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ELEC AC BUS 1-1 FAULT
Applicable to:
AIR DATA SWTG (IF ADR 3 AVAIL)............................................................................... CAPT ON 3
KEEP ENG 4 LAST (ONLY IN PHASE 9)
L2 Engine 4 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
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 16/166
FCOM 19 AUG 10
ELEC AC BUS 1-1 FAULT (Cont'd)
L12
STATUS
• On ground:
CAB TEMP REGUL DEGRADED
INOP SYS
LAV + GAL VENT
GND COOL
L WNDOWHEAT
CAPT AOA
CAPT TAT
G ELEC PUMP
L WSHLD HEAT
ACARS 1+2
PART GALLEY
TCAS
Other INOP SYS
PARTIAL CKPT LIGHTS
WATER HEATER
L VACUUM GEN
PVI
DME 1
FWD APU PUMP
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 17/166
FCOM 19 AUG 10
ELEC IDG 1(2)(3)(4) OIL SYS FAULT
(ON GROUND)
Applicable to:
L2Crew awareness.
ELEC AC BUS 1 FAULT
Applicable to:
L2 If the automatic transfer of AC ESS BUS is inoperative, the ECAM’s E/WD and SD DUs are
simultaneously lost.
The ECAM/ND SEL must be used to recover the E/WD on the NDU, in order to apply the ECAM
procedure.
L1AC ESS FEED........................................................................................................................... ALTN
L2 This line is displayed, if automatic AC ESS transfer has failed.
L1 EMER ELEC PWR.................................................................................................................MAN ON
L2 This line is displayed, if manual AC ESS transfer has failed.
L1VENT EXTRACT........................................................................................................................OVRD
L2 Air is blown through the overboard valve which is partially open.
L1 PACK FLOW...................................................................................................................................HI
ENG 1 N1 DEGRADED MODE
NOT EXCEED N1 LIMIT
ENG 1 AND 2 N1 MODE............................................................................................................... ON
MAN THR............................................................................................................................. ADJUST
PAX SYS (ONLY IN PHASE 1, 2, 9 OR 10, VCC )...............................................................OFF
PAX SYS AVAIL IN FLT (VCC )
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 18/166
FCOM 19 AUG 10
ELEC AC BUS 1 FAULT (Cont'd)
L12
STATUS
• Only on ground:
CAB TEMP REGUL DEGRADED
CAT 2 ONLY
ENG 1 N 1 DEGRADED MODE
• If VCC installed:
PAX SYS AVAIL IN FLT
INOP SYS
See below
INOP SYS
EFIS DMC 3 ECAM DMC 1 REV 1
STBY AOA ACARS 1+2 PART GALLEY
RA 1 R FUEL STBY L FUEL STBY
TR 1 G ELEC PUMP Y ELEC PUMP
L CAB VENT GND COOL VENT EXTRACT
AFT CRG VENT CAT 3 LAV + GAL VENT
GPWS TCAS LWNDWHEAT
STBY PITOT (1) CAPT TAT ADR 1
ADR 3 FUEL AFT XFR L CTR PUMP
Other INOP SYS
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 19/166
FCOM 19 AUG 10
ELEC AC BUS 1 FAULT
Applicable to:
L2 If the automatic transfer of AC ESS BUS is inoperative, the ECAM’s E/WD and SD DUs are
simultaneously lost.
The ECAM/ND SEL must be used to recover the E/WD on the NDU, in order to apply the ECAM
procedure.
L1AC ESS FEED........................................................................................................................... ALTN
L2 This line is displayed, if automatic AC ESS transfer has failed.
L1 EMER ELEC PWR.................................................................................................................MAN ON
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 6(151)
