The Falcon 7X fuel storage system uses three structural tank groups. Which statement correctly describes the normal relationship between the tank groups and their consumers?, The Left-Hand tank group supplies Engine 1, the center tank group supplies Engine 2 and the Auxiliary Power Unit, and the Right-Hand tank group supplies Engine 3., The Left-Hand tank group supplies Engine 1 and the Auxiliary Power Unit, the center tank group supplies Engine 2, and the Right-Hand tank group supplies Engine 3., The Left-Hand and Right-Hand tank groups normally supply Engines 1 and 3 respectively, while Engine 2 can be supplied simultaneously from either lateral tank group., What is the primary operational purpose of pressurizing the Falcon 7X fuel tanks with Low Pressure engine bleed air?, To maintain approximately 2.9 pounds per square inch above ambient pressure so fuel supply can continue following booster pump failures and fuel vaporization is limited at altitude., To maintain approximately 4.8 pounds per square inch above ambient pressure so the jet pumps can operate independently of the booster pumps., To maintain approximately 1.0 pound per square inch above ambient pressure so the refueling valves remain closed during flight., The fuel pressurization system incorporates automatic drain valves at low points in the pressurization lines. Under which condition do these valves automatically close?, When system pressure exceeds approximately 70 hectopascals, equivalent to approximately 1.01 pounds per square inch., When system pressure exceeds approximately 215 hectopascals, equivalent to approximately 3.11 pounds per square inch., When system pressure exceeds approximately 330 hectopascals, equivalent to approximately 4.78 pounds per square inch., In the normal Falcon 7X fuel distribution system, what is the principal function of the thirteen jet pumps?, To use motive fuel supplied by the booster pumps to create a Venturi-induced suction that transfers fuel from the various tanks into the feeder tanks and maintains booster pump immersion., To provide an independent pressure source capable of supplying the engines following failure of both booster pumps in a tank group., To transfer fuel directly between the three tank groups whenever the Fuel Quantity Management Computer detects a fuel imbalance., During normal operation of a Booster Pump pushbutton, what occurs when the pushbutton is held for more than approximately 1.5 seconds?, Both the normal and standby booster pumps associated with that tank group are stopped and the OFF indication illuminates., The normal booster pump is stopped and the standby booster pump is automatically started., Both booster pumps operate simultaneously to provide maximum fuel pressure to the applicable engine supply line., In the normal fuel supply mode, which sequence correctly represents the intended emptying sequence of a Falcon 7X Left-Hand or Right-Hand tank group?, Front tank, wing outboard tank, wing middle tank, wing inboard tank, center-wing tank, feeder tank., Wing outboard tank, wing middle tank, wing inboard tank, front tank, center-wing tank, feeder tank., Feeder tank, center-wing tank, wing inboard tank, wing middle tank, wing outboard tank, front tank., The Fuel Quantity Management Computer uses fuel gauging probe information to calculate tank quantity. Which additional parameters are used to correct the measured fuel-height values?, Fuel density, aircraft attitude, wing deflection between ground and flight conditions, and tank geometry., Fuel temperature, engine fuel flow, aircraft groundspeed and tank pressurization pressure only., Aircraft pitch attitude, engine thrust setting, booster pump discharge pressure and fuel transfer valve position only., The Falcon 7X has independent indications for approximately 1000 pounds and 250 pounds of remaining fuel. Which statement correctly describes how these two thresholds are generated?, The 1000-pound level is detected by dedicated level sensors connected to the Fuel Level Control Unit, while the 250-pound level is calculated by the Fuel Quantity Management Computer from feeder-tank gauging probes., Both the 1000-pound and 250-pound levels are calculated exclusively by the Fuel Quantity Management Computer using the same feeder-tank probes., The 1000-pound level is calculated by the Fuel Quantity Management Computer, while the 250-pound level is independently detected by the Fuel Level Control Unit., During pressure refueling, which system relationship correctly describes how a full refueling operation is stopped?, The Fuel Level Control Unit uses high-level sensor information to control the applicable refueling valves, while the Fuel Quantity Management Computer is used for quantity calculation and partial-refueling control., The Fuel Quantity Management Computer directly closes all refueling valves from fuel-flow information, and the Fuel Level Control Unit is used only for cockpit low-level warnings., The Front Tank Printed Circuit Board closes all six refueling valves directly when any single high-level sensor detects fuel., During suction defueling of the Falcon 7X, how can maintenance personnel select only one tank group for defueling?, Operate only the booster pumps corresponding to the required tank group while the defueling manifold transfer path is established., Close the refueling valves of the two tank groups that are to retain fuel while operating all six booster pumps., Depressurize only the required tank group and allow fuel to flow by gravity through the pressure refueling coupling.

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