18LP Pilots Environment Flashcards

1
Q

What instruments are affected by the pitot static system

A

Airspeed, altimeter, vertical speed indicator

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2
Q

What are the two major parts of the pitot static system

A

The Peto tube with impact pressure chambers and lines,

static air vents with static pressure chambers and lines

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3
Q

Static air vents are the source of _______pressure

A

External atmospheric

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4
Q

What instruments are affected if the static air vents are blocked

A

All three Peto static system instruments: altimeter, airspeed indicator, vertical speed indicator

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5
Q

Pressure is sensed by a _______ in the altimeter and converted to an altitude

A

Aneroid wafer, barometer

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6
Q

What does the altimeter indicate

A

Height above sea level when set to the local altimeter setting

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7
Q

The altimeter setting of 29.92 is always used for flights at _____

A

And above 18,000 feet MSL

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8
Q

When flying from higher pressure to lower pressure the altimeter will read___.

A

A higher altitude than the actual altitude

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9
Q

When flying from lower pressure to higher pressure the altimeter will read_____.

A

A lower altitude than actual altitude

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10
Q

VSI measures what

A

The rate of climb or discent in hundreds of feet per minute

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11
Q

The VSI gives immediate indication of changes in _______and utilizes _____pressure only

A

Altitude and static pressure

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12
Q

On the airspeed indicator, what do these colors mean?

White arc, green arc, yellow arc, red line

A

White- flap operating range
Green- normal operating range
Yellow- caution range
Red line- never exceed speed

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13
Q

What is the only instrument that uses the pitot tube for information

A

The airspeed indicator

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14
Q

What is the difference in indicated airspeed and true airspeed?

A

IAS- read directly from airspeed indicator

TAS-airspeed corrected for temperature and pressure

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15
Q

What airspeed is used for flight plans that are being filed

A

True airspeed

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16
Q

True airspeed and indicated airspeed are approximately _______at sea level

A

Equal

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17
Q

Indicated airspeed becomes _____ then true airspeed as altitude increases

A

Less

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18
Q

What is the only self contained direction seeking instrument in an aircraft

A

The magnetic compass

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19
Q

This is mounted behind the glass of the instrument that can be used for a reference line when aligning the headings on the Compass card

A

Lubber line

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20
Q

What type of Compass error is this?

Angular difference between true North and direction indicated by the magnetic compass

A

Variation

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21
Q

What type of Compass error is this?

Magnetic compass error caused by electromagnetic interference with in the aircraft

A

Deviation

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22
Q

What are two types of Compass errors

A

Variation and deviation

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23
Q

What flight instruments use a gyroscope for their operation

A

Turn coordinator,
heading indicator (directional gyro),
attitude indicator

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24
Q

In some aircraft the gyros are _______, ____ or _____operated

A

Vacuum, pressure, electrically

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25
Q

What instruments would be affected if the vacuum pump failed

A

Heading indicator, attitude indicator

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26
Q

What are the two fundamental properties of a gyroscope

A

Rigidity in space and Percision

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27
Q

A body at rest will remain at rest; or if in motion in a straight line it will continue in a straight line unless acted upon by an outside force. What law is this

A

Newtons first law of motion

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28
Q

What is newtons first law of motion?

A

A body at rest will remain at rest

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29
Q

All flight instruments using the gyroscope property rely on _____ for their operation

A

Rigidity

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30
Q

What is the second property of a gyroscope

A

Percision

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31
Q

A turn coordinator is what 2 instruments combined into one

A

Rate of turn indicator and inclinometer

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32
Q

What instrument in a turn coordinator uses a gyroscopic principal for its operation

A

Rate of turn indicator

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33
Q

The inclinometer of the turn coordinator indicates the coordination of

A

The aileron and rudder

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34
Q

A standard rate of turn is _____degrees per second and the aircraft should complete a 360 in ______

A

3

2 min

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35
Q

The ball on a inclinometer indicates whether the airplane is in coordinated flight or a _____ _____

A

Slip or skid

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36
Q

The heading indicator is also referred to as

A

Directional Gyro DG

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37
Q

This is a mechanical instrument designed to facilitate the use of the magnetic compass

A

Heading indicator/DG

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38
Q

Is a heading indicator affected by the forces that make a magnetic compass difficult to interpret?

