Section I: A2.U8 Quiz Aircraft Systems

Section I: A2.U8 Quiz Aircraft Systems

27 Qs

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Section I: A2.U8 Quiz Aircraft Systems

Section I: A2.U8 Quiz Aircraft Systems

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Tiffany Getty

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27 questions

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1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which fuel system component vaporizes fuel and pushes it directly into the cylinders? (A2.U8.SA.L1)
Filler
Primer
Pump
Vent

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

An aircraft engine specifies that it requires 100LL fuel. What color avgas should be used in this engine? (A2.U8.SA.L1)
Blue
Green
Red
Yellow

3.

MULTIPLE SELECT QUESTION

30 sec • 1 pt

Which of these could occur if a fuel tank is allowed to run dry? Select all that apply. (A2.U8.SA.L1)
Engine may stop or be difficult to restart
Water could enter the tank
The fuel lines will freeze
Vapor lock may occur in the fuel lines
Requires in-air refueling

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

True or False. The aircraft must be connected to the fuel pump with a ground wire before fueling. (A2.U8.SA.L1)
True
False

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Why are aircraft fuel tanks vented to the outside? (A2.U8.SA.L1)
To let volatile gases escape
To allow excess fuel to drain out of the tank
To prevent the fuel from freezing in cold weather
To maintain atmospheric pressure inside the tank

6.

MULTIPLE SELECT QUESTION

30 sec • 1 pt

Why does a pilot drain a small amount of fuel from each sump before each flight? Select all that apply. (A2.U8.SA.L1)
To check the grade of fuel in the tank
To reduce the pressure in the tank
To ensure the tank is not overfilled
To drain the tank of fuel vapors
To clean contaminants from the tank

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

An aircraft designed to fly upside down would most likely have which type of fuel system? (A2.U8.SA.L1)
Gravity feed fuel system, because the fuel would be stored above the wings even when the aircraft is upside down
Gravity feed fuel system, because the fuel would be pumped into the engine even when the aircraft is upside down
Inverted fuel system, because the fuel would be pressurized even when the aircraft is upside down
Inverted fuel system, because the flop tube would draw from the lowest point in the fuel tank even when the aircraft is upside down

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