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TR
GEN1
ESS
TR
GEN1
BAT1 BAT2
TR1 + 2 FAULT GEN1 GEN2GEN1 GEN1 - - - GEN1 - - - ESS
TR
-GEN1
ESS
TR
-GEN1
BAT1 BAT2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A318/A319/A320/A321 FLEET DSC-24-10-30-40 P 3/4
FCOM 19 AUG 10
ON GROUND
BAT. ONLY
AC
BUS
1
AC
BUS
2
AC
ESS
BUS
AC
SHED
ESS
AC
STAT
INV
TR1 TR2 ESS
TR
DC
BUS
1
DC
BUS
2
DC
BAT
BUS
DC
ESS
BUS
DC
SHED
ESS
HOT
BUS
1
HOT
BUS
2
Speed >100 kt - - EMER
GEN
EMER
GEN
- - - EMER
GEN
- - - ESS
TR
EMER
GEN
ESS
TR
EMER
GEN
BAT1 BAT2
rat stall or 50 kt ≤
speed ≤ 100 kt
- - ST
INV
BAT1
- ST
INV
BAT1
- - - - - BAT
1-2
BAT2 - BAT1 BAT2
Speed < 50 kt - - - - ST
INV
BAT1
- - - - - BAT
1-2
BAT2 - BAT1 BAT2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-24-10-30-40 P 4/4
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
CONTROLS AND INDICATORS
A318/A319/A320/A321 FLEET DSC-24-20 P 1/44
FCOM 19 AUG 10
OVERHEAD PANEL
Applicable to:
(1) BAT 1 (2) ind.
Shows battery voltage in white.
(2) BAT 1 (2) pb sw
Controls the operation of the corresponding battery charge limiter.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
CONTROLS AND INDICATORS
A318/A319/A320/A321 FLEET DSC-24-20 P 2/44
FCOM 19 AUG 10
Auto : The battery charge limiter controls automatically the connection and the
disconnection of the corresponding battery to the DC BAT BUS (3 PP) by closing
and opening of the battery line contactor.
The batteries are connected to the DC ‐ BAT BUS in the following cases :
• APU starting (MASTER SW at ON and N < 95 %).
Note: The connection is limited to 3 min when the emergency generator
is running.
• Battery voltage below 26.5 V (battery charge). The charging cycle ends
when battery charge current goes below 4 A.
‐ on ground, immediately
‐ in flight, after a time delay of 30 min .
• Loss of AC BUS 1 and 2 when below 100 kt (EMER GEN not supplying).
‐ If AC BUS 1 and 2 are not energized and the EMER GEN is not supplying :
• battery 1 supplies the AC STAT INV BUS, and, if speed is greater than 50 kt,
the AC ESS BUS.
• battery 2 supplies the DC ESS BUS.
Note: In normal configuration the batteries are disconnected most of the
time.
Note: A battery automatic cut-off logic prevents the batteries from
discharging completely when the aircraft is on the ground (parking).
Automatic battery contactors open when :
‐ The aircraft is on the ground.
‐ The BAT pushbutton switches are at AUTO.
‐ The main power supply (EXT PWR + GEN) is cut off.
‐ Battery voltage is low.
The flight crew can reset the contactors by switching the BAT
pushbutton switch to OFF then to AUTO.
OFF : The battery charge limiter is not operating : the battery line contactor is open.
OFF comes on white if the DC BAT BUS is supplied. Hot buses remain
supplied.
FAULT lt : Comes on amber, accompanied by an ECAM caution, when the charging
current for the corresponding battery is outside limits.
In this case the battery contactor opens.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
CONTROLS AND INDICATORS
A318/A319/A320/A321 FLEET DSC-24-20 P 3/44
FCOM 19 AUG 10
(3) IDG 1 (2) (Integrated Drive Generator) pb sw (guarded)
CAUTION 1. Holding this pushbutton switch in for more than about 3 s may damage the
disconnection mechanism.
2. Do not disconnect the IDG when the engine is not running (or not
windmilling), because starting the engine after having done so will damage
the IDG.
The IDG switches are normally springloaded out.
Pressing this switch disconnects the IDG from its driveshaft : only maintenance personnel can
reconnect it.
FAULT lt : Lights up amber, and ECAM caution comes on, if :
IDG oil outlet ‐ overheats (above 185 °C), or
‐ IDG oil pressure is low (inhibited at low engine speed : N2 below 14 %)
　
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