PT1 CHP4 Aircraft Instruments Flashcards

1
Q

What is the weight of pressure a column of air 1 sq. in. by 1 sq. in. at sea level?

A

14.7 PSI

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2
Q

What is the pressure of a column of air 1 sq. in. by 1 sq. in. at 18,000 feet?

A

7.4 PSI

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3
Q

What is the concept to remember that relates to a column of air 1 sq. in. by 1 sq. in. at sea level versus at 18,000 feet?

A

At sea level, the column of air will have a weight of 14.7 PSI and 7.4 PSI (half) at 18,000 feet. As altitude increases (the aircraft climbs), pressure decreases

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4
Q

What is the temperature, pressure and altitude on a standard day?

A

Temperature: 15°C (59°F)
Pressure: 29.92” Hg
Altitude: sea level
29.92 is referred to as the Standard Datum Plane

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5
Q

Standard atmosphere pressure at sea level is know as what?

A

1 atmosphere (atm)

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6
Q

What is the equivalent of atm/psi/in Hg when not flying in the US?

A

hPa (hectoPascals)
mb (millibars)
mm Hg (millimeters of mercury)

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7
Q

What is the rate that pressure decreases?

A

1” Hg for per 1,000 feet (28.86” Hg at 1,000 feet)

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8
Q

Which flight instruments are Pitot-Static?

A

ASI (airspeed indicator)
Altimeter
VSI (vertical speed indicator)

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9
Q

What is the Pitot-Static System?

A
  • Provides RAM air that enters the pitot tube from an opening at the front
  • Pressure accumulates in the pressure chamber provided from the RAM air (faster the speed, the faster the pressure)
  • The static port/hole will measure the outside pressure surrounded by the aircraft
  • The drain hole will drain anything unnecessary (rain/condensation)
  • The heater will melt any ice accumulation (turned by the heather switch)
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10
Q

Which flight instrument is the only instrument that solely relies on the pitot tube?

A

ASI (airspeed indicator)

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11
Q

Are the VSI (vertical speed indicator and altimeter connected to the pitot tube?

A

No

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12
Q

What does the static port measure?

A

The pressure from the outside and indicates that decrease/increase in pressure

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13
Q

Which instruments is the static port connected to?

A
  • ASI (airspeed indicator)
  • VSI (vertical speed indicator)
  • Altimeter
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14
Q

If the static port becomes clogged, what can be used?

A

Alternate static port

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15
Q

If the static port becomes clogged and you use the alternate static port, what pressure does the static port use/measure?

A

The pressure inside the cabin

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16
Q

What does the altimeter measure?

A

Indicates height of the aircraft above a reference point (usually sea level)

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17
Q

What does each needle on the altimeter indicate?

A
  • 100s (long, thick)
  • 1,000s (short, thick)
  • 10,000s (short, thin)
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18
Q

What does the long, thick needle on the altimeter measure?

A

100s of feet

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19
Q

What does the short, thick needle on the altimeter measure?

A

1,000s of feet

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20
Q

What does the short, thin needle on the altimeter measure?

A

10,000s of feet

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21
Q

What is the principle of operation of the altimeter?

A
  • Inside, there is an aneroid wafer that is contains a specific pressure (29.92)
  • The static port sends pressure to the aneroid wafer that causes it to expand or contract
  • As altitude increases/decreases, the outside pressure decreases/increases, which the static port sends lower/higher pressure inside the altimeter
  • The pressure inside the wafer remains the same (29.92)
  • The wafer will expand/contracts as the outside pressure is lower (less)/ higher (more)
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22
Q

Describe what happens inside the altimeter as altitude increases.

A
  • The outside pressure decreases
  • The static port sends lower (less) pressure inside the altimeter
  • The pressure inside the wafer remains the same (29.92)
  • The wafer will expand as the outside pressure is lower (less)
  • The instrument needles will indicate an increase in altitude
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23
Q

Describe what happens inside the altimeter as altitude decreases.

A
  • The outside pressure increases
  • The static port sends higher (more) pressure inside the altimeter
  • The pressure inside the wafer remains the same (29.92)
  • The wafer will contract as the outside pressure is higher (more)
  • The instrument needles will indicate an decrease in altitude
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24
Q

In order for the altimeter to properly measure outside air pressure, what adjustment to the instrument must be made?

A

Turn the knob on the altimeter so the Kollsman window will indicate the correct outside pressure

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25
Q

Does the Kollsman window need to be updated through the flight? Why?

A

Yes, as pressure changes at different altitudes

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26
Q

How do you find the outside pressure?

A

METAR, ATIS, or ask ATC

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27
Q

On a low-pressure day, how is the standard datum plane affected?

