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GPS 2
Note: STATUS is
simplified in
ELEC EMER
CONFIG. Only the
most significant
STS items are
displayed.
(1)
AL2fter LAND RECOVERY pb selection:
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 67/166
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
(GEN NOT RECOVERED OR APU GEN NOT AVAILABLE)
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 68/166
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.
L1 ALL GEN..................................................................................................................... OFF THEN ON
L2 If at any time GEN 1 or/and GEN 2 recover, or if the APU GEN is available, Refer to
PRO-ABN-24-AJ ELEC EMER CONFIG (GEN 1 or/and GEN 2 Recovered or APU GEN Available)
or Refer to PRO-ABN-24-AJ ELEC EMER CONFIG (GEN 1 or/and GEN 2 Recovered or APU GEN
Available) - FWSPAGE for the applicable ECAM procedure and status.
L1 BUS TIE.......................................................................................................................................OFF
L2 Setting BUS TIE pb-sw to OFF segregates both generator channels.
L1 ALL GEN..................................................................................................................... OFF THEN ON
VHF 1/ATC 1...............................................................................................................................USE
L2 Only VHF 1, HF 1 and ATC 1 are supplied in electrical emergency configuration.
SELCAL is inoperative.
L1 VENT 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).
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 69/166
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.
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 6(168)
