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Note: If sufficient visibility is not granted for approach, consider AUTOLAND. If AUTOLAND
is not available, consider opening the sliding window on the PF’s side, after cabin
depressurization. To manually depressurize the cabin:
CAB PRESS MODE SEL.............................................................................................. MAN
MAN V/S CTL.........................................................................................................PULL UP
Due to the increased noise level, pay particular attention to visual warnings.
COCKPIT WINDSHIELD/WINDOW ARCING
Applicable to: ALL
Affected WINDSHIELD/WINDOW WHC reset button................................................................. PULL
In case of electrical arcing, pull the Window Heat Computer reset button that is located on the
affected side.
‐ WINDSHIELD/WINDOW LEFT SIDE - WHC 1 C/B (261 VU)
‐ WINDSHIELD/WINDOW RIGHT SIDE - WHC 2 C/B (262 VU).
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A330/A340 FLEET PRO-ABN-80 P 42/140
FCOM 19 AUG 10
ECAM ADVISORY CONDITIONS
Applicable to:
SYST CONDITIONS RECOMMENDED ACTION
CAB VERT SPD
V/S >1 800 ft/min or V/S < −1 800 ft/min
CPC changeover is recommended:
MODE SEL: MAN
AFTER 3 s:
MODE SEL: AUTO
CAB ALT
ALT ≥ 8 800 ft
MODE SEL: MAN
CAB PRESS Manual pressure control
CAB DIFF PRESS
ΔP ≥ 1.5 PSI in phase 7
LDG ELEV: ADJUST
If unsuccessful:
MODE SEL: MAN
Manual pressure control
COND
PACK LO FLOW
Pack flow not sufficient to satisfy
temperature demand
PACK FLOW: INCREASE
ELEC
IDG OIL TEMP
T > 142 °C
Reduce IDG load, if possible (GALLEY or GEN OFF).
If required, restore when the temperature has dropped.
Restrict use of the generator to a short time, if temperature
rises again excessively.
FUEL
The difference between L and R wing fuel
quantities is greater than 3 000 kg (6 614 lb)
FUEL MANAGEMENT: CHECK
If a fuel leak is suspected, Refer to PRO-ABN-28 FUEL
LEAK
For limitations, Refer to LIM-28 MAXIMUM ALLOWED WING
FUEL IMBALANCE
OXY/DOOR PAX OXY
200 < pressure < 1 200 PSI
LOW OIL LEVEL The APU may be started and operated for 15 h, if there is no
APU EGT high oil leak.
(inhibited during APU start)
ENG
OIL PRESS > 90 PSI Under cold oil condition it is permissible ‐ to exceed 90 PSI
at high power before engine warm up.
‐ An oil pressure > 90 PSI during steady-state engine
operation indicates an engine malfunction, unless all other
engine parameters are normal.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A330/A340 FLEET PRO-ABN-80 P 43/140
FCOM 19 AUG 10
Continued from previous page
OIL TEMP
140 °C < T < 155 °C for 15 min
A rise in oil temperature during normal steady-state
operation indicates a system malfunction and should be
closely monitored for other symptoms of engine malfunction.
Note: If OIL TEMP rise follows thrust reduction, increasing
thrust may reduce oil temperature.
In addition, a rise in oil temperature could be related to the
IDG oil cooling system. To reduce oil temperature rise before
limits are reached, the following are recommended:
1. Low Speed - Increase engine speed to increase fuel flow
and thereby cool IDG oil.
2. High Speed - Reduce generator load or turn off generator.
If oil temperature continues to rise, mechanically
disconnect IDG.
OIL QTY < 1.8 qt If oil quantity low at high power setting, expect level increase
after power reduction.
NAC TEMP > 240 °C Monitor engine parameters and cross check with other
engine.
VIBRATION
N1 ≥ 5.7 units
N2 ≥ 5.6 units
Refer to PRO-ABN-70 HIGH ENGINE VIBRATION
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A330/A340 FLEET PRO-ABN-80 P 44/140
FCOM 19 AUG 10
ECAM ADVISORY CONDITIONS
Applicable to: ,
SYST CONDITIONS RECOMMENDED ACTION
CAB VERT SPD
V/S >1 800 ft/min or V/S < −1 800 ft/min
CPC changeover is recommended:
MODE SEL: MAN
AFTER 3 s:
MODE SEL: AUTO
CAB ALT
ALT ≥ 8 800 ft
MODE SEL: MAN
CAB PRESS Manual pressure control
CAB DIFF PRESS
ΔP ≥ 1.5 PSI in phase 7
LDG ELEV: ADJUST
If unsuccessful:
MODE SEL: MAN
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 9(43)
