Piston Aircraft Aerodynamic,Structure And System Mod 11B

Piston Aircraft Aerodynamic,Structure And System Mod 11B

72 Qs

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Piston Aircraft Aerodynamic,Structure And System Mod 11B

Piston Aircraft Aerodynamic,Structure And System Mod 11B

Assessment

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Easy

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Faizal Fauzi

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72 questions

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1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

which of the following control surface is used to yaw control about normal axis in an aircraft?

rudder

aileron

elevator

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

which of the following statement is true when a control column is push forward?

the nose of the aircraft would drop

the nose of the aircraft would move up

the nose of the aircraft would remain on thhe current path

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

where does the rudder located on aircraft?

trailing edge of fin

trailing edge of mainplane

trailing edge of horizantal stabilizer

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

what couse flying fault during normal flight?

change in mass of the aircraft

change in weight and centre of gravity

change in velocity and centre of pressure

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

which of the following component is used to adjust cable tension?

fairleads

end fitting

tumbuckle

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

aircraft fuel system can be classified into two board categories,that is ………………………

pump-feed and motor-feed

gravity-feed and pressure-feed

kinatec-feed and potential-feed

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

which of thee following is a tank that is part off basic structure of the aircraft ???

integral tank

bladder tank

rigid removable tank

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