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BATTERY BUS caution (amber)
Indicates that battery bus is not powered.
DC CROSS, MAIN or ESS TIE CLSD status (white)
Indicates that the corresponding bus tie is closed.
ESS TRU 2 XFER status (white)
Indicates that essential TRU 2 is powered
by AC essential bus.
Primary Page
Status Page
DC CROSS TIE CLSD
DC MAIN TIE CLSD
DC ESS TIE CLSD
ESS TRU 2 XFER
APU BATT CHGR
MAIN BATT CHGR
BRT
FLT. NO. CRJ
01 01 01 01
100 430
DOOR OPEN
APU
RPM EGT BRAKE TEMP
NU
10.3
OXY
CALT
RATE
P
LDG ELEV
C TEMP
1500
00
0.0
100
AIL
--TRIM--
STAB
LWD RWD
ND
NL NR
RUDDER
93.5 93.5
93.5 93.5
TO
N1
0 0.0
C ALT RATE P
GEAR
2200 1070 2200
FUEL QTY (KG)
TOTAL FUEL 5470
OIL PRESS
OIL TEMP
FF (KPH)
48
96
210
56
97
210
N2
ITT
600
91.0
600
90.2
DN DN DN
0
BRT
APU BATT OFF
MAIN BATT OFF
DC BUS 1
DC BUS 2
DC EMER BUS
DC ESS BUS
DC SERV BUS
BATTERY BUS
0.9
VIB
SLATS / FLAPS 20
FAN
0.9
Vol. 1 07--30--8
ELECTRICAL
DC Electrical System Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
Transformer Rectifire Unit Fail --- Status Page
Figure 07---30---6
ESS TRU 1 FAIL status (white)
Indicates that essential TRU 1 voltage
is < 18 volts with AC essential bus on line
or
essential tie is closed with essential
TRU 1 load < 3.7 amps.
TRU 1 FAIL status (white)
Indicates that TRU 1 voltage is
< 18 volts with AC bus 1 on line
or
main tie is closed with TRU 1 load
< 3.7 amps.
ESS TRU 2 FAIL status (white)
Indicates that essential TRU 2 voltage is
< 18 volts with AC bus 2 on line or essential
TRU 2 is powered by AC essential bus
or
essential tie is closed with essential
TRU 2 load < 3.7 amps.
TRU FAN FAIL status (white)
Indicates that any of 4 TRU fans have failed.
Status Page
TRU 2 FAIL status (white)
Indicates that TRU 2 voltage is
< 18 volts with AC bus 2 on line
or
main tie is closed with TRU 2 load
< 3.7 amps. BRT
01 01 01 01
100 430
DOOR OPEN
APU
RPM EGT BRAKE TEMP
TRU 1 FAIL
TRU 2 FAIL
ESS TRU 1 FAIL
ESS TRU 2 FAIL
TRU FAN FAIL
FLT. NO.
NU
10.3
CRJ
OXY
CALT
RATE
P
LDG ELEV
C TEMP
1500
0
0
0.0
100
AIL
--TRIM--
STAB
LWD RWD
ND
NL NR
RUDDER
Vol. 1 07--30--9
ELECTRICAL
DC Electrical System Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
D. DC Loads Distribution
DC BUS 1
Flight Recorder Control
EICAS Primary Display
EICAS Secondary Display
Left Lamp Driver Unit
EICAS Dimming
Data Loader
Left IAPS
Boarding Music
Passenger Door Actuator
ACPC Control 1
Baggage Compartment Control
Fan Monitor
Cabin Pressure Control 1
Cockpit Temperature Sensors
Aft Cabin Temperature Sensors
ACS Control 2 Channel A
Lavatory Smoke Detector
SSCU 1 Channel A
Pitch Feel 1
Radio Altimeter 1
Hydraulic Pump 2 and 3B
Control
Hydraulic System Fan Control
Hydraulic System 2 Indication
Anti-Ice Control Channel A
Left T2 Heater
Pilot Windshield Wiper
Left Windshield Heater Control
ADS Heater Control 2
Right Static Heaters
Brake Pressure Application
PSEU Channel A
Nose Wheel Steering
Anti-Skid
Left Cabin Reading Lights
Cockpit Dome Light
Taxi Lights
Nose Landing Lights
Cockpit Floor Lights
Rear Anti-Collision Lights
Wing Inspection Lights
Maintenance Lights
GPS 1
DME 1
Weather Radar
DC BUS 2
Right IAPS
Right AFCS
Right IAPS Fan
Observer Audio
VHF Communication 2
RTU 2
Service Bus Feed
ACPC Control 2
Left ACS Pressure Sensors
Cabin Pressure Control 2
Galley Heater Control
Fwd Cabin Temperature Sensors
ACS Control 1 Channel B
Right ACS Manual
SSCU 1 Channel B
Aileron and Rudder Trim
Clock 2
Radio Altimeter 2 <1045>
Air Data Computer 2
Primary Flight Director 2
Multifunctional Display 2
EFIS Control Panel 2
Attitude Heading 2
Right Fuel Pump and Control
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