Fuel Flashcards

1
Q

Crossfeed Selector Knob LOW 1 (2)/OFF

A
LOW 1 (2) - opens crossfeed valve and activates AC fuel pump, supply fuel to both engines from one wing tank
OFF - closes crossfeed valve
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2
Q

DC Fuel Pump Selector Knob AUTO/OFF/ON

A

OFF - deactivates DC fuel pump
AUTO - operates DC fuel pump according to system logic
ON - activates the DC fuel pump

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3
Q

AC Fuel Selector Knob AUTO/OFF/ON

A

OFF - deactivates associated AC fuel pump
AUTO - operates AC fuel pumps according to system logic
ON - activates the AC fuel pump

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4
Q

Each wing tank incorporates:

A
  • a collector tank

- a surge tank

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5
Q

What is the purpose of the collector tank

A

keeps fuel pumps submerged ensuring a constant fuel flow

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6
Q

Describe vent tank

A

ensures a differential pressure between tank and ambient and prevents fuel spillage during flight maneuvers, vented through vent lines and supplemented by a high capacity pressure relief valve to guard against fuel tank overpressure

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7
Q

Fuel quantity indication

A
  • thirteen electrical sensors in each tank
  • additional independent fuel low lever sensor
  • three magnetic level indicator under each wing
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8
Q

Each fuel tank contains the following pumps

A
  • ejector fuel pump
  • AC electric fuel pump
  • three scavenge ejector pumps
  • DC electric fuel pump (right tank only)
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9
Q

Describe the primary ejector pump

A
  • venturi ejector pump
  • no moving parts
  • powered by motive flow
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10
Q

The AC electric fuel pump supplies fuel to the following components

A
  • onside engine during engine starts
  • cross side engine during crossfeed operations
  • APU when engine is not running
  • backup if ejector pump fails
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11
Q

What busses power which AC fuel pump

A

left - AC BUS 1

right - AC ESS BUS

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12
Q

Describe the scavenge ejector pumps

A

three scavenge jet pumps maintain fuel level in collector tank

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13
Q

Describe the DC fuel pump

A
  • installed in right wing only
  • provides pressurized fuel for APU operation and engine start when AC pumps not available
  • powered by DC ESS BUS 2
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14
Q

When will the fuel low level warning activate

A

660 lbs remaining in associated tank

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15
Q

FUEL 1 or 2 LO LEVEL warning

A

low level senors indicate that 660 lbs of fuel remain in respective tank

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16
Q

APU FUEL SOV FAIL caution

A

shutoff valve is not in the commanded position

17
Q

ENG 1 or 2 FUEL SOV FAIL caution

A

associated shutoff valve is not in the commanded position

18
Q

FUEL IMBALANCE caution

A

indicates an imbalance of fuel between the two tanks of greater than or equal to 800 lbs. it remains displayed until the imbalance is reduced to 100 lbs

19
Q

FUEL TANK LO TEMP caution

A

temperature sensed in the left collector bay is less than or equal to -40C

20
Q

FUEL XFEED FAIL caution

A

indicates a discrepancy between the cockpit control position and either the valve position or the affected pump status

21
Q

DEFUEL SOV OPEN advisory

A

defuel shutoff valve is open

22
Q

FUEL AC 1 or 2 PUMP FAIL advisory

A

indicates a discrepancy between the commanded and actual pump state

23
Q

FUEL DC PUMP FAIL advisory

A

indicates a discrepancy between the commanded and actual pump state

24
Q

FUEL EQUAL XFEED OPEN advisory

A

the imbalance is less than 100 lbs and the crossfeed valve is open

25
FUEL FEED 1 or 2 FAULT advisory
respective AC pump is ON due to a failure in the primary engine feed system. The message will not be displayed when the respective N2 is less than idle.
26
FUEL KG-LB MISMATCH advisory
label united defined at FCU do not agree with label unit set on the EICAS
27
APU FUEL SOV CLOSED status
APU fuel shutoff valve is fully closed
28
ENG 1 or 2 FUEL SOV CLOSED status
associated engine shutoff valve is fully closed
29
FUEL XFEED SOV OPEN status
crossfeed valve is open and associated AC fuel pump is operating