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The C/B TRIPPED warning on the ECAM indicates the location of the affected C/B. The following
panels are monitored : OVHD PNL, L(R) ELEC BAY, REAR PNL J-M or N-R or S-V or W-Z.
Note: The C/B TRIPPED caution may be cleared from the ECAM by pressing the CLR or the
EMER CANCEL pushbutton. If the EMER CANCEL is used, and if a second C/B is tripped
on the same panel, the corresponding C/B TRIPPED caution will not be triggered.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A318/A319/A320/A321 FLEET DSC-24-10-30-10 P 1/2
FCOM 19 AUG 10
GENERAL
GENERAL
Applicable to: ALL
GEN 1 and 2 when operating have priority over the APU generator and over external power.
External power has priority over the APU generator when the EXT PWR pushbutton switch is ON.
The APU generator or external power can supply the entire network.
One engine generator can supply the entire network.
The generators cannot be connected in parallel.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-24-10-30-10 P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A318/A319/A320/A321 FLEET DSC-24-10-30-20 P 1/6
FCOM 19 AUG 10
NORMAL CONFIGURATION
IN FLIGHT
Applicable to:
Each engine-driven generator supplies its associated AC BUS (1 and 2) via its generator line
contactor (GLC 1 and GLC 2).
AC BUS 1 normally supplies the AC ESS BUS via a contactor.
TR 1 normally supplies DC BUS 1, DC BAT BUS, and DC ESS BUS.
TR 2 normally supplies DC BUS 2.
The two batteries are connected to the DC BAT BUS, if they need charging. When they are fully
charged, the battery charge limiter disconnects them.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A318/A319/A320/A321 FLEET DSC-24-10-30-20 P 2/6
FCOM 19 AUG 10
IN FLIGHT
Applicable to:
,
,
MSN,,,,
Each engine-driven generator supplies its associated AC BUS (1 and 2) via its generator line
contactor (GLC 1 and GLC 2).
AC BUS 1 normally supplies the AC ESS BUS via a contactor.
TR 1 normally supplies DC BUS 1, DC BAT BUS, and DC ESS BUS.
TR 2 normally supplies DC BUS 2.
The two batteries are connected to the DC BAT BUS, if they need charging. When they are fully
charged, the battery charge limiter disconnects them.
ON GROUND
Applicable to:
Either the APU generator, or external power, may supply the complete system.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A318/A319/A320/A321 FLEET DSC-24-10-30-20 P 3/6
FCOM 19 AUG 10
On ground, when only ground services are required, external power can supply the AC and DC
GND/FLT BUSES directly without supplying the entire aircraft network.
Personnel select this configuration with the MAINT BUS switch in the forward entrance area.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A318/A319/A320/A321 FLEET DSC-24-10-30-20 P 4/6
FCOM 19 AUG 10
ON GROUND
Applicable to:
,
,
MSN,,,,
Either the APU generator, or external power, may supply the complete system.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A318/A319/A320/A321 FLEET DSC-24-10-30-20 P 5/6
FCOM 19 AUG 10
On ground, when only ground services are required, external power can supply the AC and DC
GND/FLT BUSES directly without supplying the entire aircraft network.
Personnel select this configuration with the MAINT BUS switch in the forward entrance area.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A318/A319/A320/A321 FLEET DSC-24-10-30-20 P 6/6
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A318/A319/A320/A321 FLEET DSC-24-10-30-30 P 1/22
FCOM 19 AUG 10
ABNORMAL CONFIGURATIONS
FAILURE OF ONE ENGINE GENERATOR
Applicable to:
The system automatically replaces the failed generator, with the :
‐ APU GEN, if available, or
‐ Other engine generator (automatically shedding part of the galley load).
FAILURE OF ONE ENGINE GENERATOR
Applicable to:
MSN,
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 2(150)
