曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
2 Figure 13-
30-
3 Figure 13-
30-
4
FUEL DISTRIBUTION
Figure 13-
40-
1
Figure 13-
40-
2
Figure 13-
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3
FuelControlPanel -
General 13-
30-
4 FuelSystem EICASIndications 13-
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5 FuelSystem Controls -
Synoptic PageIndications 13-
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6
StandbyFuelFeedSystem 13-
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2
StandbyFuelFeedSystem -
EICASMessages 13-
40-
3
StandbyFuelFeedSystem -
Fuel Synoptic PageIndications 13-
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4
REFUELING AND DEFUELING
Figure 13-
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1 Refuel/Defuel System 13-
50-
2
Figure 13-
50-
2 Fuel System Computer 13-
50-
3
Figure 13-
50-
3 Refuel/Defuel Control Panel 13-
50-
5
FUEL QUANTITY GAUGING
Figure 13-
60-
1 Refuel/Defuel -
EICAS Messages 13-
60-
2
Figure 13-
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2 Refuel/Defuel System -
Fuel Synoptic Page Indications 13-
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3
Figure 13-
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3 Fuel System -
Menu Page 13-
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4
Figure 13-
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4 Magnetic Level Indicators 13-
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6
Figure 13-
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5 Pitch and Roll Inclinometers 13-
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7
Flight Crew Operating Manual MASTER
CSP A-
013
FUEL SYSTEM Vol. 1 13-
10-
1
Introduction REV 56, Jan 31/03
1. INTRODUCTION
The fuelsystemconsists ofthree integraltanks within the wingbox structure. Ejectorpumps andelectricalboostpumpssupplyfueltoeachengine. The fuelsystem also provides facilities for pressure refueling/defueling andgravity refueling/defueling. Powerandgravity crossflowsystems allow fueltransfer between wingtanks and also provides fueltothe auxiliarypower unit(APU).
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