MOD 1-2-3 Flashcards

1
Q

Which of the following best describes the operation of the generator portion of a ‘tach generator’ style of aircraft tachometer?

It produces an AC output with a frequency proportional to RPM

or

It produces an AC output with an amplitude proportional to RPM

A

It produces an AC output with a frequency proportional to RPM

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2
Q

Which electrical property is used in a solid state type of electrical tachometer system?

A

Inductance

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3
Q

Which electrical position indicating systems operate on AC (as opposed to DC)?

A

Autosyn and Magnasyn

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4
Q

Which AC position indicating system(s) uses permanent magnet rotors?

A

Magnasyn

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5
Q

What aircraft instrument functions are presented on a PFD?

A

Attitude, heading, airspeed and altitude indications

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6
Q

What is the name of the instrument in Figure

A

An EHSI

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7
Q

What item in Figure 1 is identified as item 5?

A

Course pointer

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8
Q

Which items in Figure 1 indicate failures or lack of proper signal?

A

Items 2 and 4

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9
Q

Which identified numbered item in Figure 1 is used as the reference for the aircraft heading indications?

A

Item 1

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10
Q

Which identified numbered item in Figure 1 is used as the reference for the aircraft heading indications?

A

Item 1

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11
Q

Which identified numbered item in Figure 1 indicates the selected aircraft heading?

A

Item 6

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12
Q

This must be present on an indicator if the operating range markings are applied to the glass face

A

Slippage mark

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13
Q

Rubber shock proof mounts are used to secure these in place

A

instruments panels

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14
Q

What color is the Prohibited Operation Range on an instrument face

A

red

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15
Q

You would find the regulations regarding aircraft instruments here

A

canadian aviation regulations

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16
Q

This item is located the lower centre of the T

A

heading inducator

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17
Q

Airspeed, attitude, altitude, vertical speed and this can all be displayed on an Electronic Attitude indicator.

A

radio altimeter

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18
Q

A set of flying conditions which require clear visibility outside of the flight deck

A

VFR Visual flight rules

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19
Q

This type of lighting allows the pilot to see the instrument displaywhile holding the instrument in place

A

postlight

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20
Q

This is used to inidcate a problem that requires pilot attention. This will continue until the problem is rectified.

A

anunciator lights

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21
Q

This item is located in the upper left of the T

A

air speed indicator

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22
Q

The best single engine rate of climb speed is indicated by this

A

blue line

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23
Q

This indicates a NEVER EXCEED

A

red line

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24
Q

This item is located in the Centre upper portion of the T

A

attitud indicator

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25
Flying conditions with limited visibility out of the flight deck is
IFR Instruments flight rules
26
The letter T is used to indicate this standard layout
primary flight instruments
27
Forward mounted instruments can be installed using this
expanding clamp
28
Instruments are held in place using these
brass screws
29
This is used to provide a path for current to flow from the instrument panels to the airframe
bonding straps
30
The color of a CAUTION advisory
amber
31
This unit indicates rough handling of instruments, gyros
shock watch
32
This item is located in the upper right of the T
altimeter
33
A red flashing annunciator indicates this
Master Warning
34
The color that represents the flap operating range on an airspeed indicator
white
35
You have completed your compass adjustments. You move the aircraft to 000 degress (North). The aircraft reads 004 degrees. What do you record, compass rose heading or aircraft heading?
aircraft heading
36
This is one mechanical method of temperature measurement
bimetal strip
37
When adjusting the magnetic compass on the initial reading of East, you take out this much error
full error
38
This indicator monitors the rotational speed of a reciprocating engine crankshaft
tachometer
39
Full meaning of inHg
inches of mercury
40
This type of pressure measurement is used in an airspeed indicator
differential
41
This aircraft instrument measures absolute pressure
altimeter
42
By monitoring the force that is exerted to a pressure of a known area results
gauge pressure
43
Complete this statement, Pressure as related to aircraft instruments is a _______ acting on a(n)\_\_\_\_\_\_\_.
force aerea
44
A capsule constructed of two corrugated metal dics which are soldered together
aneroid barometer (mesure atmospheric pressure from a static port )
45
This is another method of mechanical measurement, also found in mechanical pressure sensing of fliud systems
bourdon tube
46
This is one style of measurement using for monitoring rotational speed
drag cup
47
After completing the error adjustments, the aircraft is repositioned this many degress each time
thirty
48
This source of pressure can be used for both Gyro Instruments and De-Ice Boots
pneumatic
49
After completing a compass swing, this must be signed, dated and placed in view of the pilot(s)
compass correction card
50
Full meaning of psi
pounds square inch
51
This is an area that could be dedicated to complete a compass correlation check
compass rose
52
This system requires forward movement of the aircraft in order to generate a source of vacuum.
venturi
53
A compass swing needs to be carried out after a partial or complete crew change.
no
54
When adjusting the magnetic compass for the initial South heading, you take out this much error
half error
55
This is another style of measurement for monitoring a rotational speed
flight weights
56
A barometer measures this kind of pressure
absolute pressure
57
If the Autosyn synchros rotate in the same direction but are 180 degrees apart, the problem is this
rotor wiring
58
This electrical property is used to measure RPM by using no moving parts
inductance
59
This electronic system displays engine and system parameters to the pilots
EICAS
60
An AC output is created with frequency that is proportional to RPM by this device
Tachgenerator
61
This instrument electronically displays Compass information, Heading Selection, Course Selection and Navigation information
EHSI (Electronic horizontal situation indicator
62
This electrical position indicating system uses DC power
DC selsyn
63
This electrical device compares inlet pressure to outlet pressure of the engine to deterrmine engine preformance
Engine pressure ratio
64
The acronym EICAS means this
engine indicating and crew alerting system
65
This AC electrical position indicating system uses electromagnets for the rotor
AC Autosyn
66
This electronic indicator can display Airspeed, Attitude, Alttitude, Vertical Speed and Radio Altitude information
electronic attitude indicator
67
This aircraft instrument displays Attitude, Heading, Airspeed and Altitude.
PFD PRYMARY FLIGHT DISPLAY
68
This electrical circuit uses a variable resistor in its series/parallel circuit to measure temperature
Wheaston Bridge
69
On the EHSI in module 3, the green line in the center of the display indicates this
course pointer
70
This system senses high temperatures using 2 dissimilar conductors that create a small voltage
thermocouple
71
This line is used to indicate the Aircraft Heading
lubber line
72
This AC electrical position indicating system uses permanent magnets for its rotor
AC magnasyn
73
On an electronic display, selected information that is not valid will display this
red flags