Pumps
Indicator & Gauges
System Components
Procedures
Operation
100

A fuel pressure relief valve is required on ____ ____ _____ type fuel pumps. 

engine driven vane 

100

Fuel quantity is measured in pounds instead of gallons, because fuel volume varies with ____ change.

temperature 

100

A fuel strainer or filter must be located between the _____ ____ and the _____ _____ device. 

Tank outlet and the fuel metering device.

100

Aircraft _____  should be in the open air for good ventilation.

 defueling

100

Fuel lines are routed away from heat and sharp bends to prevent _____ _____.

Vapor lock.

200

Most large aircraft reciprocating engines are equipped with which type of engine driven fuel pump?

______ ______ type fuel pump

Rotary vane

200

____ turbine fuel filter has the greatest filtering action.

Micron

200

The engine fuel shutoff valve usually located aft of the _________.

 firewall

200

A fuel pressure warning switch closes and turns on the warning light when the fuel pressure ____ ____ specified limits.

drops below 

200

Regarding fuel pressure gauges:

(1) They are differential pressure indicators.

(2) They indicate fuel pressure entering the carburetor.

Both no. 1 and no. 2 are true.

300

The purpose of an engine-driven fuel pump bypass valve to prevent a damaged or inoperative pump _____ the fuel flow of another pump in series with it. 

blocking 

300

The method used on turbine aircraft to detect fuel approaching icing conditions is the _____ _____ indicator.

Fuel temperature

300

Fuel crossfeed systems are used to maintain _____ _____.

aircraft stability.

300

____ _____ mechanism unit is generally adjusted to change the fuel pressure warning limits.

Pressure sensitive 

300

Kerosene is used as turbine engine fuel because is has more heat energy per gallon and ______ fuel system components. 

lubricates

400

T/F : The centrifugal type pump is classified as a positive displacement pump.

False

400

A float-operated transmitter installed in a fuel tank sends an _____ signal to the fuel quantity indicator.

electric


400

The purpose of a flapper valve in a fuel tank is to act as _____ ______.

check valves.

400

The ____ _____ manual's are necessary to troubleshoot a fuel pressure warning system.

 manufacturer’s maintenance

400

The ___ ____ warning would give the first positive indication a tank changeover is needed.

Fuel pressure

500

_____ _____ provides a positive flow of fuel to the engine pump in a fuel system.

Boost pumps 

500

In an electronic fuel quantity system, the tank sensing unit is a _____.

Capacitor 

500

_____ _____ must be interconnected when using a gravity-feed fuel system from more than one tank.

Tank airspaces 

500

The fuel pressure taken for the pressure warning signal on most engines is the fuel pressure line of the ______.

 carburetor.

500

On pressure refueling:

(1) A single receptacle allows one person to fuel/defuel all tanks.

(2) Light aircraft have more advantages with pressure fueling.


Only no. 1 is true.