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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.
If the APU is available, the APU may be started when below FL 250.
L1 BLOWER + EXTRACT...............................................................................................................OVRD
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 159/252
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
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
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 160/252
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
L2 ECAM lower display is not available. STATUS page is displayed on the upper ECAM display, as
long as the STS pb is pressed.
L12
STATUS
MIN RAT SPEED..................................................... 140 KT
MAX SPEED............................................................ 320 KT
MAX BRK PR........................................................1000 PSI
FUEL GRVTY FEED
AVOID NEGATIVE G FACTOR
Note: If there are discrepancies between airspeed indications
on the Captain’s PFD and on the STBY indicator,
disregard the STBY indication (probe not deiced).
APPR PROC
FOR LDG...................................................................USE FLAP 3
�� AT FT AGL:
L/G.......................................................................................DN
Note: 1. With the landing gear down, electrical power is
supplied by batteries only. Battery endurance
time is approximately 22 min.
2. Both FACs are not supplied after landing gear
extension. Check the approach speed on the
QRH.
APPR SPD........................................................VREF +10/140 KT
Approach speed must be at least minimum RAT speed (140 kt).
　
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