737 AQP FUEL

What is the maximum allowed random lateral fuel imbalance between tanks 1 and 2?. 1100 lbs. 1000 lbs. 800 lbs.

The fuel crossfeed valve is normally _________ . open. closed. open if the fuel quantity in the center tank is between 1000 and 5000 lbs.

For ground operation, center tank fuel pump switches must not be positioned ______________ unless the center tank fuel quantity exceeds 1000 pounds. ON. OFF.

Center tank fuel pump switches must not be positioned ON unless __________. maintenance is available. personnel are available on the flight deck to monitor low-pressure lights. center tank fuel quantity is between 500-900 lbs.

Each fuel tank uses two AC-powered fuel pumps, which are ________ and lubricated. fuel cooled. oil cooled. pneumatically cooled.

On a B737-800, the center tank pumps produce _______ pressure than the main tank pumps. higher. lower.

The engine driven fuel pumps _________________ in the event normal electrical fuel pump operation is not available. will provide suction feed. will not provide suction feed. will run on alternate DC power.

________________ close(s) whenever the/their respective engine fire warning switch is pulled or engine start lever is placed to CUTOFF. The spar fuel shutoff valve. The engine fuel shutoff valve. Both the spar fuel shutoff valve and the engine fuel shutoff valve.

When AC fuel pumps are operating, fuel for the APU is normally supplied from the ______ fuel manifold. left. right. center.

An extinguished ENGINE VALVE CLOSED light indicates the related valve is ___________. open. closed. in transit.

An illuminated (blue) _________ SPAR VALVE CLOSED light indicates the valve is closed. bright. dim. flashing.

On the forward overhead fuel control panel, the FUEL temperature (TEMP) indicator indicates fuel temperature in the _____________. No. 1 tank. No. 2 tank. center tank.

An illuminated bright blue crossfeed VALVE OPEN light indicates ____________. the crossfeed valve is in transit. the crossfeed valves position and CROSSFEED selector disagree. all answers are correct.

An illuminated (amber) FILTER BYPASS light indicates ____________. the engine is starting. an impending fuel filter bypass. an impending hydraulic filter bypass.

An illuminated (amber) FUEL PUMP LOW PRESSURE light indicates _________. the aircraft is being pressure refueled. fuel pump output pressure is low and the respective FUEL PUMP switch is ON. fuel pump output pressure is high and the respective FUEL PUMP switch is ON.

Placing the FUEL PUMP Switch ON ______________. activates the fuel pump. deactivates the fuel pump. allows for refueling.

The resetting of a tripped fuel pump or fuel pump control circuit breaker is __________. allowed. allowed one time. not allowed.

The fuel quantity indication system calculates _________ fuel quantity in each tank. the useable and unusable. the useable. the unusable.

An illuminated (amber) Fuel (LOW) indication is displayed when __________. the fuel quantity is less than 2000 lbs. in the related main tank. the fuel quantity is less than 2500 lbs. in the related main tank. the fuel quantity is less than 2676 lbs. in the related main tank.

A displayed (amber) fuel configuration (CONFIG) alert indicates ____________. center fuel tank quantity is greater than 1600 lbs. either engine running and both center fuel pump switches are positioned OFF, and center fuel tank quantity is greater than 1600 lbs. either engine running and both center fuel pump switches are positioned OFF.

An illuminated (amber) Fuel Imbalance (IMBAL) Indication is displayed when main tanks differ by more than ____________ and is displayed until imbalance is reduced to _______. 1676 lbs; 500 lbs. 1000 lbs; 500 lbs. 1000 lbs; 200 lbs.

The Fuel Flow Readout on the upper display unit displays fuel flow to engine with the FUEL FLOW switch in the RATE position ____________. in pounds per hour X 1000. in gallons per hour X 100. kilograms per hour X 100.