ACI 2 (Mod 2) Flashcards

(54 cards)

1
Q

Different flight instruments

A
  • Attitude Indicator
  • Altimeter
  • Airspeed Indicator
  • Heading Indicator
  • Vertical Speed Indicator
  • Turn Coordinator
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2
Q

This type of instruments help pilots determine their position and navigate from one location to another

A

Navigation Instrument

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3
Q

Types of Navigation Instrument

A
  • Global Positioning System
  • VHF Omnidirectional Range
  • Automatic Direction Finder
  • Instrument Landing System
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4
Q

Provides precise location data using
satellite signals

A

Global Positioning System

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5
Q

Helps in navigating to or from a radio beacon

A

VHF Omnidirectional Range

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6
Q

Indicates the direction to a radio station

A

Automatic Direction Finder

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7
Q

Assists in landing by providing lateral and vertical guidance

A

Instrument Landing System

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8
Q

This type of instruments monitor the performance and condition of the aircraft’s engine

A

Engine instruments

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9
Q

Types of Engine instruments

A
  • Tachometer
  • Oil pressure gauge
  • Fuel flow indicator
  • Exhaust gas temperature gauge
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10
Q

Measure’s the engine RPM

A

tachometer

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11
Q

Indicates the pressure of the engine oil

A

oil pressure gauge

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12
Q

Shows the rate of fuel consumption

A

Fuel flow indicator

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13
Q

Measures the temperature of the exhaust gases

A

Exhaust gas temperature

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14
Q

These instruments keep track of various aircraft systems to ensure they are operating correctly.

A

Systems Monitoring Instruments

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15
Q

Types of Systems Monitoring Instruments

A
  • Hydraulic pressure gauge
  • Electrical system monitor
  • Cabin pressure gauge
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16
Q

Monitors the pressure in the hydraulic
system

A

Hydraulic pressure gauge

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17
Q

Displays information about the aircraft’s
electrical system, such as voltage and current

A

Electrical system monitor

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18
Q

Indicates the cabin pressure, essential for
maintaining a safe and comfortable environment for passengers

A

Cabin Pressure Gauge

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19
Q

shown on the airspeed indicator, not
corrected for altitude, temperature, or instrument error

A

Indicated Air Speed (IAS)

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20
Q

Speed of the aircraft relative to the air, corrected
for altitude and temperature

A

True Airspeed (TAS)

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21
Q

Speed of the aircraft relative to the ground, which is TAS
corrected for wind

A

Ground Speed

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22
Q

is indicated airspeed corrected for
instrument errors and position error (due to incorrect pressure at the
static port caused by airflow disruption)

A

Calibrated Air Speed

23
Q

The direction in which the aircraft’s nose is pointing, measured in degrees from North

24
Q

The actual path of the aircraft over the ground, which may differ from the heading due to wind

25
The height of the aircraft above a given reference point, usually sea level
Altitude
26
The rate at which the aircraft is climbing or descending, typically measured in feet per minute (fpm)
Vertical Speed
27
The orientation of the aircraft relative to the horizon, including pitch (nose up/down) and roll (wing up/down)
Attitude
28
The pressure exerted by the atmosphere, used in altimeters to determine altitude
Barometric Pressure
29
The difference between true north and magnetic north, which varies by location
Magnetic Variation
30
It provides essential information related to airspeed, altitude, and vertical speed
Pitot Static System
31
2 subsystems of pitot static system
- Pitot tube - Static Port
32
What flight instruments uses the Pitot static system
- Airspeed indicator - Altimeter - Vertical Speed Indicator
33
Usually mounted on the aircraft's wing or nose, positioned to face the oncoming air flow
Pitot tube
34
What does the pitot tube determine
Airspeed
35
Measures the static pressure of the ambient air.
Static port
36
Where is the static port located
Mounted on the fuselage, away from the airflow disturbance
37
What does the static port determine
- Altitude - Vertical Speed
38
How the Pitot-Static System Works?
capturing and comparing different types of air pressure
39
The pressure caused by the motion of the aircraft through the air.
Dynamic Pressure
40
Dynamic pressure is measured by the
Pitot tube
41
How is dynamic pressure used
combined with static pressure to determine airspeed
42
The pressure of the still air surrounding the aircraft.
Static pressure
43
Static pressure is measured by the
Static Port
44
How is static pressure used
Used directly by the altimeter and VSI; combined with dynamic pressure for the airspeed indicator.
45
The sum of dynamic and static pressure
Total pressure
46
What is the source of total pressure
Derived from the pitot tube
47
How is total pressure used
Calculating indicated airspeed
48
What to do during pre-flight checkers regarding the pitot static system
Check for blockages
49
What to do during in-flight monitoring regarding the pitot static system
Be aware of unusual behavior
50
What to do during post-flight inspections regarding the pitot-static system
Perform thorough checks
51
This computer, rather than individual instruments, can determine the calibrated airspeed, Mach number, altitude, and altitude trend data from an aircraft's Pitot Static System
Air Data Computer (ADC)
52
Provides primary flight instruments, including attitude, airspeed, altitude, magnetic heading, DG, VSI, AOA, G-meter, turn rate, slip/skid ball, OAT, and TAS.
Air Data/Attitude/Heading Reference System (ADAHRS)
53
What instrument uses both the pitot tube and static port
Airspeed Indicator
54
What instrument uses only static port
- Altimeter - Vertical Speed Indicator