曝光台 注意防骗
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Due to the increased noise level, pay particular attention to visual warnings.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A318/A319/A320/A321 FLEET PRO-ABN-80 P 68/182
FCOM 19 AUG 10
COCKPIT WINDSHIELD/WINDOW ARCING
Applicable to: ALL
Affected WINDOW/WINDSHIELD ANTI ICE C/B........................................................................PULL
In case of electrical arcing, pull the circuit breaker of the affected window/windshield heating system
on the rear C/B panel:
ANTI ‐ ICE L WHSLD AF10 C/B (123VU).
‐ ANTI ICE R WHSLD AF03 C/B (123VU).
‐ ANTI ICE L WINDOWS X14 C/B (122VU).
ANTI ICE ‐ R WINDOWS W14 C/B (122VU).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A318/A319/A320/A321 FLEET PRO-ABN-80 P 69/182
FCOM 19 AUG 10
ECAM ADVISORY CONDITIONS
Applicable to:
SYSTEM CONDITIONS RECOMMENDED ACTION
CAB VERTICAL SPEED
V/S > 1 800 ft/min
CPC changeover is recommended:
MODE SEL: MAN
Wait 10 s then:
MODE SEL: AUTO
CAB ALTITUDE
altitude ≥ 8 800 ft
MODE SEL: MAN
CAB PRESS Manual pressure control
CAB DIFF PRESS
ΔO≥04ORHhmogrd6
LDG ELEV: ADJUST
If unsuccessful:
MODE SEL: MAN
Manual pressure control
ELEC
IDG OIL TEMP ≥ 147 °C Reduce IDG load if possible (GALLEY or GEN OFF).
If required, restore when temperature has dropped.
Restrict use of generator to short time, if temperature rises
again excessively.
Difference between wing fuel quantities
greater than 1 500 kg (3 307 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
Fuel temp greater than 45 °C in inner cell,
or 55 °C in outer cell
GALLEY: OFF
FUEL
Fuel temp lower than -40 °C in inner or
outer cell
Consider descending to a lower altitude and/or increasing
Mach to increase TAT.
FLAP OPEN
Flap not fully closed when APU master
switch is off.
EGT > EGT MAX - 33 °C (inhibited during
APU start)
APU
OIL QTY (message LOW OIL LEVEL
pulsing)
If there is no oil leak, then the remaining oil quantity allows
normal APU operation for about 10 h.
ENG
OIL PRESS
Yip < 16 PSI If oil pressure ‐ is between 16 and 13 PSI
(advisory), continue normal operation.
‐ If oil pressure is below 13 PSI (red indication) without
the ENG OIL LO PR ECAM warning, continue normal
engine operation (it can be assumed that the oil pressure
transducer is faulty).
In both cases, monitor other engine parameters especially oil
temperature and oil quantity.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A318/A319/A320/A321 FLEET PRO-ABN-80 P 70/182
FCOM 19 AUG 10
Continued from previous page
OIL PRESS
P > 90 PSI
Monitor other engine parameters closely for symptoms of
engine malfunction.
If high oil pressure is not accompanied by other abnormal
indications operate engine normally for remainder of flight.
Record high oil pressure and corresponding N2 readings for
maintenance action.
OIL TEMP
T > 140 °C
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 the 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
< 3 qt
If oil quantity low at high power setting, expect level increase
after power reduction
NAC TEMP ≥ 240 °C Monitor engine parameters and crosscheck with other engine
VIBRATION
N1 ≥ 6 units
N2 ≥ 4.3 units
Refer to PRO-ABN-70 HIGH ENGINE VIBRATION.
Note : The advisory threshold may be decreased by a MCDU
procedure at the level of vibration reached during the last
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 11(51)
