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BUS 2 BUS 1 Bus powered Bus not powered _ Invalid data
UTIL BUS 1 UTIL BUS 2 Bus powered _ Bus not powered Invalid data
ESS BUS Bus powered Bus not powered _ Invalid data
BATT BUS Bus powered Bus not powered _ Invalid data
SERV BUS Bus powered Bus not powered _ Invalid data
APU BATT DIR BUS Battery 18 VDC or greater Battery less than 18 VDC _ Invalid data
MAIN BATT DIR BUS Battery 18 VDC or greater Battery less than 18 VDC _ Invalid data
EICAS BUS BAR OUTLINE GREEN WHITE AMBER HALF-
INTENSITY MAGENTA
APU BATT MAIN BATT Battery 18 VDC or greater External dc in use Battery less than 18 VDC Invalid data
V A
Always displayed between 18V & 32V. Less that 18V or greater than 32V. _ _
DC Emergency Bus <MST>
Figure 07---30---4
Flight Crew Operating Manual MASTER
CSP A-
013
ELECTRICAL DC Electrical System Vol. 1 07-
30-
8
REV 56, Jan 31/03
SERVICE CONFIGURATION (Amber)
Indicates that the DCSERVICE switch has been selectedON. Only theDC
Corresponds to DC AVAIL/INUSE switch/light.
SERVICE BUS
(Service Configuration)
Displayedwhenthe
DCService switch
is selectedON.
NOTE
Either the battery master switch or externalDC must be selectedON.
External DC Flow Line
Figure 07 ---30 ---5
Flight Crew Operating Manual MASTER
CSP A-
013
ELECTRICAL Vol. 1 07-
30-
9
DC Electrical System REV 56, Jan 31/03
E. DC Loads Distribution
DC BUS 1 (CBP-
1)
Spoiler Electronic Unit Spoiler Electronic Control System (PWR 1) Heaters, Static (R) and ADS Controller (R) Cockpit Temperature Control Left Windshield Heat Controller 14th-
Stage Bleed Air Isolation and Shutoff Valve (L) 10th-
Stage Bleed Air Isolation and Shutoff Valve (L) Anti-
ice Automatic NORM (1) Proximity Sensor (Landing Gear Control/Door 1) (Weight-
on-
wheels 1) Lights (cockpit floor, rear anti-
collision, wing inspection) Maintenance Diagnostic Computer DME 1 Radio Altimeter Flight Data Recorder Control Weather Radar (receiver, transmitter and control) EICAS Primary Display EICAS Secondary Display Left Lamp Driver Unit Bright/dim Power supply unit Data Loader Flap Control (CH 1) Nose Landing Lights Brake Temperature Monitor FMS (CDU 1) <0024><0050> DC Tie Control Bus 1 Feed Utility Bus 1 Feed DC 1 power Sensing TRU 1 Power Sensing AC Utility Bus Control 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)
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