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L2 Switch EXTRACT pb-sw OVRD since extract fan and cabin fans are lost.
CAUTION In case of discrepancies between air speed indications on captain PFD and on
standby indicator, disregard standby indicator (probe not deiced).
Note: 1. In case of an engine 2 failure, engine windmilling at around 210 kt may induce transient
hydraulic system lo press and right outer aileron motion. The OFF selection of the
yellow hydraulic pump, on the overhead panel, is inoperative.
Only VOR 1 or ADF 1 (as selected on the DDRMI) is available. The ADF selector/VOR
selector position on the FCU must be in accordance with ADF selector/VOR selector on
DDRMI
2. Engine anti-ice is ON, regardless of the pushbutton's position, so fuel consumption
increases by approximately 1.5 %.
L1 ENG 1+2 N1 DEGRADED MODE
ENG 1 N1 MODE........................................................................................................................... ON
ENG 2 N1 MODE........................................................................................................................... ON
DO NOT EXCEED N1 LIMIT
MAN THR............................................................................................................................. ADJUST
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 73/166
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
(GEN NOT RECOVERED OR APU GEN NOT AVAILABLE)
SEC 2.................................................................................................................................KEEP ON
WEIGHT/CG........................................................................................................................INITIALIZE
L2 This line appears because the FCMCs lose the WEIGHT/CG information, due to the power
interruption that occurs before EMER GEN activation.
The GW and CG must be initialized again in the FCMC, by manually re-entering their values in the
FUEL PRED SD page.
L1�� FOR SLATS EXTENSION:
LAND RECOVERY................................................................................................................... ON
L2 SFCC 1, LGCIU 1, BSCU 1 and WHC 1 are recovered. The remaining fuel pump is lost.
L1�� FOR L/G GRVTY EXTN:
MAX SPEED...................................................................................................................... 200 KT
L/G GRVTY EXTN..............................................................................................................DOWN
�� WHEN L/G DOWNLOCKED:
L/G LEVER......................................................................................................................... DOWN
L2Note: In case of a go-around, gear retraction is not available, and CLIMB performance is
degraded.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 74/166
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
(GEN NOT RECOVERED OR APU GEN NOT AVAILABLE)
L12
STATUS
SPD BRK.......................................................DO NOT USE
MAX SPEED.......................................................... 330/0.82
APPR PROC
�� FOR SLATS EXTENSION:
LAND RECOVERY............................................................. ON
FOR LDG............................................................ USE FLAP 3
This line is replaced by "FOR LDG: USE FLAP 3" when
CONF 3 is selected, as a reminder.
�� FOR L/G GRVTY EXTN:
MAX SPEED................................................................ 200 KT
L/G GRVTY EXTN........................................................DOWN
�� WHEN L/G DOWNLOCKED:
L/G LEVER................................................................... DOWN
�� WHEN L/G DN:
MAN PITCH TRIM............................................................USE
As Direct law becomes active at landing gear extension, the
Automatic Trim is inoperative.
LDG DIST PROC................................................................APPLY
ALTN LAW: PROT LOST
INCREASED FUEL CONSUMP
• Only in case of GEN or ENG failure. For this purpose, BUS
TIE pb must be switched back to AUTO:
CONSIDER APU GEN USE
ENG HI IDLE
ENG 1 N1 DEGRADED MODE
ENG 2 N1 DEGRADED MODE
INOP SYS
F/CTL PROT
PRIM 2+3
RA 1+2
AP 2
VHF 2+3
HALF SPLRS
REVERSERS
ADR 2
See (1)
CAT 2
N/W STRG
MOST F PUMPS
See (1)
GPS 2
Note: STATUS is
simplified in
ELEC EMER
　
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