AMT 2102 Flashcards

(88 cards)

1
Q

Give the three (3) instruments that relies on the Pitot Static System.

A
  1. Altimeter
  2. Vertical Speed Indicator
  3. Airspeed Indicator
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2
Q

What does the Airspeed Indicator measure?

A

Pressure Differential

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3
Q

The indicated airspeed is ______ to the dynamic pressure

A

Directly Proportional

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3
Q

It indicates the speed of an aircraft in relation to the air.

A

Airspeed Indicator

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4
Q

This sensing system collects data covering a wide range of area and inaccessible locations.

A

REMOTE SENSING INSTRUMENTS

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5
Q

The error that causes to have an inaccurate indication because of the minor flaws in the installation and gears of the instrument

A

INSTRUMENT ERROR

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6
Q

What is the actual airspeed in relation to the ground

A

GROUND SPEED

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7
Q

It has a lag error when an aircraft made a rapid climb/descent. Usually the delay is between 1-4 SECONDS

A

VSI

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8
Q

The Airspeed Indicator has a ____?

A

density error

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9
Q

When the density of air is ___, the IAS is also ____?

A

LOW

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10
Q

Total Pressure - Static Pressure = ?

A

Dynamic Pressure

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11
Q

As the dynamic pressure increases, what happens to the diaphragm?

A

Expands

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12
Q

Static Pressure + Dynamic Pressure = ?

A

Total Pressure / Constant Pressure

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13
Q

If the dynamic pressure reduces, what will happen to the diaphragm?

A

Contracts

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14
Q

It does not include any correction

A

Indicated Airspeed

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15
Q

Small manufacturing imperfections and gear wear of the instrument

A

Instrument Error

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16
Q

Pitot-Static System errors in pressure measurement due to maneuvers or changes in aircraft configuration.

A

Position Error

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17
Q

Indicated speed (IAS) corrected for instrument and position errors.

A

Calibrated Airspeed

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18
Q

The manufacturer will publish a _____ in the aircraft manual to determine the (calibrated airspeed) CAS based on a certain configuration and (indicated airspeed) IAS

A

Calibration Table

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19
Q

In the design of the pitot-static system, air is assumed to be an ideal (incompressible gas)

A

Compressibility Error

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20
Q

It is the calibrated airspeed (CAS) corrected for air compressibility errors.

A

Equivalent Airspeed

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21
Q

The dynamic pressure depends not only on the airspeed, but also on the density of the air.

A

Density Error

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22
Q

It is the airspeed corrected for density error (temperature and pressure.

