FUEL SYSTEM Flashcards
Where is the fuel stored?
Two integral wing tanks.
How many pumps are found in each tank and what are they called?
Three; one ejector pump, one scavenge ejector pump, one electric fuel boost
pump.
What is normally used to supply fuel from the wing to the engine fuel control
unit in flight?
Ejector pumps.
How is the primary fuel ejector pump powered?
Motive flow from the respective engine.
What is the primary purpose of the scavenge jet pump?
Maintains the fuel level in the collector tank ensuring a constant flow of fuel to the
engine during normal flight.
When is the electric fuel pump activated if in the auto position?
Engine start, crossfeed operation, if primary ejector pump fails.
What ensures that the differential pressure between the tank and ambient
remains within structural limits and prevents fuel spillage?
A vent system including a NACA air inlet/outlet.
How is crossfeeding performed?
Select the XFEED switch to the wing tank with the low fuel quantity
(LO 1 or LO 2). This opens the XFEED valve and turns on the electric DC pump in
the wing tank with the highest level of fuel. Both engines will utilize fuel from that
tank.
What is the restriction on crossfeed operation?
Shall not be performed during takeoff and landing.
When fuel becomes balanced and the XFEED valve is still open, what CAS
message will be annunciated?
“FUEL EQUAL”.
Will the total tank quantity indication be lost if only one wing tank quantity
indicator fails?
Yes.
The fuel shutoff valves are normally open. What is the only way to close one of
these valves?
By pushing the fire shutoff pushbutton.
What would cause a “FUEL LO LEVEL” CAS message?
310 lbs of fuel remaining in the respective tank.
What would cause a “FUEL IMBALANCE” CAS message?
220 lbs imbalance.
Is there de-fueling capability?
Yes, by means of a dump valve located under each wing.
