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BRK FAN (WHEELS 5, 6, 7, 8) MDDU PRINTER
PVI ECAM SD AEVC
DATA LOADER FWD APU PUMP PART CKPT LIGHTS
L VACUUM GEN HUD
Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
(1) (If AIR DATA SWTG is set to CAPT ON 3, STBY PITOT is supplied by the AC ESS BUS, CAPT
PITOT is no longer supplied.)
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 23/166
FCOM 19 AUG 10
ELEC AC BUS 1-2 FAULT
Applicable to:
VENT EXTRACT........................................................................................................................OVRD
L2 Air is blown through the overboard valve which is partially open.
L1 PACK FLOW...................................................................................................................................HI
L12
STATUS
CAT 2 ONLY INOP SYS
See below
INOP SYS
EFIS DMC 3 ECAM DMC 1 GPWS
l CAB VENT PART GALLEY FUEL PUMP 2
ADR 3 AFT CRG VENT TR 1
REV 2 ENG 2 IGN B ENG 4 IGN B
RA 1 F STBY PUMP 3 L CTR PUMP
Y ELEC PUMP STBY AOA STBY PITOT
HF 1 VENT EXTRACT CAT 3
Other INOP SYS
BRK FAN (WHEELS 5,6,7,8) CAPT ND ECAM SD
RADAR 1 MDDU L LDG LTS
PARTIAL CKPT LIGHTS
Note: The warning may be caused by a failure in a sub BUS. Consequently only a part of
the systems listed above may be lost.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 24/166
FCOM 19 AUG 10
ELEC AC BUS 2-3 FAULT
Applicable to:
F/O EFIS DMC (IF AC BUS 2-4 FAULT NOT TRIGGERED)............................................................3
AIR DATA SWTG (IF AC BUS 2-4 FAULT NOT TRIGGERED).......................................... F/O ON 3
L2 If not already used on opposite side.
L1 PACK FLOW...................................................................................................................................HI
L12
STATUS
INOP SYS
See below
INOP SYS
EFIS DMC 2 FDIU R CAB VENT
ENG 1 IGN B ENG 3 IGN B RA 2
SDAC 2 CAT 2 B ELEC PUMP
REV 3 F/O PITOT F/O TAT
HF 2 ADr 2 ILS 2
TR 2 ATC 2 F/O AOA
PART GALLEY F. STBY PUMP 1 FUEL PUMP 3
R CTR PUMP F T.TK PUMP
Other INOP SYS
BRK FAN (WHEELS 1,2,3,4) DME 2 RADAR 2
VOR 2 F/O PFD ADF 2
Note: The warning may be caused by a failure in a sub BUS. Consequently only a part of
the systems listed above may be lost.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 25/166
FCOM 19 AUG 10
ELEC AC BUS 2-3 FAULT
Applicable to:
F/O EFIS DMC (IF AC BUS 2-4 FAULT NOT TRIGGERED)............................................................3
AIR DATA SWTG (IF AC BUS 2-4 FAULT NOT TRIGGERED).......................................... F/O ON 3
L2 If not already used on opposite side.
L1 PACK FLOW...................................................................................................................................HI
L12
STATUS
INOP SYS
See below
INOP SYS
EFIS DMC 2 FDIU R CAB VENT
ENG 1 IGN B ENG 3 IGN B RA 2
SDAC 2 CAT 2 B ELEC PUMP
REV 3 F/O PITOT F/O TAT
HF 2 ADr 2 ILS 2
TR 2 ATC 2 F/O AOA
PART GALLEY F. STBY PUMP 1 FUEL PUMP 3
R CTR PUMP F T.TK PUMP GPS 2
Other INOP SYS
BRK FAN (WHEELS 1,2,3,4) DME 2 RADAR 2
VOR 2 F/O PFD ADF 2
Note: The warning may be caused by a failure in a sub BUS. Consequently only a part of
the systems listed above may be lost.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 26/166
FCOM 19 AUG 10
ELEC AC BUS 2 FAULT
Applicable to: ,
PACK FLOW...................................................................................................................................HI
ENG 2 N1 DEGRADED MODE
NOT EXCEED N1 LIMIT
ENG 1 AND 2 N1 MODE............................................................................................................... ON
MAN THR............................................................................................................................. ADJUST
ELEC AC BUS 2-4 FAULT
Applicable to:
KEEP ENG 1 LAST (ONLY IN PHASE 9)
L2 Engine 1 must be the last engine to be shut down, to keep power supply to the HP fuel valves.
To be continued on next page
A330/A340 FLIGHT CREW
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 6(153)
