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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 50/166
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 CONSUM
• 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
CTR TK UNUSABLE IF < 15 T
CTR TO INR: MAN ONLY
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/WSTRG
MOST F PUMP
See (1)
GPS 2
Note: STATUS is
simplified in
ELEC EMER
CONFIG. Only the
most significant
STS items are
displayed.
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 51/166
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
(GEN NOT RECOVERED OR APU GEN NOT AVAILABLE)
(1)
AL2fter LAND RECOVERY pb selection:
SLATS/FLAPS channel 1, LGCIU 1, BSCU 1 and WHC 1 are ‐ recovered. But FLAPS remain
lost, if ENG 2 failed and IDG 1 lost.
‐ Remaining fuel pump (L FUEL PUMP 2 or R FUEL PUMP 2) will stop.
‐ SLATS/FLAPS SLOW is displayed as information on STS.
‐ HF 1, AP 1 and ADR 3 are lost after LAND RECOVERY pb selection.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 52/166
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.
　
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