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A330/A340 FLEET DSC-28-40 P 1/4
FCOM 19 AUG 10
BUS EQUIPMENT LIST
Applicable to:
L3
NORM EMER ELEC
AC DC DC
BAT
AC
ESS
DC
ESS HOT
1 LeveMl Saeinnsing SSHHEEDD
Main DC2 X (1) FCMC
2 Level Sensing SHED
1 X (3)X
2 AC1-2 DC1
3 AC2-3 DC2
4 AC2-4 DC2
STBY 1 AC2-3 DC2
STBY 2 AC2-4 DC2
STBY 3 AC1-2 DC1
INNER TANK PUMPS
STBY 4 DC1 (2)X (3)X (2)
TRIM TK FWD XFR PUMP AC2-3 DC2
CTR TK 1 AC1-2 DC1
TRANSFER PUMPS 2 AC2-3 DC2
CROSS FEED MOTOR 1 X
VALVES MOTOR 2 DC2
ENGINE LP VALVES MMOOTTOORR 12 DC2 X
AFT XFR VALVES RLHH DDCC12
TRIM TK ISOL VALVE X
TRIM PIPE ISOL VALVE X X (1)
AUX FWD XFR VALVE X
OUTR TK XFR VALVES X
TRIM TK X X (1)
LH OUTR DC1
RH OUTR DC1
LH INR DC1
RH INR X X (1)
TANK INLET VALVES
CTR DC2 X (1)
AFT PUMP X (2)X (1)
APU FWD PUMP AC1-1
ISOL VALVE X
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
ELECTRICAL SUPPLY
A330/A340 FLEET DSC-28-40 P 2/4
FCOM 19 AUG 10
Continued from previous page
NORM EMER ELEC
AC DC DC
BAT
AC
ESS
DC
ESS HOT
LP VALVE X X
JETTISON MOT 1 DC1
VALVES L AND R MOT 2 DC1
REFUEL VALVES X X (1)
(1) HOT BUS supply during refueling on batteries.
(2) Normal control is from DC1.
In emergency configuration, if the normal PUMP 1 is failed or switched OFF, then the control of STBY PUMP 4 is
automatically switched to the DC ESS BUS.
(3) In emergency configuration, this supply is lost on batteries only, or if the EMER GEN is powered by :
The RAT when LAND RECOVERY is selected, or when the speed is below 260 kt (‐ whichever occurs first) ;
‐ An engine-driven pump, when LAND RECOVERY is selected.
BUS EQUIPMENT LIST
Applicable to:
NORM EMER ELEC
AC DC DC
BAT
AC
ESS
DC
ESS HOT
1 LeveMl Saeinnsing SSHHEEDD
Main DC2 X (1) FCMC
2 Level Sensing SHED
L 1 AC2 DC2
L 2 X (3)X
R 1 AC2 DC2
R 2 DC1 (2)X (3)X (2)
L STBY AC1 DC1
INNER TANK PUMPS
R STBY AC1 DC1
TRIM TK FWD XFR PUMP AC2 DC2
CROSS FEED X-FEED MOTOR 1 X
VALVES MOTOR 2 DC2
ENGINE LP VALVES MMOOTTOORR 12 DC2 X
AFT XFR VALVES RLHH DDCC12
TRIM TK ISOL VALVE X
TRIM PIPE ISOL VALVE X X (1)
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
ELECTRICAL SUPPLY
A330/A340 FLEET DSC-28-40 P 3/4
FCOM 19 AUG 10
Continued from previous page
NORM EMER ELEC
AC DC DC
BAT
AC
ESS
DC
ESS HOT
AUX FWD XFR VALVE X
XFR VALVES X
TANK INLET VALVES X X (1)
REFUEL VALVE(S) X X (1)
FWD PUMP AC1
AFT PUMP X (3)X (1)
APU ISOL VALVE X
LP VALVE X X
(1) HOT BUS supply during refueling on batteries.
(2) Normal control is from DC1.
In emergency configuration, if the normal PUMP L2 is failed or switched OFF, then control of the normal PUMP R2 is
automatically switched to DC ESS BUS.
(3) In emergency configuration, this supply is lost on batteries only, or if the EMER GEN is powered by :
The RAT when LAND RECOVERY is selected, or when the speed is below 260 kt (‐ whichever occurs first) ;
‐ An engine-driven pump, when LAND RECOVERY is selected.
BUS EQUIPMENT LIST
Applicable to: ,
NORM EMER ELEC
AC DC DC
BAT
AC
ESS
DC
ESS HOT
1 LeveMl Saeinnsing SSHHEEDD
Main DC2 X (1) FCMC
2 Level Sensing SHED
L 1 AC2 DC2
L 2 X (3)X
R 1 AC2 DC2
R 2 DC1(2)X (3)X (2)
L STBY AC1 DC1
INNER TANK PUMPS
R STBY AC1 DC1
CTR TK 1 AC1 DC1
TRANSFER PUMPS 2 AC2 DC2
TRIM TK FWD XFR PUMP AC2 DC2
CROSS FEED X-FEED MOTOR 1 X
VALVES MOTOR 2 DC2
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
ELECTRICAL SUPPLY
A330/A340 FLEET DSC-28-40 P 4/4
FCOM 19 AUG 10
Continued from previous page
NORM EMER ELEC
AC DC DC
BAT
AC
ESS
DC
ESS HOT
ENGINE LP VALVES MMOOTTOORR 12 DC2 X
AFT XFR VALVES RLHH DDCC12
TRIM TK ISOL VALVE X
TRIM PIPE ISOL VALVE X X (1)
AUX FWD XFR VALVE X
XFR VALVES X
TANK INLET VALVES X X (1)
REFUEL VALVE(S) X X (1)
CENTER TANK INLET VALVE X
FWD PUMP AC1
AFT PUMP X (3)X (1)
APU ISOL VALVE X
LP VALVE X X
(1) HOT BUS supply during refueling on batteries.
(2) Normal control is from DC1.
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 3(29)
