FUEL SYSTEM QUIESTIONS MADE FROM AOM VOL. 2GOOD LUCK!SANTIAGO STOCKER.
Wing tank 1.
Wing tank 2.
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(360 kg)
(630 kg)
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Collector tank
Surge tank
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Ejector pump failure.
DC electric fuel pump.
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400 kg
1000 kg
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Collector tank
Surge tank
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2800 kg
4800 kg
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Low pressure pump
Vent system
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Three
Four
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45 kg
54 kg
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AC ESS BUS.
AC BUS 1.
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Wing tank 1.
Wing tank 2.
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Venturi ejector pump (jet pump)
Wing AC electric fuel pump.
DC electric fuel pump
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It depends
Is independent
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Ejector fuel pump.
Wing AC electric fuel pump.
Three scavenge ejector pumps.
DC electric fuel pump.
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5°
15°
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Three
Six
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6550 each tank, 13100 total.
8550 each tank, 17100 total.
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Must be manually
Is automatically
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AUTO
ON
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AC ESS BUS.
AC BUS 1.
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Onside engine during engine starts and cross side engine during crossfeed operations.
Onside engine during engine starts, cross side engine during crossfeed operations and APU, when engine is not running.
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Lower
Higher
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Out
In
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Ejector fuel pump.
Wing AC electric fuel pump.
Three scavenge ejector pumps.
DC electric fuel pump.
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One
Two
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Two
One
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DC ESS BUS 2
DC ESS BUS 3
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