Aviation Flashcards

1
Q

Lift

A

Force necessary to overcome gravitational force to keep the airplane flying is termed

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2
Q

Ailerons are used primarily to

A

Roll the airplane

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3
Q

Ailerons are located

A

On the outer edge of the wings

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4
Q

Pitch makes the airplane

A

Nose tilt up and down

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5
Q

Bank makes the airplane

A

Roll, which results a turn

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6
Q

The four aerodynamic forces acting on an airplane are

A

Drag, lift, thrust and weight

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7
Q

An airplane wing is designed to produce lift resulting from relatively

A

Positive (High) air pressure below the wings surface and negative (Low) air pressure above the wings surface

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8
Q

Flight Instruments

A

Airspeed Indicator, Altimeter Attitude Indicator, Vertical Speed Indicator, Heading Indicator, Magnetic Compass, Turn Coordinator (AKA Rate of Turn Indicator), inclinometer

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9
Q

Engine Instruments

A

Tachometer, Ammeter (battery), voltmeter,

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10
Q

Altimeter

A

Altitude in MSL (based on barometric pressure)

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11
Q

Attitude

A

Artificial horizon

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12
Q

Vertical Speed

A

How many feet per minute climbing/descending

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13
Q

Tachometer

A

Engine RPM

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14
Q

Ammeter

A

Battery Power

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15
Q

Forces acting on an aircraft in a steady flight condition (no change in speed or flight path) AKA equilibrium

A

Lift equals Weight, Thrust equals Drag

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16
Q

A flashing green air traffic control signal directed to an aircraft on the surface is a signal that the pilot

A

Is cleared to taxi

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17
Q

Steady red light signal from the tower to aircraft approaching to land

A

Continue circling

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18
Q

Flashing red light signal from the tower to aircraft approaching to land

A

Airport is unsafe for landing

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19
Q

Propeller blades are curved on one side and flat on the other side to

A

Produce thrust

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20
Q

When in the down (extended) position wingflaps provide

A

Greater lift and more drag

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21
Q

What makes an airplane turn

A

Horizontal componenet of lift

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22
Q

What is one advantage of an airplane said to be inherently stable

A

Airplane will require less effort to control

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23
Q

If the elevator trim tabs on the airplane are lowered, the plane will tend to

A

Nose up

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24
Q

The pilot always advances the throttle during a

A

Climb

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25
Q

The pilot of an airplane can best detect the approach of a stall by the

A

Ineffectiveness of the ailerons and elevator, shaking/buffeting of control surfaces, stall horn noise (if stall warning equipped)

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26
Q

It is ordinarily desirable to provide an unusually long flight strip at municipal airports for the take-off of

A

Heavily loaded ships in still air

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27
Q

A closed runway is marked on an airfield diagram with

A

X X X

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28
Q

Over run is marked on an airfield diagram with

A

> > >

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29
Q

The rearward retarding force of airplane drag is opposed by

A

Thrust

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30
Q

Cowling is located

A

Around the engine

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31
Q

Airport taxiways are identified at night by omni directional edge lights in what color

A

Blue

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32
Q

If the aircraft ammeter is indicating a minus value, this means the

A

Generator or alternator output is inadequate, because the battery is discharging

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33
Q

The angle formed by the chord of an airfoil and the direction of the relative wind is called the

A

Angle of attack

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34
Q

Aircraft Structure

A

Fuselage Wings (w/ ailerons & flaps) Empennage (tail) Landing Gear Power Plant

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35
Q

Empannage Parts

A

Fixed: Vertical stabilizer and horizontal stabilizer Moveable: Rudder, elevator, trim tabs

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36
Q

Power Plant Parts

A

Engine Propeller

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37
Q

What does the cowling do

A

Helps cool the engine

38
Q

Propeller creates

A

Thrust

39
Q

What does the rudder do

A

Moves the airplane nose left and right (yaw)

40
Q

What does the elevator do

A

Moves airplane nose up and down

41
Q

Atmospheric pressure

A

Weather changes help lift airplane, actuates some flight instruments

42
Q

Air Density

A

Effects airplanes capability

43
Q

Less dense air

A

reduces power, thrust and lift

44
Q

Density

A

Decreases with altitude

45
Q

Increase temps

A

Decreases density

46
Q

Axes of Flight

A

Pitch, Roll, Yaw

47
Q

Pitch

A

Lateral Axis (thru wings) Nose & Tail up and down Elevators

48
Q

Roll

A

Longitudinal Axis (thru body) Wings up and down Ailerons

49
Q

Yaw

A

Vertical Axis (up and down) Wings side to side Rudder

50
Q

Rudder

A

Push left pedal, rudder moves left, moves tail to right and nose to the left.