A

It is not affected

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39
Q

Because of ______caused chiefly by friction, the heading indicator creeps or drifts from a heading

A

Precession

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40
Q

The heading indicator is not a direction seeking instrument, however the ____ is

A

Magnetic compass

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41
Q

What may be obtained from the attitude indicator

A

Degrees of bank

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42
Q

What is the most realistic flight instrument on the instrument panel

A

The attitude indicator

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43
Q

Name the instruments that are used by the pilot to determine position, Course, and distance traveled
7

A
Automatic direction finder ADF
VOR instrument, 
instrument landing system ILS receiving equipment, 
radio magnetic indicator RMI
horizontal situation indicator HSI, 
distance measuring equipment DME,
 global positioning system GPS
44
Q

The automatic direction finder is used to navigate using _______

A

Nondirectional radio beacons NDBs

45
Q

What presents information to indicate bearing to or from the station

A

The VOR receiver

46
Q

This instrument consist of an Omni bearing selector OBS, course deviation indicator needle, to- from indicator, and navigation frequency tuner

A

VOR instrument

47
Q

What is a radial and a reciprocal on a VOR instrument

A

Radial- magnetic course from the station

Reciprocal- magnetic course to the station

48
Q

ILS receiving equipment is used to do what

A

Make an ILS approach

49
Q

The red localizer and glideslope warning flags appear when ________ to actuate the needles

A

Insufficient voltage is received

Also appear when an unstable signal or receiver malfunction occurs

50
Q

The radio magnetic indicator RMI is designed to receive what

A

Both VOR and NDB signals

51
Q

The RMI consist of what three things

A

Rotating compass card,
double barred bearing indicator
single barred bearing indicator

52
Q

The RMI can be set up to indicate either bearing to ____ or to ____

A

Waypoint or VORTAC

53
Q

HSI

A

Horizontal situation indicator

54
Q

The horizontal situation indicator is a combination of what three instruments

A

Heading indicator, VOR/LOC indicator, glideslope indicator

55
Q

The DME is used in conjunction with the VOR system to show the pilot the exact distance from that_____.

56
Q

The DME transmit a ________signal which is received by the DME ______antenna at the ground facility.

A

Interrogating, transponder

57
Q

This instrument provides accurate position, speed, precise time information on a continuous global basis, reported and latitude and longitude.

58
Q

The VOR course deviation needle indicate the Aircrafts position in relation to the selected______.

59
Q

The range displayed on the DME indicator is called _____range

60
Q

The NAV/COM incorporates what two radios in one unit

A

Navigation and communications radios

61
Q

Civilian transceivers operate in what frequency range?

A

VHF

Very high frequency

62
Q

What is used to set beacon codes a signed by Atc?

A

The transponder

63
Q

When a controller assigns a Beacon code to an aircraft he/she uses the word_____

64
Q

The_______ is the airborne portion of the secondary radar system

A

Transponder

65
Q

True or false

A transponder is also required to operate in certain controlled air spaces

66
Q

A transponder code consists of____ numbers, ranging from _____to_____
how many possible codes?

A

4 numbers,
0 to 7,
4096 possible codes.

67
Q

What codes are assigned only to one aircraft for identification purposes?

A

Discrete codes

68
Q

What squawk codes are used in aviation,
e.g.
7700 emergency, 1200 VFR

A

Non-discrete codes

69
Q

What has to be set on the mode C for secondary radar to receive altitude information?

A

ALT on the aircraft mode C

70
Q

This is a computer system that uses a large database to allow routes to be pre-programmed and fed into the system by means of a data loader

A

Flight management system – FMS

71
Q

The electronic flight instruments, are commonly referred to as

A

Glass cockpit

72
Q
What includes all of these  
-Primary flight display, 
-navigation display 
– engine indicating and crew alerting system (EICAS)
– multi function display (MFD)
 – primary flight display (PFD)
A

Flight management system – FMS

73
Q

What replaces the attitude indicator, altimeter, radar altimeter, airspeed indicator, and glideslope indicator?

