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We have a DC fuel pump to provide pressurized fuel for normal APU operation and
engine start when AC power or the AC fuel pump is not available. (true/false) - Answer-
True
How can the aircraft be refueled? - Answer- 2 over wing manual refueling ports and 1
pressurized refueling point on the right wing
The engine fuel shutoff valves can be closed via selector knobs on the FUEL panel.
(true/false) - Answer- False
The_________ are powered by engine motive flow. - Answer- Ejector pumps
The fuel crossfeed valve automatically opens when a fuel imbalance of 800 lb occurs.
(true/false) - Answer- False
Will selecting the AC PUMP 1 (2) selector knob to any position other than auto override
the crossfeed commands? - Answer- Yes
The collector tank keeps the fuel pumps submerged, ensuring a constant fuel flow to the
respective engine (true/false) - Answer- True
How many fuel tanks does the aircraft have? - Answer- 2 integral tanks (1 in each wing)
How is the fuel tank set up, in each wing? - Answer- Collector tank in the inboard
section and a surge tank located in the outboard section
Where would the fuel system indications and parameters be displayed? - Answer- MFD
fuel synoptic page and EICAS
What would be the EICAS indication of a max fuel imbalance? - Answer- An EICAS
FUEL IMBALANCE caution is displayed when the imbalance reaches 800lb until the
imbalance is reduced to 100lb
What fuel level does the EICAS message FUEL IMBALANCE appear and when does it
clear? - Answer- 800lb, 100lb