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PRI PUMPS OFF
L PRI PUMPS OFF
L AUX PUMP OFF
R AUX PUMP OFF
XFEED VALVE OPEN
WING FUEL XFER OFF
APU FUEL SOV CLSD
L ENG SOV CLSD
L FUEL RECIRC OFF
−> FUEL XFER ON
<− FUEL XFER ON
R ENG SOV CLSD
R FUEL RECIRC OFF
FUEL
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
12−10−33
FUEL
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
12−10−34
THIS PAGE INTENTIONALLY LEFT BLANK
CB - FUEL SYSTEM
FGF1220_001
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
CB − FUEL SYSTEM 4/5
R ENG FUEL SOV
CB − FUEL SYSTEM 5/5
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 1/5
DC ESS
XFER SOV O DC ESS
XFER SOV C BATT
XFER SOV O BATT
IN
IN
IN
IN
CB − FUEL SYSTEM 2/5
APU FIRE SOV DC EMER DCPC
FUEL COMPUTR CH A BATT
IN
IN
FUEL COMPUTR CH B
CB − FUEL SYSTEM 3/5
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 APU BATT ASCA
XFEED SOV C BATT
XFEED SOV O BATT
IN
IN
IN
L ENG FUEL SOV 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
NOTE
The fuel recirculation protection is not
active, TBD by flight test.
FUEL
EMS CIRCUIT PROTECTION
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
12−20−1
FUEL
EMS CIRCUIT PROTECTION
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
12−20−2
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