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MEMO DISPLAY
OUTR TK FUEL XFRD appears in green, if at least one transfer ‐ valve is open in one wing tank.
‐ CTR TK FEEDG appears in green, if at least one center tank pump is energized.
‐ FUEL X FEED appears in green, if the fuel X FEED valve pushbutton is ON, and the X FEED
valve is not fully closed. It appears in amber in flight phases 3, 4, or 5.
‐ REFUELG appears in green, when the door of the refuel control panel on the fuselage is open.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
WARNINGS AND CAUTIONS
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FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
ELECTRICAL SUPPLY
A318/A319/A320/A321 FLEET DSC-28-40 P 1/2
FCOM 19 AUG 10
BUS EQUIPMENT LIST
Applicable to:
MSN,
NORM EMER ELEC
AC DC AC
ESS
DC
ESS HOT
CH 1 SHED (1)FQI CH 2 DC2 (1)
L 1 AC1 (3)DC1 X (2) (3)
L 2 AC2 DC2
R 1 AC1 (3)DC1 X (2) (3) INNER TANK PUMPS
R 2 AC2 DC2
CTR TK PUMPS �� 12 AACC12 DDCC12
CROSS FEED VALVE MMOOTT 12 DC2 SHED
ENG 1 MOT 1 X
ENG 1 MOT 2 DC2
ENGINE LP VALVES ENG 2 MOT 1 X
ENG 2 MOT 2 DC2
L1 SHED
L2 DC2
XFR VALVES R1 SHED
R2 DC2
PUMP
AC STAT
INV or AC
ESS SHED
APU HOT1
LP VALVE DC BAT HOT1
REFUEL VALVES DC2 (1)
(1) HOT BUS supplies power during refueling on battery.
(2) This occurs, if DC BUS 1 is lost.
(3) In smoke configuration (GEN 1 LINE pushbutton OFF), inner tank pumps 1 are supplied directly by IDG (instead of AC
1) and pump relays by DC ESS (instead of DC 1).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
ELECTRICAL SUPPLY
A318/A319/A320/A321 FLEET DSC-28-40 P 2/2
FCOM 19 AUG 10
BUS EQUIPMENT LIST
Applicable to: ,
, MSN,,
NORM EMER ELEC
AC DC AC
ESS
DC
ESS HOT
CH 1 SHED (1)FQI CH 2 DC2 (1)
L 1 AC1 (3)DC1 X (2) (3)
L 2 AC2 DC2
R 1 AC1 (3)DC1 X (2) (3)WING TANK PUMPS
R 2 AC2 DC2
CROSS FEED VALVE MMOOTT 12 DC2 SHED
ENG 1 MOT 1 X
ENG 1 MOT 2 DC2
ENGINE LP VALVES ENG 2 MOT 1 X
ENG 2 MOT 2 DC2
CTR TK XFR VALVES DC1
DC2
PUMP
AC STAT
INV or AC
ESS SHED
APU HOT1
LP VALVE DC BAT HOT1
REFUEL VALVES DC2 (1)
(1) HOT BUS supplies power during refueling on battery.
(2) This occurs, if DC BUS 1 is lost.
(3) In smoke configuration (GEN 1 LINE pushbutton OFF), wing tank pumps 1 are supplied directly by IDG (instead of AC
1) and pump relays by DC ESS (instead of DC 1).
AIRCRAFT SYSTEMS
HYDRAULIC
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A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
HYDRAULIC
PRELIMINARY PAGES - TABLE OF CONTENTS
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DSC-29-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
DSC-29-10 DESCRIPTION
DSC-29-10-10 GENERAL
GENERAL............................................................................................................................................................1/2
DSC-29-10-20 GENERATION
GREEN SYSTEM PUMP.................................................................................................................................... 1/8
BLUE SYSTEM PUMPS..................................................................................................................................... 1/8
YELLOW SYSTEM PUMPS................................................................................................................................1/8
POWER TRANSFER UNIT (PTU)........................................................................................................................1/8
RAM AIR TURBINE (RAT)................................................................................................................................. 2/8
SYSTEM ACCUMULATORS.............................................................................................................................. 2/8
LOAD ALLEVIATION FUNCTION (LAF) ACCUMULATORS............................................................................... 2/8
PRIORITY VALVES............................................................................................................................................ 2/8
FIRE SHUTOFF VALVES...................................................................................................................................2/8
　
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