Quiz 1 Flashcards

1
Q

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

A

Longitudinal Axis

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2
Q

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

A

True

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3
Q

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

A

Bernoulli’s Principle

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4
Q

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

A

False

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5
Q

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

A

False

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6
Q

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

A

Angle of Incidence

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7
Q

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

A

Nitrogen and Oxygen

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8
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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9
Q

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

A

True

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10
Q

What is Velocity?

A

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

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11
Q

Which force counteracts the effect of weight and acts vertically?

A

Lift

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12
Q

What force is responsible for moving an aircraft forward?

A

Thrust

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13
Q

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

A

Increasing the air velocity over the wing

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14
Q

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

A

False

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15
Q

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

A

Positive static stability

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16
Q

What is the law of conservation of energy?

A

Energy can neither be created nor destroyed

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17
Q

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

A

Rudder

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18
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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19
Q

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

20
Q

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

A

Horizontal Stabilizer

21
Q

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

22
Q

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

23
Q

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

24
Q

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

25
Q

What is the primary purpose of winglets on an aircraft?

A

To reduce aerodynamic drag associated with vortices at the wingtips.

26
Q

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

27
Q

How do single-main rotor helicopters counteract torque?

A

Tail rotor and foot pedals

28
Q

What is the effect of increasing the helicopter’s speed on the rotor blades’ movement and the rotor disc’s position?

A

Blades flap and cause the rotor disc to tilt backwards.

29
Q

What is the purpose of a freewheeling unit in a helicopter?

A

Allow the rotor to spin freely if the engine fails

30
Q

What is the effect of gyroscopic precession on a helicopter’s main rotor?

A

Rotor disc tilts forward

31
Q

What happens to lift when the angle of attack (AOA) of the rotor blades is increased during vertical flight?

A

Helicopter Ascends

32
Q

During hovering flight, in which direction does a single main rotor helicopter tend to drift due to the tail rotor thrust?

A

In the direction of tail rotor thrust

33
Q

How does a dual-rotor helicopter balance aerodynamic torque?

A

Two horizontal counter-rotating rotors.

34
Q

What distinguishes a fully articulated rotor system from other rotor systems?

A

Each blade moves in three directions, pitch, lead-lag, and flap

35
Q

Which force acts upward and adjusts with rotor tilt in a helicopter?

36
Q

What is the primary purpose of rigging in helicopter assembly and maintenance?

A

Ensure the coordination and precise movement of flight controls

37
Q

What happens when the collective pitch control is raised?

A

Pitch angle of all main rotor blades increases

38
Q

What is the primary function of a stabilizer bar in a helicopter’s Bell Stabilizer Bar System?

A

Improve helicopter stability

39
Q

How does an offset flapping hinge enhance helicopter control?

A

Creating powerful moments for control with greater offset

40
Q

What is the primary method used for rotor blade tracking?

A

Using a stroboscopic light to measure blade positions

41
Q

What is the purpose of the freewheeling unit in a helicopter?

A

Disconnect the main rotor from the engine when rotor RPM exceeds engine RPM

42
Q

What is the primary function of the helicopter transmission system?

A

Transfer power from the engine to the rotors and other accessories

43
Q

What is the purpose of Stability Augmentation Systems (SAS) in helicopters?

A

Stabilize helicopters and reduce pilot workload

44
Q

How do anti torque pedals help control a helicopter?

A

Controlling the pitch and thrust of the tail rotor blades.

45
Q

Which type of engine is commonly used in training helicopters due to its simplicity and cost-effectiveness?

A

Reciprocating Engine

46
Q

What is the primary function of the awash plate assembly in a helicopter?

A

Transmit pilot controls to the main rotor blades