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LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
ALTN LAW: PROT LOST
WHEN L/G DN: DIRECT LAW
BAT ONLY
CTR TK FUEL UNUSABLE
INOP SYS
F/CTL PROT
REVERSER 1+2
ADR 2+3
IR 2+3
RA 1+2
SPLR 1+2+5
ELAC 2
SEC 2+3
A/CALL OUT
AP 1+2
A/THR
FUEL PUMPS
ANTI SKID
N.W. STEER
For other systems’ status:
Refer to the “ELEC EMER
CONFIG SYS REMAINING”
table.
Note: For go-around
procedure, Refer
to PRO-ABN-24
ELEC ESS
BUSES ON BAT.
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 161/252
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
SLATS/FLAPS SLOW
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 162/252
FCOM 19 AUG 10
ELEC EMER CONFIG
Applicable to:
MSN,
LAND ASAP
MIN RAT SPEED......................................................................................................................140 KT
CAUTION The RAT is capable of supplying the EMER GEN down to 125 kt, except during
flare.
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
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.
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 163/252
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
If the APU is available, the APU may be started when below FL 250.
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
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
　
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