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时间:2010-05-17 21:43来源:蓝天飞行翻译 作者:admin
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CIRCUIT BREAKER SYSTEM
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
BRT
L ENG FUEL SOV
CB − FUEL SYSTEM 4/6
DC EMER DCPC
L FUEL RECIRC VLV DC 1
L FWD PRI PUMP AC 2
R AFT PRI PUMP AC 4
R AUX PUMP BATT
R CTR XFER PUMP AC 4
IN
IN
IN
IN
IN
IN
R ENG FUEL SOV
CB − FUEL SYSTEM 5/6
DC EMER DCPC
R FUEL RECIRC VLV DC 2
R FWD PRI PUMP AC 3
R/D MOTOR VALVES APU BATT ASCA
R/D PANEL COCKPIT APU BATT ASCA
R/D PANEL EXT APU BATT ASCA
IN
IN
IN
IN
IN
IN
XFER SOV C
CB − FUEL SYSTEM 1/6
DC ESS
XFER SOV O DC ESS
XFER SOV C BATT
XFER SOV O BATT
AFT TANK L PUMP AC 2
AFT TANK L SOV C DC 1
IN
IN
IN
IN
IN
IN
AFT TANK L SOV O
CB − FUEL SYSTEM 2/6
DC 1
AFT TANK R PUMP AC 3
AFT TANK R SOV C DC 2
AFT TANK R SOV O DC 2
APU FIRE SOV DC EMER DCPC
FUEL COMPUTR CH A BATT
IN
IN
IN
IN
IN
IN
FUEL COMPUTR CH B
CB − FUEL SYSTEM 3/6
DC ESS
FUEL R/D CH A APU BATT ASCA
FUEL R/D CH B APU BATT ASCA
L AFT PRI PUMP AC 1
L AUX PUMP DC ESS
L CTR XFER PUMP AC 1
IN
IN
IN
IN
IN
IN
R/D SOL VALVES
CB − FUEL SYSTEM 6/6
APU BATT ASCA
XFEED SOV C BATT
XFEED SOV O BATT
IN
IN
IN
FUEL
EMS CIRCUIT PROTECTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
12−20−1
CB - FUEL SYSTEM (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.
GF1220_002
STAT SYS BUS PREV CNTL TEST
PAGE
NEXT
PAGE
EMER
CNTL
BUS
CIRCUIT BREAKER − SYSTEM 1/2
CIRCUIT BREAKER SYSTEM
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
BRT
BATT
CB − FUEL SYSTEM 1/8
XFER SOV O
XFER SOV C
AFT TANK L PUMP
AFT TANK L SOV C
XFER SOV C IN
IN
IN
IN
IN
DC ESS
DC ESS
BATT
XFER SOV O
AC 2
DC 1
IN
AC 1
CB − FUEL SYSTEM 3/8
FUEL R/D CH A
FUEL R/D CH B
L AUX PUMP
L CTR XFER PUMP
FUEL COMPUTR CH B IN
IN
IN
IN
IN
DC ESS
APU BATT ASCA
APU BATT ASCA
L AFT PRI PUMP
DC ESS
AC 1
IN
DC 2
CB − FUEL SYSTEM 2/8
AFT TANK R PUMP
AFT TANK R SOV C
APU FIRE SOV
FUEL COMPUTR CH A
AFT TANK L SOV O IN
IN
IN
IN
IN
DC 1
AC 3
DC 2
AFT TANK R SOV O
DC EMER DCPC
BATT
IN
DC 1
L FWD PRI PUMP
L RECIRC SOV 1 C
L RECIRC SOV 2 C
L RECIRC SOV 2 O
L ENG FUEL SOV IN
IN
IN
IN
IN
DC EMER DCPC
AC 2
DC 1
L RECIRC SOV 1 O
DC 1
DC 1
IN
L RECIRC SOV 3 O
R AFT PRI PUMP
R AUX PUMP
R CTR XFER PUMP
R ENG FUEL SOV
L RECIRC SOV 3 C IN
IN
IN
IN
IN
DC 1
DC 1
AC 4
BATT
AC 4
DC EMER DCPC
CB − FUEL SYSTEM
IN
5/8
R RECIRC SOV 1 C
R RECIRC SOV 1 O
R RECIRC SOV 2 C
R RECIRC SOV 2 O
R RECIRC SOV 3 C
R FWD PRI PUMP IN
IN
IN
IN
IN
AC 3
DC 2
DC 2
DC 2
DC 2
DC 2
CB − FUEL SYSTEM
IN
6/8
R RECIRC SOV 3 O DC 2 IN
APU BATT ASCA
R/D MOTOR VALVES
R/D PANEL COCKPIT
R/D SOL VALVES
XFEED SOV C
IN
IN
IN
IN
APU BATT ASCA
APU BATT ASCA
R/D PANEL EXT
APU BATT ASCA
BATT
IN
XFEED SOV O BATT IN
CB − FUEL SYSTEM 8/8
CB − FUEL SYSTEM 4/8 CB − FUEL SYSTEM 7/8
FUEL
EMS CIRCUIT PROTECTION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
12−20−2
DESCRIPTION
General 13−10−1
System 1 and 2 13−10−1
System 3 13−10−1
Emergency Hydraulic Power 13−10−1
Hydraulic Accumulators 13−10−1
 
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