A

True Airspeed

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23
Q

The higher the altitude, the lower the ______

A

Air Density

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24
It is the actual aircraft speed in relation to the ground.
Groundspeed
25
The instruments used in controlling the aircraft’s flight attitude, altitude, speed, and direction are known as the?
Flight Instruments
26
Designed to measure operating parameters of the aircraft’s engine(s).
Engine Instruments
27
Contribute information used by the pilot to guide the aircraft along a definite course.
Navigation Instruments
28
Pressure exerted by the atmosphere. We feel this all the time
Static Pressure
29
Caused by movement through the air. As the speed increases so does the?
Dynamic Pressure
30
The function of this is to gather and distribute various air pressures for flight instrumentation.
Pitot Static System
31
Usually beneath a wing. In free-stream airflow. Often heated to avoid the entrance being blocked by ice
Pitot Tube
32
This needs to be in a free stream air flow to provide an accurate measurement as possible.
Pitot Tube
33
Usually on the side of the fuselage. Out of airflow. Some aircraft have 2 to average out reading and reduce errors
Static Vent / Static Port
34
This is designed to protect the pitot tube from moisture and dirt entering the pitot tube.
Baffled Plate / Baffle Plate
35
It is at the back of the chamber, allowing moisture to escape.
Drain Hole
36
The VSI must receive information from what to have an indication?
Static Port
37
The component of Pitot Static System is provided in some aircraft to provide static pressure should the primary static source become blocked?
Alternate Static Source
38
The instrument that indicates how high the aircraft is.
Altimeter
39
3 types of Altimeter
Barometric Altimeter, Radio Altimeter (Radar Altimeter), and GNSS Altimeter
40
Determine altitude by measuring air pressure.
Barometric Altimeter
41
In Barometric, As altitude increases, air pressure ______?
Decreases
42
What type of an Altimeter that sends a radio or laser signal toward the surface and measure the time it takes for the signal to bounce back?
Radio Altimeter (Radar Altimeter)
43
Determine altitude by using satellites to calculate altitude.
GNSS Altimeter
44
As altitude increases: The static pressure outside the aneroid gradually decreases. Since the pressure inside the aneroid capsule ____?
Expand
45
Vertical distance between mean sea level and a point in the air
Altitude
46
Vertical distance between a point on the ground and a point in the air.
Height
47
What is the vertical distance between mean sea level and a point on the ground.
Elevation
48
The concept of _____ also corresponds to a certain vertical distance
Flight Level
49
High Static Pressure = ?
Low Altitude
50
Low Static Pressure = ?
High Altitude
51
Interpret changes in pressure as changes in
Altitude
52
Uses input data from static port because it utilize static pressure to determine vertical distance between the aircraft and a reference level
Altimeter
53
If the altimeter senses a static pressure at exactly 29.92 InHg, it will read ______.
Zero Feet
54
As the aircraft climbs, pressure decreases. Therefore, the altimeter will indicate an increase in ______?
Altitude
55
The altimeter compares the actual static pressure with the _____?
Sea Level Pressure
56
A stack of sealed _____ comprise the main component of the altimeter.
Aneroid Wafers
57
An aneroid wafer is a sealed wafer that is evacuated to an internal pressure of ____?
29.92 inches of mercury / 1013HPA
58
At sea level, the altimeter indicates ______ ?
Zero Feet
59
The ______ causes the aneroid capsule to expand.
Pressure Differential
60
As altitude decreases: The static pressure outside the aneroid gradually increases causing the aneroid capsule to _____ again.
Contract
61
The barometric reference to be used by the altimeter can be set through the ______ (InHg ; hPa)
Kollsman Window
62
In altimeter needles, short needle reads
Thousands of feet
63
In altimeter needles, long needle reads
Hundreds of feet
64
This feature helps the pilots to quickly distinguish between altitudes in thousand and hundreds of feet.
Crosshatch Flag / 10,000 ft FLAG
65
Indicates the rate at which the aircraft climbs or descends. Also known as rate-of-climb indicator
Vertical Speed Indicator
66
VSI is the instruments that measures
Changes in altitude
67
VSI instrument can be divided into two parts into upper and lower parts, the upper part is called
Rate of Climb
67
VSI instrument can be divided into two parts into upper and lower parts, the lower part is called
Rate of Descend
68
Although the VSI operates solely from static pressure, it is a ____ instrument.
Differential Pressure
69
It contains a _______ with connecting linkage and gearing to the indicator pointer inside an airtight case
Diaphragm
70
The _____ of the diaphragm is connected directly to the static line of the pitot-static system.
Inside
71
The ______ the diaphragm, which is inside the instrument case, is also connected to the static line but through a restricted hole
Area outside
72
In level flight, The static pressure inside and outside the diaphragm are?
Equal
73
As pressure decreases, the static pressure inside the diaphragm/ capsule _____ immediately compares to the pressure in the instrument case due to the calibrated leak which restrains the static pressure to get out.
Decrease
74
Delay in the instrument indication due to rapid changes in climb / descent rate. Usually the delay is between 1 and 4 seconds
Lag Error
75
This prevents icing on the pitot tube.
Heater
76
The VSI has a lag error when an aircraft made a rapid climb/descent. Usually the delay is between how many seconds?
1-4 SECS
76
Give the three (3) instruments that Wright Brothers used on their Wright Flyer?
1. Engine Tachometer, 2. Anemometer 3. Stop Watch
77
On the Altimeter, what is the reading of the triangular needle?
Tens of Thousands of Feet
78
On the airspeed indicator, the static pressure is subtracted to what in order to obtain the dynamic pressure?
TOTAL PRESSURE
79
The Airspeed Indicator has a density error. When the density of air is low, what is the IAS?
LOWER IAS
80
What does the head wind do to an aircraft?
PUSHES THE AIRCRAFT
81
What is the instrument that measures the changes in altitude?
VERTICAL SPEEDINDICATOR
82
The devices and systems installed in an aircraft to provide essential information to the pilot about the status and performance of the aircraft while in flight
AIRCRAFT INSTRUMENTS
83
In airspeed indicator, what is the relationship of dynamic pressure to the speed of the aircraft?
DIRECTLY PROPORTIONAL
84
In vertical speed indicator, what is the relationship of static pressure to the altitude of the aircraft?
INVERSELY PROPORTIONAL
85
ELEVATION + HEIGHT WILL RESULT IN GETTING THE?
ALTITUDE