Basics Flashcards

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1
Q

FAA Advisory Circulars are available to all pilots and are obtained by

A

Downloading them from the FAA website

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2
Q

FAA advisory circulars containing subject matter specifically related to Airspace are issued under which subject number?

A

70

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3
Q

An airplane said to be inherently stable will

A

Require less effort to control

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4
Q

As an airplane’s CG moves aft, the airplane becomes

A

Less stable at all airspeeds

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5
Q

What is the purpose of the rudder on an airplane?

A

To control yaw

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6
Q

What determines the longitudinal stability of an airplane?

A

The location of the CG with respect to the center of lift.

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7
Q

One of the main functions of flaps during approach and landing is to

A

Increase the angle of descent without increasing the airspeed.

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8
Q

After takeoff, which airspeed should the pilot use to gain the most altitude in a given period of time?

A

Vy

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9
Q

Trim systems are designed to do what?

A

They relieve the pilot of the need to maintain constant back pressure on the flight controls.

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10
Q

To minimize the side loads placed on the landing gear during touchdown, the pilot should keep the…

A

longitudinal axis of the aircraft parallel to the direction of its motion.

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11
Q

Longitudinal stability refers to an aircraft’s stability about which axis?

A

Lateral

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12
Q

Which would provide the greatest gain in altitude in the shortest distance during a climb after takeoff?

A

Vx

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13
Q

What causes an airplane (except a T-tail) to pitch nosedown when power is reduced and controls are not adjusted?

A

The downwash on the elevators from the propeller slipstream is reduced and elevator effectiveness is reduced.

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14
Q

FAA advisory circulars containing subject matter specifically related to Air Traffic Control and General Operations are issued under which subject number?

A

90

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15
Q

Changes in the center of pressure of a wing affect the aircraft’s

A

aerodynamic balance and controllability.

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16
Q

What is one purpose of wing flaps?

A

allow the pilot to make steeper approaches to a landing without increasing airspeed.

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17
Q

In comparison to an airplane with a conventional tail, a T-tail airplane (such as a Diamond DA-40) is

A

more susceptible to stall recovery difficulties because the elevator is above the propeller slipstream.

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18
Q

Loading an airplane to the most aft CG will cause the airplane to be

A

Less stable at all speeds

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19
Q

An airplane has been loaded in such a manner that the CG is located aft of the CG limit. One undesirable flight characteristic a pilot might experience would be

A

Difficulty in recovering from a stall

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20
Q

An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would be

A

Difficulty in recovering from a stalled condition

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21
Q

FAA advisory circulars containing subject matter specifically related to Airmen are issued under which subject number?

A

60

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22
Q

An aircraft’s 100-hour inspection was due at 3302.5 hours. The inspection was actually performed at 3309.5 hours. When is the next 100-hour inspection due?

A

3402.5

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23
Q

Your airplane underwent an annual inspection on June 15 of last year. When is the next annual inspection due?

A

June 30th this year

24
Q

Where might the aircraft’s Operating Limitations be found?

A

Onboard the aircraft, usually in the Pilot’s Operating Handbook and required placards.

25
Q

What are Primary Controls

A

Ailerons, Elevator (or stabilator), Rudder

26
Q

What are the secondary controls?

A

Flaps, trim tab, spoilers (in some aircraft)

27
Q

What is CG

A

Center of Gravity

28
Q

What is CL

A

Center of Lift

29
Q

What is Vx

A

Best angle of climb (slower)

30
Q

What is Vy

A

Best Rate of Climb (faster)

31
Q

What are the two types of Drag?

A

Parasite and Induced

32
Q

What are the four forces

A

Weight, lift, thrust, drag

33
Q

Lift equals weight and thrust equals drag in ____________ flight

A

Unaccelerated

34
Q

The longitudinal axes runs __________ to _________

A

Tail to nose

35
Q

Longitudinal axes control

A

Roll

36
Q

What control is associated with the longitudinal axes

A

Ailerons

37
Q

Lateral axes runs ______ to _______

A

Wing to wing

38
Q

What motion is on the lateral axes?

A

Pitch

39
Q

What control is used for the lateral axes?

A

Elevators

40
Q

Vertical axes runs ______ to _______

A

Top to bottom

41
Q

What motion is along the vertical axes?

A

Yaw

42
Q

What controls are used along the lateral axes?

A

Rudders

43
Q

Definition of airfoil

A

An object that produces and aerodynamic force when moved through a fluid

44
Q

Airfoil produces ______

A

Lift

45
Q

Wider edge of airfoil

A

Leading edge

46
Q

Thinner edge of airfoil

A

Trailing edge

47
Q

Curved side of airfoil

A

Camber

48
Q

Line from leading edge to trailing edge

A

Chord

49
Q

Relative wind is _________ of direction of flight

A

Opposite

50
Q

Angle of attack

A

Angle defined by the wings chord line and relative wind

51
Q

A ___________ angle of attack is required for lift

A

Positive

52
Q

Critical angle of attack

A

When airflow cannot follow the curve of the wing

53
Q

What causes a stall

A

Exceeding critical angle of attack

54
Q

Bernoullis principal

A

When the speed of a fluid is increased, pressure decreases

55
Q

When the speed of a fluid _________
Pressure __________

A

Increases
Decreases

56
Q

What lifts a wing?

A

Air pressure differential

57
Q

Newton’s third law

A

Every action has an opposite and equal reaction