Day 1 Progress Check Flashcards

1
Q

Which of the following auxiliary lift devices is primarily used to increase lift during takeoff and improve handling characteristics at low airspeeds?

A

Slats

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2
Q

Dynamic stability deals with the tendency of a displaced body to return to equilibrium.

A

F

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3
Q

What is the law of conservation of energy?

A

Energy can neither be created nor destroyed.

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4
Q

Spoilers are used to increase lift and improve handling characteristics at low airspeeds.

A

F

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5
Q

What force is responsible for moving an aircraft forward?

A

Thrust

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6
Q

Parasite drag can be completely eliminated by streamlining the shape of the aircraft.

A

F

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7
Q

Which control surface is responsible for controlling the pitch of an aircraft?

A

Elevators

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8
Q

At sea level, what is the standard atmospheric pressure measured in pounds per square inch (psi)?

A

14.7 psi

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9
Q

What axis extends lengthwise through the fuselage from the nose to the tail of an aircraft?

A

Longitudinal axis

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10
Q

The CG (Center of Gravity) of an aircraft is the point where all the weight of the aircraft is concentrated.

A

T

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11
Q

What is the primary composition of the air in Earth’s atmosphere?

A

Nitrogen and oxygen

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12
Q

Servo tabs are designed to move in the opposite direction of the primary flight control surface.

A

F

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13
Q

What is the primary purpose of trim tabs on an aircraft?

A

To correct any tendency of the aircraft to move toward an undesirable flight attitude

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14
Q

Which of the following can increase lift on an aircraft wing?

A

Increasing the air velocity over the wing

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15
Q

What is velocity?

A

The rate of motion in a particular direction in relation to time.

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16
Q

Which control surface is responsible for controlling the yaw of an aircraft?

A

Rudder

17
Q

What is the primary purpose of winglets on an aircraft?

A

To reduce aerodynamic drag associated with vortices at the wingtips

18
Q

Air density is directly proportional to pressure and inversely proportional to temperature.

A

T

19
Q

The angle of incidence is the angle between the chord line of the wing and the direction of the relative wind.

A

F

20
Q

What is the angle between the chord line of the wing and the longitudinal axis of the aircraft called?

A

Angle of Incidence

21
Q

Which force counteracts the effects of weight and acts vertically?

A

Lift

22
Q

Bernoulli’s principle states that as the speed of a fluid increases, its pressure also increases.

A

F

23
Q

What principle explains the creation of lift due to the difference in air velocity over and under the wing?

A

Bernoulli’s Principle

24
Q

What type of stability exists when a disturbed object tends to return to equilibrium?

A

Positive static stability

25
Q

The aspect ratio is the comparison of the wingspan to the chord length, and a higher aspect ratio results in greater lift.

A

T

26
Q

What surface is primarily responsible for controlling longitudinal stability in an aircraft?

A

Horizontal stabilizer