCCB DC 2 1 D4
DC E ti l
DC ESS FEED DC
2
R6
Essential
Bus
PWR SENS
ESSENTIAL R11
RCCB DC ESS 1 D5
DC
EMER BUS
FEED
APU BATT
DIRECT BUS 5 A10
DC Electrical
Power
Emergency
Bus
EMER BUS
FEED
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