51
Q

Secondary Flight Controls

A

Flaps, leading edge devices, spoilers and trim devices

52
Q

Trim Systems

A

Relieve pilot of the need to maintain constant pressure on flight controls

53
Q

Altimeter Purpose

A

One of most vital inst. in acft. Measures where acft is at in atmosphere presents as altitude.

54
Q

Altimeter Hands

A

Short: 10,000’s feet Middle: 1,000’s feet Long: 100’s feet

55
Q

Vertical Speed Indicator VSI or VVI

A

Indicates whether plane is climbing, descending or in level flight Ex: rate of climb 500fpm

56
Q

Airspeed Indicator

A

Pressure measured, different colored arcs. White-Flap operating range Green-Normal Operating Range Yellow-Caution range Red-Never exceed speed

57
Q

Turn Indicators

A

Like a “level”, if ball is uncentered aerodynamic forces are unbalanced.

58
Q

Attitude Indicator

A

Miniture airplane and horizon bar. Indicates attitude of airplane relative to the true horizon.

59
Q

Heading Indicator (aka directional gyro)

A

Basically compass, not affected by flight.

60
Q

Turn Indicator

A

If aileron & rudder mvmnts are coordinated during turn, ball remains centered.

61
Q

Magnetic Compass

A

Sets gyroscopic heading indicator. 30 degrees appears as 3.

62
Q

Basic Flight Maneuvers

A

Straight & Level Turns Climbs Descents

63
Q

Rudder moves

A

airplanes nose left and right

64
Q

Aileron moves

A

Airplane wing

65
Q

Elevator control moves

A

airplane nose up and down

66
Q

Flying by attitude

A

visually establishing airplanes attitude with reference to natural horizon

67
Q

Trim

A

Used to relieve all possible control pressures held after desired altitude has been attained

68
Q

Straight and level flight

A

Main maneuver Constant heading and altitude is maintained Wing tips even with horizon

69
Q

Level Turns

A

All 4 primary ctrls used (ailerons, elevator, throttle & rudder)

70
Q

3 Types Level Turns

A

Shallow 20 degrees Medium 20-45 degrees Steep 45+ degrees

71
Q

Empannage (cabin)

A

not considered a major component of an aircraft structure

72
Q

Moving the control wheel or stick to the right will cause the right aileron to

A

Rotate forward

73
Q

If the control wheel or stick is moved forward

A

Airspeed will increase Aircraft pitch will change

74
Q

If the left rudder is pressed then the aircraft will

A

yaw

75
Q

Mach refers to

A

speed of sound

76
Q

As the radius of a turn decreases the

A

positive g-forces are increased

77
Q

As altitude increases in order to maintain the same amount of lift an aircraft must

A

fly faster

78
Q

If a pilot is instructed to land on Rwy 27 using a straight approach, the heading should be

A

270 degrees

79
Q

When flaps are extended

A

Drag and lift increase

80
Q

Which two flight controls are used to control the rate of a turn

A

Elevator and ailerons

81
Q

An aircraft on a heading of 325 is flying

A

Northwest

82
Q

Under normal VFR conditions how much of a pilots attention should be focused on cockpit instruments

A

10%

83
Q

Large yellow X’s painted on the end of the runway indicate

A

closed runway

84
Q

The axis which extends lengthwise thru the fuselage from the nose to tail is

A

longitudinal axis

85
Q

The transponder code which indicates an in-flight emergency is

A

7700

86
Q

Climb Types

A

Normal Best rate of climb (Vy) Best angle of climb (Vx)

87
Q

An aircraft instructed to land on Rwy 23L would establish an approach heading of

A

230 degrees

88
Q

Flaps are generally used

A

during takeoff and during landing

89
Q

The tachometer

A

indicates the speed at which the engine crankshaft is rotating. Not a flight instrument!

90
Q

The pilot of an airplane can best detect the approach of a stall by the

A

ineffectiveness of the ailerons and elevator