A

Primary flight display – PFD

74
Q

The primary flight display – PFD – can be configured in what two configurations

A

Approach configuration, Cruise configuration

75
Q
What configuration is this – PFD: 
– Localizer information
 – glideslope information
 – radar altitude, not usable above 1200 feet
 – altimeter 
– DME
 – decision altitude (DA)
A

Approach configuration

-only information unique to The approach phase of flight will be displayed

76
Q
What configuration is this – PFD:
– Pressure altitude
 – indicated airspeed Mach number
 – heading
 – Course
A

Cruise configuration

- only information you need to the en route phase of flight will be displayed

77
Q

What instrument can be configured in either the full compass configuration or the segmented arc configuration?

A

The navigation display – ND

78
Q

Traffic alert and collision avoidance system

79
Q

A self-contained, airborne collision avoidance system that is intended to provide a back up for the separation services provided by Atc

80
Q

Generates traffic advisories and resolution/collision avoidance advisories in the vertical plane…
TCAS I or TCAS II

81
Q

Is TCAS and air traffic system?

A

No, but it is a system that directly affects Atc

82
Q

On what aircraft is TCAS required?

A

Most commercial, and some general aviation aircraft

83
Q

TCAS consist of what three functions?

A

Surveillance,

  • collision avoidance system (CAS) algorithms,
  • air to air coordination
84
Q

What interrogators are on the same frequency as ground radar and receives replies from the same transponder used to reply to ground interrogations?

85
Q

The surveillance function on a TCAS provides information of an intruder’s Aircrafts:
(4 things)

A

– Range
– closure rate
– bearing
-altitude and vertical speed

86
Q

TCAS has how many levels of alerting

87
Q

Traffic advisories – TAs) – are issued about _________prior to the closest point of approach – CPA)

One of the two levels of alerting (TCAS)

A

45 seconds

88
Q

Resolution advisories – (RA’s) are issued about______ prior to CPA
(TCAS II only)
One of two levels of alerting

A

30 seconds

89
Q

When an aircraft under your control informed you that it is responding to a TCAS RA, what do you do?

A

Do not issue control instructions that are contrary to the RA

90
Q

TCAS I =

TCAS II=

A

Traffic,

RA and traffic (2)

91
Q

Only aircraft with an ________ will be identified by the TCAS system

A

Operational transponder

92
Q

What occurs when the oxygen available to the body tissues is insufficient to meet their needs?

93
Q

What induces a feeling of well-being/euphoria that can prevent the pilot from recognizing it’s effects?

94
Q

Hypoxia – pilot performance can seriously deteriorate within ______minutes at _____feet

A

15 min

15,000

95
Q

What can hypoxia result in?

A

Unconsciousness and death

96
Q
What are the symptoms of
– Slow reactions
 – impaired thinking
 – unusual fatigue
 – pilot sounds intoxicated and they reflect carefree, humorous attitude
A

Symptoms of hypoxia

97
Q

If the pilot is showing symptoms of hypoxia, and has no oxygen system, suggest a dicsent below _____feet

98
Q

What occurs when there is an abnormal increase in the volume of air breathe in and out by the lungs

A

Hyperventilation

99
Q

What are the symptoms of?
– Dizziness
– nausea
– drowsiness

A

Hyperventilation

100
Q

This is the loss of proper bearings: state of mental confusion as to position, location, or movement relative to the position of the earth.

A

Spatial disorientation/vertigo

101
Q

What occurs when an aircraft returns to straight and level flight, but the pilot feels compelled to lean into an imaginary turn which is still sensed by the inner ear.?

102
Q

This occurs when a pilot in a turn makes a sudden head movement.

A

Coriolis illusion

103
Q

Components of a Pitot static system instruments:

A

Altimeter, vertical speed indicator, airspeed indicator

104
Q

self contained instruments:

A

Magnetic compass

105
Q

Gyroscopic instruments:

A

Turn coordinator
– heading indicator
– attitude indicator

106
Q

Radio/satellite instruments:

A

-ADF (NDB receiver)
-VOR
– ILS
– DME
– GPS

107
Q

Combination instruments:

A
Radio magnetic indicator :
– heading indicator
 – dual VOR/ADF display, 
horizontal situation indicator:
 – heading indicator 
– VOR or LOC indicator
 – glideslope indicator