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The AC ESS SHED, the DC ESS SHED and the SHED LAND RECOVERY are not supplied.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A330/A340 FLEET DSC-24-10-30-30 P 15/16
FCOM 19 AUG 10
Note: ELEC AC ECAM page is identical to the one for flight with batteries only.
ON GROUND, BATTERIES ONLY
Applicable to: ,
Provided they are both selected AUTO, batteries supply the :
‐ DC ESS BUS
‐ DC BAT BUS
‐ DC LAND RECOVERY (whatever the position of the LAND RECOVERY pushbutton)
And, through the static inverter, the :
‐ AC ESS BUS, and
‐ AC ESS GND
‐ AC LAND RECOVERY (whatever the LAND RECOVERY pushbutton position is)
The AC ESS SHED, the DC ESS SHED and the SHED LAND RECOVERY are not supplied.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A330/A340 FLEET DSC-24-10-30-30 P 16/16
FCOM 19 AUG 10
Note: ELEC AC ECAM page is identical to the one for flight with batteries only.
On ground, the external horn is activated, if the following conditions are met :
‐ External power contactor OFF (ground power unit disconnected, or EXT PWR pushbutton at OFF ;
‐ Generators not running ;
‐ BAT pushbutton switched at auto, and batteries connected to the aircraft network.
If the batteries are not switched off, the horn automatically stops after 5 min.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A330/A340 FLEET DSC-24-10-30-40 P 1/4
FCOM 19 AUG 10
DISTRIBUTION TABLE
DISTRIBUTION TABLE
Applicable to:
White compartments : Same supply as in normal configuration.
Shaded
compartments
: Back up supply.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A330/A340 FLEET DSC-24-10-30-40 P 2/4
FCOM 19 AUG 10
EMER CONFIG AC
BUS
1-1
AC
BUS
1-2
AC
BUS
2-3
AC
BUS
2-4
AC
ESS
BUS
AC
ESS
GND
AC
ESS
SHED
AC
LAND
REC
DC
BUS
1
DC
BUS
2
DC
BAT
BUS
DC
ESS
BUS
DC
ESS
SHED
DC
LAND
REC
SHED
LAND
REC
• BATTERIES
ONLY (in flight)
– – – – STAT
INV
BAT
1-2
– – STAT
INV
BAT
1-2
– – See BAT
1-2
– BAT
1-2
–
• EMER GEN
SUPPLIED BY
ENGINE DRIVEN
PUMP
– – – – EMER
GEN
– EMER
GEN
EMER
GENSee
– – – ESS
TR
EMER
GEN
ESS
TR
EMER
GEN
ESS
TR
EMER
GENSee
ESS
TR
EMER
GENSee
• EMER GEN
SUPPLIED BY
RAT
– – – – EMER
GEN
– – EMER
GENSee
– – – ESS
TR
EMER
GEN
– ESS
TR
EMER
GENSee
–
ON GROUND AC
BUS
1-1
AC
BUS
1-2
AC
ESS
BUS
2-3
AC
BUS
2-4
AC
ESS
BUS
AC
ESS
GND
AC
ESS
SHED
AC
LAND
REC
DC
BUS
1
DC
BUS
2
DC
BAT
BUS
DC
ESS
BUS
DC
ESS
SHED
DC
LAND
REC
SHED
LAND
REC
BAT only, V>50 kt – – – – STAT
INV
BAT
1-2
– – STAT
INV
BAT
1-2
– – – BAT
1-2
– BAT
1-2
–
BAT only, V<50 kt – – – – STAT
INV
BAT
1-2
STAT
INV
BAT
1-2
– STAT
INV
BAT
1-2
– – BAT
1-2
BAT
1-2
– BAT
1-2
–
(1) Supplied when LAND RECOVERY pushbutton is at ON.
(2) Lost in case of overcurrent on the faulty TR.
(3) In case of differential protection failure :
• The affected generator is not replaced ;
• The associated TR is switched off.
(4) Lost after 7 s.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ELECTRICAL
DESCRIPTION - OPERATIONS
A330/A340 FLEET DSC-24-10-30-40 P 3/4
　
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