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2/3
DU 6
FLOOR/EYE LTS
FMS 2 CDU
GALLEY FAN
MFD 2 CTLR
DAU 2 CH B IN
IN
IN
IN
IN
IN
CB − DC BUS 2, SPDA1
R FOOTWARMER
PBA BRT/DIM 2 B IN
IN
R NOSE LDG LT
RMU 2 PWR A
IN
IN
CB − DC BUS 2, SPDA1 3/3
GF0720_080
CIRCUIT BREAKER − SYSTEM 1/1
DC ESS
BATT
AC 3
AC 4
AC 1
AC 2 DC 2
DC 1
AC ESS AV BATT
DC EMER APU BATT
DC BUS 2 FEEDERS 1/1
CABIN FEED
SPDA1 FEED
ALL
SPDA2 FEED
SPDA3 FEED
SPDA4 FEED
ELECTRICAL
EMS CIRCUIT PROTECTION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
07−20−22
BUS KEY (CONT'D)
DC BUS 2 (Cont’d)
CB − DC BUS 2, SPDA2 1/3
DU 4 PWR B
FDR
FDR ACCELEROMETER
GEAR CTL B PWR 1
DAU 3 CH. B IN
IN
IN
IN
IN
2/3
HUMIDIFIER
HYD 2 PRESS XDCR
IIRS 2 PWR A
L BMC CH B
HF 1 TRANSCVR IN
IN
IN
IN
IN
CB − DC BUS 2, SPDA2
L PACK CTLR CH B IN
OIL TANK PRODE
TRANSPONDER 1
VHF COM 1
IN
IN
IN
CB − DC BUS 2, SPDA2 3/3
HF 1 COUPLER IN
DME 1 IN
VOR/ILS 1
IN
GF0720_081A
DC BUS 2 FEEDERS 1/1
CABIN FEED
SPDA1 FEED
ALL
SPDA2 FEED
SPDA3 FEED
SPDA4 FEED
NOTE
The OIL TANK PROBE power source is tied to the MAP LTS circuit breaker, therefore,
the OIL TANK PROBE circuit breaker is OUT for airplanes incorporating SB 700−79−005.
ELECTRICAL
EMS CIRCUIT PROTECTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
07−20−23
BUS KEY (CONT'D)
DC BUS 2 (Cont’d)
Effectivity:
· Airplanes 9002 thru 9122 not incorporating Service Bulletin:
· SB 700−24−045, AC and DC Power Distribution − Unit Change and Activation of Build 4
Electrical System.
CB − DC BUS 2, SPDA2 1/3
DU 4 PWR B
FDR
FDR ACCELEROMETER
GEAR CTL B PWR 1
DAU 3 CH. B IN
IN
IN
IN
IN
2/3
HUMIDIFIER
HYD 2 PRESS XDCR
IIRS 2 PWR A
L BMC CH B
HF 1 TRANSCVR IN
IN
IN
IN
IN
CB − DC BUS 2, SPDA2
L PACK CTLR CH B IN
TRANSPONDER 1
VHF COM 1
VOR/ILS 1
IN
IN
IN
CB − DC BUS 2, SPDA2 3/3
HF 1 COUPLER IN
DME 1 IN
GF0720_082
DC BUS 2 FEEDERS 1/1
CABIN FEED
SPDA1 FEED
ALL
SPDA2 FEED
SPDA3 FEED
SPDA4 FEED
ELECTRICAL
EMS CIRCUIT PROTECTION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
07−20−24
BUS KEY (CONT'D)
DC BUS 2 (Cont’d)
CB − DC BUS 2, SPDA3 1/2
AFT TANK R SOV O
IRS 2 FAN
L PACK DUCT HEAT
NAV LTS
AFT TANK R SOV C IN
IN
IN
IN
IN
2/2
RAD ALT 2
R PACK CTLR CH A IN
IN
CB − DC BUS 2, SPDA3
R BMC CH A IN
GPS 2 IN
GF0720_083 DC BUS 2
FEEDERS 1/1
CABIN FEED
SPDA1 FEED
ALL
SPDA2 FEED
SPDA3 FEED
SPDA4 FEED
ELECTRICAL
EMS CIRCUIT PROTECTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
07−20−25
BUS KEY (CONT'D)
DC BUS 2 (Cont’d)
Effectivity:
· Airplanes 9002 thru 9122 not incorporating Service Bulletin:
· SB 700−24−045, AC and DC Power Distribution − Unit Change and Activation of Build 4
Electrical System.
CB − DC BUS 2, SPDA3 1/2
AFT TANK R SOV O
IRS 2 FAN
L PACK DUCT HEAT
NAV LTS
AFT TANK R SOV C IN
IN
IN
IN
IN
2/2
RAD ALT 2
R PACK CTLR CH B IN
IN
CB − DC BUS 2, SPDA3
R BMC CH A IN
GPS 2 IN
NOTE
The EMS CDU indicates R PACK CTLR CH A is on DC BUS 1 and R PACK CTLR CH B is on
DC BUS 2, of SPDA #3. The EMS CDU should indicate R PACK CTLR CH A on DC BUS 2 and
R PACK CTLR CH B on DC BUS 1.
GF0720_084
DC BUS 2 FEEDERS 1/1
CABIN FEED
SPDA1 FEED
ALL
SPDA2 FEED
SPDA3 FEED
SPDA4 FEED
ELECTRICAL
EMS CIRCUIT PROTECTION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
07−20−26
BUS KEY (CONT'D)
DC BUS 2 (Cont’d)
CB − DC BUS 2, SPDA4 1/3
　
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