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L1 FAC 1.......................................................................................................................... OFF THEN ON
L2 The rudder trim is recovered, although no indication is available.
L1 BLOWER + EXTRACT...............................................................................................................OVRD
L2Cooling air is supplied by the air conditioning system and exhausted overboard through the extract
valve.
L1LDG ELEV.....................................................................................................................MAN ADJUST
L2 Landing elevation has to be manually set since no FMGC is supplied after landing gear extension.
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
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 152/252
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
* 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 153/252
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).
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 154/252
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 155/252
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
　
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