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�� IF ICE ACCRETION:
APPR SPD...........................................................VLS +10 KT
LDG DIST PROC......................................................... APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible
FCOM.
�� WHEN L/G DOWN:
MAN PITCH TRIM............................................................USE
As Direct law becomes active at landing gear extension, the
Automatic Trim is inoperative.
ALTN LAW: PROT LOST
INCREASED FUEL CONSUMP
INOP SYS
F/CTL PROT
PRIM 2+3
ADR 2+3
RA 1+2
ANTI SKID
WING A. ICE
VHF 2+3
MOST SPOILERS
REVERSERS
CAT 2
SEC 2
N/WSTRG
MOST F PUMPS
See (1)
F CTR PUMPS
GPS 1+2
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 43/166
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
(GEN NOT RECOVERED OR APU GEN NOT AVAILABLE)
See (1)
CTR TK UNUSABLE IF < 15 T
CTR TO INR: MAN ONLY
ENG HI IDLE
MCDU BACK UP NAV AVAIL
Note: Disregard the
procedure
"-T TANK
MODE...FWD",
displayed when
SPD>270 kt,
NOT IN CLIMB
and LAND
RECOVERY pb
not selected ON.
The TRIM TANK
transfer process is
automatic.
STATUS is
simplified in
ELEC EMER
CONFIG. Only the
most significant
STS items are
displayed.
(1)
AL2fter LAND RECOVERY pb ON selection:
ILS 1, LGCIU 1, SLATS/FLAPS ‐ channel 1 are recovered.
‐ Remaining fuel pump will stop (pump 1 or stby 4)
‐ SLATS/FLAPS SLOW is displayed as information in the STS.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 44/166
FCOM 19 AUG 10
ELEC EMER CONFIG
(GEN NOT RECOVERED OR APU GEN NOT AVAILABLE)
Applicable to:
LAND ASAP
EMER ELEC PWR.................................................................................................................MAN ON
L2 Display only if EMER GEN not automatically coupled.
L1ALL GEN..................................................................................................................... OFF THEN ON
L2 If at any time any GEN recover, or if the APU GEN is available, Refer to PRO-ABN-24-AI ELEC
EMER CONFIG (All GEN Recovered or APU GEN Available) and Refer to PRO-ABN-24-AI ELEC
EMER CONFIG (All GEN Recovered or APU GEN Available) - FWSPAGE for the applicable ECAM
procedure and status.
L1BUS TIE.......................................................................................................................................OFF
L2 Setting BUS TIE pb-sw to OFF segregates all generator channel.
L1ALL GEN..................................................................................................................... OFF THEN ON
VHF 1/ATC 1 (IF EMER GEN SUPPLIED BY ENG. HYD. PUMPS)........................................... USE
VHF 1 (IF EMER GEN SUPPLIED BY RAT)............................................................................... USE
L2 SELCAL is inoperative.
L1VENT EXTRACT........................................................................................................................OVRD
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).
L1 LDG ELEV............................................................................................................................ ADJUST
L2 Landing elevation has to be manually set since both FMGCs are lost.
L1AVOID ICING CONDITIONS
L2Wing anti ice, windshields, windows heat are lost.
Note: Engine anti ice is on regardless of pushbutton position. ‐ Fuel consumption increases by
approximately 1.5 %.
‐ Aircraft is out of trim due to the right aileron up float.
The rudder trim control remains operative despite no indication on control panel
(pedestal).
L1MAX FL.........................................................................................................................................350
MAX SPEED.............................................................................................................................../0.80
L2 Flight level and speed are limited due to the loss of redundancy for flight controls.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
　
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