Chapter 16A - Air Data Computer Flashcards

1
Q

What does the ADC do?

A

Converts pressure and temperature data into electronic signals and transmits them to the display instruments and other systems.

Pressure + temp data -> electronic signals -> display instruments

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2
Q

An Analog to Digital Converter is called a…?

A

Transducer

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3
Q

What are the three basic inputs and the auxiliary input into an ADC?

A

Pitot Pressure

Static Pressure

Total Air Temperature

Angle of Attack (alpha) (auxiliary)

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4
Q

What are the outputs of an ADC? 5 points

A
  • Altitude
  • Vertical Speeds
  • IAS / CAS / Mach Number
  • Static Air Temperature
  • Accurately calculated TAS
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5
Q

Detail the configuration module and how it fits into the Digital ADC

A
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6
Q

The purpose of the TAS input, from the air data computer, to the Inertial Navigation System is for:

A

The calculation of wind velocity

(already knows the drift)

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7
Q

What is the ADIRU?

A

Air Data Inertial Reference Unit

Combination of the IRS and ADC

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8
Q

What are some advantages of the ADC? (7 things)

A
  • Improved displays
  • Reduced instrument & lag errors
  • Error correction e.g. position error
  • Comparator system for failure indications
  • Central source for other systems
  • Lower maintenance costs – less pipes!
  • Shorter pitot / static lines
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9
Q

The principle of operation of an Air Data Computer (ADC) is the:

A

Input of pitot/static and temperature data, conversion to digital/electronic signals, correction of data, transmission to the instrument

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10
Q

An ADC can of cannot feed an ‘analogue’ instrument?

A

Can

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11
Q

If the Air Data Computer fails, what information is lost to the flight crew?

A

Wind speed and direction

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12
Q

An air data computer: Supplies the TAS to the computer of the INS.?

A

True

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13
Q

An air data computer: Determines the Mach number, the outside (static) air temperature.?

A

True

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14
Q

An air data computer: Receives the static pressure and the total pressure.?

A

True

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