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APU FIRE DET LAV DET ENG 1 LOOP B
ENG 2 LOOP A PACK 2 COND CTL2
L TK PUMP 2 R TK PUMP 2
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 149/252
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 CTR TK XFR valves
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 150/252
FCOM 19 AUG 10
ELEC EMER CONFIG
Applicable to:
LAND ASAP
MIN RAT SPEED......................................................................................................................140 KT
CAUTION At a speed below 140 kt the RAT will stall, and the aircraft electrical supply will be
from batteries only.
GEN 1 + 2................................................................................................................... OFF THEN ON
IF UNSUCCESSFUL:
BUS TIE................................................................................................................................OFF
L2 Setting BUS TIE pb-sw to OFF segregates both generator channels.
L1GEN 1 + 2.............................................................................................................OFF THEN ON
L2Note: If any generator reset is successful, reset both FAC’s.
L1 EMER ELEC PWR (IF EMER GEN NOT IN LINE)........................................................ MAN ON
CAUTION In case of simultaneous engine generator failure, the probability of a successful
APU GEN coupling is low. Therefore APU start attempts should be avoided, as
this will consequently reduce the flight time on batteries only (by about 3.5 min
for one start attempt).
ENG MODE SEL..................................................................................................................... IGN
L2 Engines are fed by gravity only.
L1 VHF1/HF1 /ATC1....................................................................................................................USE
L2 Only VHF 1 and ATC 1 are supplied in the electrical emergency configuration.
Note: FMGC 1, which is lost temporarily, can be regained by flight crew passing through the
MCDU MENU page.
L1 APPR NAVAID....................................................................................................................ON RMP 1
IR 2 + 3 (IF IR 1 OK)................................................................................................................... OFF
L2 ADIRS 2 and 3 will be lost 5 min after the loss of both engine generators. Therefore switching them
off will save battery charge.
L1 FUEL GRVTY FEED
L2 Engines are fed by gravity only. Avoid negative Gs.
L1 PROC: GRVTY FUEL FEEDING
L2 Apply GRVTY FUEL FEEDING procedure (Refer to PRO-ABN-28 GRVTY FUEL FEEDING).
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 151/252
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
L1 IF TIME TO LDG > 5 MN and L/G is down:
L2With landing gear down, batteries only supply the aircraft. If landing cannot be made within
5 min, emergency generator must be connected to avoid excessive batteries discharge.
L1 L/G...........................................................................................................................................UP
L2 Select landing gear up to allow EMER GEN operation.
L1 EMER ELEC PWR..........................................................................................................MAN ON
L2 Depress the EMER ELEC PWR MAN ON pb to reset the emergency generator
L1 APU MASTER SW (IF APU NOT RUNNING)................................................................ CHECK OFF
L2Make sure that the APU MASTER SW pb-sw is off.
With the APU MASTER SW pb-sw ON, batteries supply the DC BAT BUS for 3 min.
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 8(142)
