曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 33/252
FCOM 19 AUG 10
ELEC AC BUS 1 FAULT (Cont'd)
L12
STATUS
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH or Refer to 99 Duref Cible FCOM.
SLATS SLOW
CAT 2 ONLY
INOP SYS
See below
INOP SYS
BLUE HYD SPLR 3 ADR 3
RA 1 CAPT TAT L WSHLD HEAT
L WNDW HEAT REVERSER 1 L+R TK PUMP 1
CTR TK PUMP 1 VENT BLOWER GALLEY FAN
CRG VENT GND COOL N.W. STEER
MAIN GALLEY B ELEC PUMP BRAKES SYS 1
DMC 3 GPWS LAV DET
CAT 3
Other INOP SYS
Left cabin fan Radar 1 Stby Pitot/AOA
ATSU Brake fans 5, 6, 7 and 8 HUD
MCDU 3 Engine 1 ignition B EVMU eng 1 and eng 2
Printer COND controller lane A Hydraulic quantity indication
Partial galley PVI TCAS
Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 34/252
FCOM 19 AUG 10
ELEC AC BUS 2 FAULT
Applicable to:
EXTRACT.................................................................................................................................OVRD
L2 The avionics ventilation system is in the closed circuit configuration.
Air conditioning is added to the ventilation air.
L1
ASSOCIATED PROCEDURES
L/G LGCIU 2 FAULT
SECONDARY FAILURES
* AVNCS VENT
* FUEL
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 35/252
FCOM 19 AUG 10
ELEC AC BUS 2 FAULT (Cont'd)
L12
STATUS
PACK 2 AT FIXED TEMP
See (1)
CAT 1 ONLY
INOP SYS
See below
INOP SYS
ADR 2 ILS 2 RA 2
F/O PITOT F/O AOA F/O TAT
R WNDW HEAT CAT 2 L+R TK PUMP 2
CTR TK PUMP 2 LGCIU 2 REVERSER 2
VENT EXTRACT GND COOL PACK 2 REGUL
MAIN GALLEY YAW DAMPER 2 RUD TRIM 2
RUD TRV LIM 2 BRAKES SYS 2 Y ELEC PUMP
SDAC 2 FWC 2 DMC 2
FDIU R WSHLD HEAT
Other INOP SYS
Right cabin fan Brake fans 1, 2, 3 and 4 ADF 2
ECAM lower DU HF 2 MCDU 2
ENG 2 ignition B DME 2 RADAR 2
QAR ATC 2 VOR 2
F/O PFD and ND
Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
(1)DL2ue to the loss of Pack 2 controller, the pack outlet temperature is controlled by the pack anti-ice
valve and is stabilized to a temperature between 5 °C (41 °F) and 30 °C (86 °F) within a maximum
of 6 min.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 36/252
FCOM 19 AUG 10
ELEC AC BUS 2 FAULT
Applicable to:
EXTRACT.................................................................................................................................OVRD
L2 The avionics ventilation system is in the closed circuit configuration.
Air conditioning is added to the ventilation air.
L1
ASSOCIATED PROCEDURES
L/G LGCIU 2 FAULT
SECONDARY FAILURES
* AVNCS VENT
* FUEL
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 37/252
FCOM 19 AUG 10
ELEC AC BUS 2 FAULT (Cont'd)
L12
STATUS
PACK 2 AT FIXED TEMP
See (1)
INOP SYS
See below
INOP SYS
ADR 2 ILS 2 RA 2
F/O PITOT F/O AOA F/O TAT
R WNDW HEAT CAT 2 L+R TK PUMP 2
CTR TK PUMP 2 LGCIU 2 REVERSER 2
VENT EXTRACT GND COOL PACK 2 REGUL
MAIN GALLEY YAW DAMPER 2 RUD TRIM 2
RUD TRV LIM 2 BRAKES SYS 2 Y ELEC PUMP
SDAC 2 FWC 2 DMC 2
FDIU R WSHLD HEAT
Other INOP SYS
Right cabin fan Brake fans 1, 2, 3 and 4 ADF 2
ECAM lower DU HF 2 MCDU 2
ENG 2 ignition B DME 2 RADAR 2
QAR ATC 2 VOR 2
F/O PFD and ND
Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
(1)DL2ue to the loss of Pack 2 controller, the pack outlet temperature is controlled by the pack anti-ice
valve and is stabilized to a temperature between 5 °C (41 °F) and 30 °C (86 °F) within a maximum
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
A320机组操作手册FLIGHT CREW OPERATING MANUAL 8(118)
