Flashcards on Aircraft Engine Fuel Systems

Aircraft Engine Fuel Systems: Comprehensive Student Guide

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Why is an aircraft reciprocating engine killed by placing the mixture control in the cutoff position rather than by using the magneto switch?

Cutting off the mixture shuts off fuel to the cylinders, leaving combustion chambers full of air with no fuel, making the engine less likely to fire i

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Aircraft Fuel and Engine Systems

12 cards

Card 1

Question: Why is an aircraft reciprocating engine killed by placing the mixture control in the cutoff position rather than by using the magneto switch?

Answer: Cutting off the mixture shuts off fuel to the cylinders, leaving combustion chambers full of air with no fuel, making the engine less likely to fire i

Card 2

Question: Where is the fuel from a continuous-flow fuel injection system discharged?

Answer: Through injector nozzles screwed into the cylinder heads near the intake valves.

Card 3

Question: In which direction relative to the wind should a jet aircraft be positioned when the fuel control is being trimmed?

Answer: (Answer not provided in the content.)

Card 4

Question: What engine parameters are sensed by the fuel control unit of a turbine engine?

Answer: Engine RPM, inlet air pressure, compressor discharge pressure, burner can pressure, and inlet air temperature.

Card 5

Question: When does the acceleration system operate on an aircraft carburetor?

Answer: When the throttle is suddenly opened.

Card 6

Question: What is the purpose of the bypass valve in an engine-driven fuel pump?

Answer: To allow fuel to flow around the engine-driven pump for starting and for emergency operation if the engine-driven pump fails.

Card 7

Question: On which side of the firewall is the engine fuel shutoff valve located?

Answer: On the side of the firewall away from the engine.

Card 8

Question: What are the three purposes for the boost pumps in an aircraft fuel system?

Answer: To provide fuel pressure for starting the engine, to pressurize fuel lines to prevent vapor lock, and to transfer fuel from one tank to another.

Card 9

Question: What kind of boost pump is used in most aircraft fuel systems?

Answer: Electrically operated centrifugal pumps.

Card 10

Question: Where does an engine-driven fuel pump direct the excess fuel from its pressure relief valve?

Answer: Back to the inlet side of the pump.