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sub BUS failure.
Consequently,
only a part of
the above-listed
systems may be
lost.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 36/166
FCOM 19 AUG 10
ELEC AC ESS BUS SHED
Applicable to:
Crew awareness.
L12
STATUS
INOP SYS
ATC 1
Other INOP SYS
MCDU 1
CVR
Note: The warning may
be caused by a
sub BUS failure.
Consequently,
only a part of
the above-listed
systems may be
lost.
ELEC AC ESS BUS SHED
Applicable to: ,
AIR DATA SWTG............................................................................................................. CAPT ON 3
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 37/166
FCOM 19 AUG 10
ELEC AC ESS BUS SHED (Cont'd)
L12
STATUS
INOP SYS
CAPT AOA
ATC 1
FUEL AFT XFR
HF 1
L WSHLD HEAT
L FUEL PUMP 2
R FUEL PUMP 2
Other INOP SYS
MCDU 1
CVR
L LDG LTS
CAPT ND
DME 1
RADAR 1
Note: 1. The warning
may be caused
by a sub
BUS failure.
Consequently,
only a part of
the above-listed
systems may
be lost.
2. AP2 pb light
is lost. AP2
engagement
can be checked
on the FMA.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 38/166
FCOM 19 AUG 10
ELEC AC ESS BUS SHED
Applicable to:
Crew awareness.
AIR DATA SWTG............................................................................................................. CAPT ON 3
L12
STATUS
INOP SYS
ATC 1
Other INOP SYS
MCDU 1
CVR
Note: The warning may
be caused by a
sub BUS failure.
Consequently,
only a part of
the above-listed
systems may be
lost.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 39/166
FCOM 19 AUG 10
ELEC AC ESS BUS SHED (Cont'd)
L12
STATUS
INOP SYS
CAPT AOA
ATC 1
FUEL AFT XFR
HF 1
L WSHLD HEAT
L FUEL PUMP 2
R FUEL PUMP 2
Other INOP SYS
MCDU 1
CVR
L LDG LTS
CAPT ND
DME 1
RADAR 1
Note: 1. The warning
may be caused
by a sub
BUS failure.
Consequently,
only a part of
the above-listed
systems may
be lost.
2. AP2 pb light
is lost. AP2
engagement
can be checked
on the FMA.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 40/166
FCOM 19 AUG 10
ELEC EMER CONFIG
(GEN NOT RECOVERED OR APU GEN NOT AVAILABLE)
Applicable to:
LAND ASAP
EMER ELEC PWR.................................................................................................................MAN ON
L2 Display only if EMER GEN not automatically coupled.
L1ALL GEN..................................................................................................................... OFF THEN ON
L2 If at any time any GEN recover, or if the APU GEN is available, Refer to PRO-ABN-24-AI ELEC
EMER CONFIG (All GEN Recovered or APU GEN Available) and Refer to PRO-ABN-24-AI ELEC
EMER CONFIG (All GEN Recovered or APU GEN Available) - FWSPAGE for the applicable ECAM
procedure and status.
L1BUS TIE.......................................................................................................................................OFF
L2 Setting BUS TIE pb-sw to OFF segregates all generator channel.
L1ALL GEN..................................................................................................................... OFF THEN ON
VHF 1/ATC 1 (IF EMER GEN SUPPLIED BY ENG. HYD. PUMPS)........................................... USE
VHF 1 (IF EMER GEN SUPPLIED BY RAT)............................................................................... USE
L2 SELCAL is inoperative.
L1VENT EXTRACT........................................................................................................................OVRD
L2 Switch EXTRACT pb-sw OVRD since extract fan and cabin fans are lost.
CAUTION In case of discrepancies between air speed indications on captain PFD and on
　
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