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APU ECB Manual pressure control FMGC 2
Rudder trim indication BMC 2 FQI channel 2
Eng 1 and 2 fire ext btl 2 X Bleed auto control SDCU 2
(1) LL2ost after 30 s, but is recovered at landing gear extension.
(2) Note: The warning may be caused by a failure in a sub BUS. Consequently, only a part of the
above-listed systems may be lost.
(3) Note: The APU battery start can be recovered by setting the APU MASTER SW pb-sw to ON.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 141/252
FCOM 19 AUG 10
ELEC DC BUS 1+2 FAULT
Applicable to:
MSN,
BLOWER.................................................................................................................................. OVRD
EXTRACT.................................................................................................................................OVRD
BARO REF.............................................................................................................................CHECK
L2Crosscheck the barometer reference settings on the FCU and PFDs.
L1MAX BRK PR.......................................................................................................................1 000 PSI
L2 Brake pressure must be limited to approximately 1 000 PSI, since antiskid is lost.
L1
ASSOCIATED PROCEDURES
ELEC DC BAT BUS FAULT
SECONDARY FAILURES
* CAB PRESS
* FUEL
* AIR COND
* BRAKES
* WHEEL
* F/CTL
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 142/252
FCOM 19 AUG 10
ELEC DC BUS 1+2 FAULT (Cont'd)
L12
STATUS
MAX BRK PR........................................................1000 PSI
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
ENG 1 APPR IDLE ONLY
ENG 2 APPR IDLE ONLY
BOTH PFD ON SAME FAC
CTR TK FUEL UNUSABLE
APU BAT START NOT AVAIL
See (3)
CAB AT FIXED TEMP
SLATS/FLAPS SLOW
CAT 3 SINGLE ONLY
INOP SYS
See below
INOP SYS
SPLR 1+2+5 ELAC 2 SEC 2+3
VHF 2 ACP 3 CAPT STAT heat
F/O STAT heat STBY STAT heat WSHLD HEAT
WNDW HEAT AP 2 FCU 2
FCDC 2 CAT 3 DUAL FAC 2
ANTI SKID N.W. STEER NORM BRK
AUTO BRK LGCIU 2 REV 1+2
CAB PRESS 2 AVNCS VENT L+R CAB FAN
GALLEY FAN GND COOL MAIN GALLEY
Y ELEC PUMP BRAKE SYS 1 BRAKE SYS 2
APU FIRE DET LAV DET ENG 1 LOOP B
ENG 2 LOOP A PACK 2 COND CTL 2
L TK PUMP 2 R TK PUMP 2 CTR TK PUMPS
Other INOP SYS
Selcal Brake temp indication Brake fans
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 143/252
FCOM 19 AUG 10
ELEC DC BUS 1+2 FAULT (Cont'd)
TPIS Capt and F/O wipers Eng 1 and 2 oil pressure
and quantity indication
Autobrake Stick and rudder pedals lock (by AP) VHF 3
RMP 2 RMP 3 CFDIU
Right loudspeakers SFCC 2 CDLS
APU ECB Manual pressure control FMGC 2
Rudder trim indication BMC 2 FQI channel 2
Eng 1 and 2 fire ext btl 2 X Bleed auto control CIDS 2 SMOKE DETECT
(1) LL2ost after 30 s, but is recovered at landing gear extension.
(2) Note: The warning may be caused by a failure in a sub BUS. Consequently, only a part of the
above-listed systems may be lost.
(3) Note: The APU battery start can be recovered by setting the APU MASTER SW pb-sw to ON.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 144/252
FCOM 19 AUG 10
ELEC DC BUS 1+2 FAULT
Applicable to: ,
BLOWER.................................................................................................................................. OVRD
EXTRACT.................................................................................................................................OVRD
BARO REF.............................................................................................................................CHECK
L2Crosscheck the barometer reference settings on the FCU and PFDs.
L1MAX BRK PR.......................................................................................................................1 000 PSI
L2 Brake pressure must be limited to approximately 1 000 PSI, since antiskid is lost.
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 8(140)
