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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 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 57/166
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:
LGCIU 1, SLATS/F ‐ LAPS channel 1 are recovered.
‐ Remaining fuel pump will stop (pump 1 or stby 4)
‐ SLATS/FLAPS SLOW is displayed as information in the STS.
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 58/166
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 59/166
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 60/166
FCOM 19 AUG 10
ELEC EMER CONFIG
(GEN NOT RECOVERED OR APU GEN NOT AVAILABLE)
Applicable to:
LAND ASAP
EMER ELEC PWR.................................................................................................................MAN ON
　
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