A

It is lowered
Ex. outside pressure on a low-pressure day is 29.72, since the pressure is .2” Hg lower than normal, the aircraft will read at 200ft without any adjustment

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28
Q

On a high-pressure day, how is the standard datum plane affected?

A

It is raised
Ex. outside pressure on a high-pressure day is 30.12” Hg, since the pressure is .2” Hg higher than normal, the aircraft will read at 0 feet without any adjustment (really -200ft but the altimeter doesn’t read negative below 0)

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29
Q

What is the rule of thumb when travelling from an area of high pressure to low pressure?

A

High (pressure) to Low (pressure) look out below

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30
Q

When flying high pressure to low pressure without adjusting the Kollsman window, how will that affect the indicated altitude?

A

The actual altitude will be lower than indicated altitude

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31
Q

What is the rule of thumb when travelling from an area of high temperature to low temperature?

A

High (temperature) to Low (temperature) look out below

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32
Q

When from flying warm air to low air without adjusting the Kollsman window, how will that affect the indicated altitude?

A

The actual altitude will be lower than indicated altitude

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33
Q

What is the margin the altimeter should be within when set to the correct altimeter setting?

A

±75 feet of airport elevation

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34
Q

What are the types of altitude?

A

Indicated, True (MSL), Absolute (AGL), Pressure, Density

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35
Q

What is indicated altitude?

A

read directly from the altimeter

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36
Q

What is true altitude?

A

vertical distance of the aircraft above sea level (MSL)

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37
Q

What is absolute altitude?

A

vertical distance of the aircraft above the ground/obstacle (AGL)

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38
Q

What is pressure altitude?

A

altitude indicated on the altimeter when set to 29.92 pressure setting, corrected for non-standard pressure

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39
Q

What is density altitude?

A

pressure altitude corrected for non-standard temperature (how the airplane feels it’s flying at)

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40
Q

Describe what the Vertical Airspeed (VSI) is.

A
  • Indicates whether the aircraft is climbing or descending
  • Rate of climb/descent is indicated in feet per minute (fpm)
  • Should indicate zero (or close) when on the ground
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41
Q

What is the principle of operation of the altimeter?

A
  • Static port is connected to two tubes, one directs pressure into the aneroid wafer, the other (calibrated leak) directs the pressure into the empty space inside the instrument
  • The static port sends pressure to the aneroid wafer that causes it to expand or contract
  • As altitude increases (climb) or decreases (descend), the pressure outside the aircraft decreases/increases, which the static port sends lower/higher pressure inside the VSI t
  • The static port also sends pressure through a tiny pinhole called the calibrated leak, which slowly releases static pressure inside the instrument around the wafer and slowly decreases pressure around the wafer
  • this results in a high pressure outside the wafer and a lower pressure inside the wafer
  • as the wafer contracts, this will indicate a positive vertical speed
  • as wing level, the calibrated leak will equalize the pressure around the wafer to be equal inside the wafer, the needle will then go back down to zero (will lag)
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42
Q

What does the airspeed indicator measure and indicate?

A

The difference between pitot and static pressures
- As the aircraft moves through the air, the pitot pressure is more than the static pressure

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43
Q

What unit or metric is speed expressed?

A

Knots (most common) or MPH

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44
Q

What are the types of airspeed?

A

Indicated, Calibrated (CAS), True, Grounspeed

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45
Q

What is indicated airspeed?

A

Read directly on the instrument

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46
Q

What is calibrated airspeed?

A

Indicated airspeed (IAS) corrected for installation error

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47
Q

What is installation error?

A

Due to the distance between the pitot tube and static port, there will be a minor loss in pressure and a minor loss of indicated airspeed

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48
Q

How do you find the calibrated airspeed (CAS) for the aircraft?

A

Use the calibration chart in the aircraft manual

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49
Q

What is true airspeed?

A

calibrated airspeed corrected for altitude and non-standard temperatures
- because air density decreases as altitude increases, the difference between pitot and static also decreases

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50
Q

What is groundspeed?

A

The actual speed of aircraft over the ground
- without wind, GS = TAS
- decreases with a headwind (move slower)
- increases with a tailwind (move faster)

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51
Q

On the ASI, what does the white arc signify?

A

flap operating range (flaps extended or retracted)

52
Q

Which arc represents the flap operating range?

53
Q

What is Vso?

A
  • Bottom of the white arc
  • Stall speed in the landing configuration (gear down, flaps extended at a certain angle)
54
Q

The bottom of the white arc, the stall speed in the landing gear configuration is which Vspeed?

55
Q

What is Vfe?

A
  • Top of the white arc
  • Maximum flap extended speed
56
Q

The top of the white arc, maximum flap extended speed is which Vspeed?

57
Q

On the ASI, what does the green arc signify?

A

Normal operating range

58
Q

Which arc represents the normal operating range?

