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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 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).
L1 FAC 1.......................................................................................................................... OFF THEN ON
L2 The rudder trim is recovered, although no indication is available.
L1 BUS TIE....................................................................................................................................AUTO
L2 Setting BUS TIE pb-sw to AUTO enables the APU to take an available electrical channel.
L1 APU (IF AVAIL)........................................................................................................................ START
L2 APU start is not available for 45 s after the loss of both engine generators. This 45 s delay prevents
any interference with emergency generator coupling.
If the APU is available, the APU may be started when below FL 250.
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 175/252
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
L1 BLOWER + EXTRACT...............................................................................................................OVRD
L2Cooling air is supplied by the air conditioning system and exhausted overboard through the extract
valve.
L1
L2Note: On IAE powered aircraft, the warning “EPR MODE FAULT N1 DEGRADED MODE” is
displayed.
L1
ASSOCIATED PROCEDURES
FLT CTL ALTN LAW
(PROT LOST)
MAX SPEED...........................................................................................................................320 KT
L2 Speed limited due to loss of flight control normal laws.
L1
SECONDARY FAILURES
* CAB PRESS
* HYD
* FUEL
* AIR COND
* BRAKES
* WHEEL
* F/CTL
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 176/252
FCOM 19 AUG 10
FLT ON BAT ONLY
Applicable to:
Flight time on batteries only may be increased to at least 30 min, as follows:
ENG MODE SEL.......................................................................................................................NORM
ANTI ICE PITOT 1 C/B (D 02)....................................................................................................PULL
26 V ADIRU 1 C/B (F 07)...........................................................................................................PULL
Loss of the CM 1 altitude speed, and vertical speed indication on the PFD. Use standby
instruments.
�� 7 min before landing:
ANTI ICE PITOT 1 C/B (D 02).......................................................................................... RESET
�� After 1 min:
CAUTION This time delay is necessary to ensure reliable speed information even in
icing conditions, when the ADIRU is reset to ON.
26 V ADIRU 1 C/B (F 07)...........................................................................................RESET
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 177/252
FCOM 19 AUG 10
ELEC ESS BUSES ON BAT
Applicable to:
L2DC ESS BUS is supplied by the batteries. AC ESS BUS is also supplied by the batteries, via the
STATIC INVERTER.
L1 LAND ASAP
�� WHEN L/G UPLOCKED:
EMER ELEC PWR..........................................................................................................MAN ON
L2 ESS BUSES are supplied by the emergency generator.
L1�� IF L/G RETRACT FAULT:
L2 If the landing gear fails to retract during a go-around, when in emergency configuration, the
emergency generator can be recovered as follows :
L1MIN RAT SPD....................................................................................................................180 KT
L2 Accelerate to 180 kt to recover RAT operation, with the landing gear down.
　
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