59
Q

What is Vs1?

A
  • Bottom of the green arc
  • stall speed in specified configuration
60
Q

The bottom of the green arc, stall speed in specified configuration is which Vspeed?

61
Q

What is Vno

A
  • Top of the green arc
  • Maximum structural cruising speed
62
Q

The top of the green arc, maximum structural cruising speed is which Vspeed?

63
Q

On the ASI, what does the yellow arc signify?

A

caution range

64
Q

Which arc is the caution range?

65
Q

On the ASI, what does the red arc signify?

A

Never exceed speed Vne

66
Q

What is the never exceed Vspeed?

67
Q

What is Va?

A

Maneuvering speed, the range that depends on aircraft weight

68
Q

Maneuvering speed, the range that depends on aircraft weight is which Vspeed?

69
Q

What is Vlo?

A
  • Landing gear operating speed
  • Maximum speed for extending or retracting the landing gear
70
Q

Landing gear operating speed, maximum speed for extending or retracting the landing gear is which Vspeed?

71
Q

What is Vle?

A
  • Landing gear extended
  • Maximum speed with gear extended
72
Q

Landing gear extended, maximum speed with gear extended is which Vspeed?

73
Q

What is Vmc?

A
  • Minimum controllable speed in a twin-engine aircraft with on inoperative engine
74
Q

Minimum controllable speed in a twin-engine aircraft with on inoperative engine is which Vspeed?

75
Q

What is Vx?

A

Best angle-of-climb airspeed (Vx) gives the greatest altitude gain in the shortest horizontal distance

76
Q

The best angle-of-climb airspeed that gives the greatest altitude gain in the shortest horizontal distance is which Vspeed?

77
Q

What is Vy?

A

Best rate-of-climb airspeed (Vy) gives the greatest altitude gain in the shortest time

78
Q

The best rate-of-climb airspeed that gives the greatest altitude gain in the shortest time is which Vspeed?

79
Q

What types of pitot-static system blockage scenarios are possible?

A
  • Blocked pitot + open drain hole
  • Blocked pitot + blocked drain hole (level flight)
  • Blocked pitot + blocked drain hole (climb/descent)
80
Q

What types of static system blockage scenarios are possible?

A
  • Blocked static + open pitot
  • Blocked static (altimeter + VSI)
81
Q

What will be indicated on the ASI when the pitot tube is blocked but the drain hole is open?

A
  • Pressure/RAM air will never enter
  • Only will get static pressure
  • the ASI will show zero (0)
  • no differential pressure between RAM air and static pressure
82
Q

What will be indicated on the ASI when the pitot tube is blocked but the drain hole is closed during level flight?

A
  • The pressure inside will remain inside, will not change (increase or decrease)
  • The ASI will show the same
  • If the speed is 120 knots, it will remain 120 knots regardless if the airspeed increases or decreases
83
Q

What will be indicated on the ASI when the pitot tube is blocked but the drain hole is closed during if the aircraft accelerates or decelerates?

A
  • The pressure inside will remain inside, will not change (increase or decrease)
  • The ASI will show the same
  • If the speed is 120 knots, it will remain 120 knots regardless if the airspeed increases or decreases
84
Q

What will be indicated on the ASI when the pitot tube and drain hole are open and static port is unclogged, but there is a blockage between the tube from the pitot to the ASI when climbing?

A
  • The pressure from the pitot tube remains the same due to the blockage
  • The pressure from the static port will decrease
  • Will show an increase in airspeed
  • Works as a reserve altimeter
85
Q

What will be indicated on the ASI when the pitot tube and drain hole are open and static port is unclogged, but there is a blockage between the tube from the pitot to the ASI when descending?

A
  • The pressure from the pitot tube remains the same due to the blockage
  • The pressure from the static port will increase
  • Will show a decrease in airspeed
  • Works as a reserve altimeter
86
Q

What will be indicated on the ASI when the pitot tube is open but the static port is clogged?

A
  • The ASI will indicate an airspeed, but it will be inaccurate
  • There is no proper reference from the static port
87
Q

What will be indicated on the ASI when the pitot tube is open but the static port is clogged if the aircraft climbs?

A
  • Indicated airspeed will decrease
  • Pitot pressure will decrease but not the static pressure
88
Q

What will be indicated on the VSI and altimeter when the pitot tube is open but the static port is clogged if the aircraft climbs?

A
  • The altimeter will freeze at whatever altitude was indicate before the blockage because the pressure around the wafer will remain the same
  • The VSI will indicate zero (0) because there is no differential pressure
89
Q

Which flight instruments are Gyroscopic?

A

Turn Coordinator, Heading Indicator, Attitude Indicator

90
Q

What types of systems power gyroscopic instruments?

A

Vacuum (air) system or Electrical system

91
Q

What are the principles of gyroscopes?

A
  • Any spinning object exhibits gyroscopic properties
  • Two fundamental properties of gyroscopic action are: rigidity in space and precession
92
Q

What is rigidity in space?

A
  • As the wheel increases speed, it becomes more stable
  • The gimbal remains in place while the airplane rotates around it
93
Q

What is precession?

A
  • The tilting or turning of a gyro in response to a deflective force
  • A small force is applied whenever the aircraft changes direction
  • Instead of gyro responding at the source of the force, the result will instead occur 90° ahead of that point in direction of rotation
  • Sometimes the instruments may have some unwanted errors such as slow drifting and minor erroneous indications in the insrutments
94
Q

Which instruments are powered by the vacuum system?

A

Heading indicator and attitude indicator

95
Q

The heading and attitude indicators are powered by which system?

A

vacuum system

96
Q

Which instrument is powered by the electrical system?

A

Turn coordinator

97
Q

The turn coordinator is powered by which system?

A

Electrical system

98
Q

Describe the vacuum system?

A

It sucks air via a vacuum pump to make the gyro spin

99
Q

What is a typical vacuum system consisted of?

A
  • Vacuum air filter
  • Directly to the Heading indicator and suction gauge (indicates how much suction) then to the Attitude indicator
  • Vacuum relief valve
  • Engine-driven vacuum pump (sucks air in)
  • Overboard vent line
100
Q

What does the attitude indicator do?

A

indicates the aircraft attitude (climbing or turning)
- primary instrument for instant information

101
Q

What principle does the attitude indicator use?

A

rigidity in space

102
Q

How many degrees do each tick mark on the top of the attitude indicate?

A

1st tick: 10°
2nd tick: 20°
3rd tick: 30°
4th tick: 60°
5th tick/horizon: 90°

103
Q

How many degrees do each vertical tick mark in the center of the attitude indicate?

A

Positive 2nd bar: +10°
Positive 1st bar +5°
Horizon: level
Negative 1st bar: -5°
Negative 2nd bar: -10°

104
Q

What is the heading indicator?

A

A mechanical device designed to facilitate the use of the magnetic compass
- the compass has numerous errors that make it difficult to use in all phases of flight

105
Q

What principle does the heading indicator use?

A

rigidity in space

106
Q

What is the turn indicator?

A
  • indicates a rate of turn (yaw) and rate of role
  • contains an inclinometer (the ball)
  • indicates standard-rate turn of 3° per second
107
Q

What principle does the turn coordinator use?

A

precession

108
Q

When the ball is centered on the inclinometer, what type of turn is this?

A

A coordinated turn

109
Q

What is used to ensure a turn is coordinated?

A

use the rudder pedal to “kick the ball” and remain coordinated

110
Q

When the ball is to the right on the inclinometer, what type of turn is this?

A

a slipping turn (slip in)

111
Q

When the ball is to the left on the inclinometer, what type of turn is this?

A

a skidding turn (skid out)

112
Q

What is the magnetic compass?

A

a magnet in a kerosene-type liquid that aligns with the Earth’s magnetic field

113
Q

What flight conditions is the magnetic compass accurate?

A

straight and level, unaccelerated flight

114
Q

What errors is the magnetic compass subject to?

A
  • Variation
  • Deviation
  • Dip errors
  • Turning errors
  • Acceleration error
115
Q

What is variation?

A

The difference between the true and magnetic north, measured in degrees
- the closer North, the less variation
- varies depending on your location on Earth and is identified as East or West
- East is least (subtract), west is best (add)

116
Q

What is Deviation?

A
  • magnets align with any magnetic fields, including the ones generated by the aircraft itself
117
Q

What what the turning errors for the magnetic compass?

A
  • a tendency that lags or leads when turning to northerly or southerly headings
  • lag (slow) turning toward northerly headings
  • lead (fast) turning toward southerly headings
  • Remember UNOS*
118
Q

What does UNOS mean?

A

U-undershoot
N-north
O-overshoot
S-south

119
Q

What are the acceleration errors for the magnetic compass?

A

The compass is also affected when accelerating or decelerating while on easterly and westerly headings
* Remember ANDS*

120
Q

What does ANDS mean?

A

Accelerate
North
Decelerate
South

121
Q

What are the two main references to orientate ourselves?

A

True North and Magnetic North

122
Q

What is True North?

A

the physical Earth’s North Pole, most maps are oriented in relation to the True North

123
Q

What is Magnetic North?

A

the location of the Earth’s magnetic field’s northern position

124
Q

What does the outside air temperature gauge measure?

A

Acts as a thermometer that measures the outside temperature

125
Q

How can the outside air temperature gauge be helpful?

A

helpful to determine icing conditions or performance calculations