Avionics System Overview Flashcards

1
Q

Explanation of Primary Flight Display

A

Primary display of aircraft flight parameters for VRF and IRF

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2
Q

Explanation of Secondary Flight Display

A

Backup flight reference

Provides secondary data for display in case primary data source failure

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3
Q

Explanation of Engine Monitoring Display

A

Permanently visible backup display for engine and aircraft system information

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4
Q

What are the 5 Pages of MFD

A
  • SYS Page
  • WARN Page
  • NAV Page
  • INST Page
  • OPS Page
  • MNT Page
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5
Q

4 Modes in Head-up Display

A
  • En-route Navigation
  • Approach Navigation
  • Air-to-Air
  • Air-to-Ground
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6
Q

3 Functions of HUD

A
  • Navigation Functions
  • Tactical Navigation Function (MSN)
  • Simulated Attack Function (MSN)
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7
Q

5 Functions of Flight Management System

A
  • RNAV (Area Navigation)
  • Back-up Radio Turning
  • Back-up Navigation Aids Controller
  • Back-up ATC Transponder Controller
  • Back-up Communications System Volume Controller
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8
Q

6 Functions of UPCP

A
  • VOR/ILS/DME radio navigation aids
  • Communication Radios
  • Transponder Functions
  • Tactical Navigation Moding (MSN)
  • Setting fuel system parameters
  • Control Mission Parameters
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9
Q

Function of Hand-on-throttle and Stick

A
  • PTT Radio Function
  • Airbrake and Trim Function
  • Tactical Functions (MSN)
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10
Q

What is an Angle-of-attack indexer

A

Provide user with an indication of aircraft AOA

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11
Q

What is an Air Data Computer

A

Primary interface and computer for pitot/static system and air data sensors. Information is collected and sent to navigation system, engine power management and displays and controls

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12
Q

What is Air Data Unit

A

Receives Pitot and static pressure from primary pitot and secondary static system.
Uses inputs to give an independent air data source for airspeed and altitude flight reference information to display on SFD

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13
Q

What is RADAR Altimeter

A

Gives flight crew altitude above ground level

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14
Q

What is Magnetic heading Sensor

A

Gives flight crew an independent source of magnetic heading that is shown on SFD

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15
Q

The 5 Communication Equipments

A
  • Audio Mangement Unit (AMU)
  • U/VHF Transceiver
  • Mode S Transponder
  • Emergency Locator Transmitter (ELT)
    Automatic Dependent Surveillance-Broadcast / Traffic Information Service-Broadcast (ADS-B/TIS-B) Receiver
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16
Q

What is the purpose of VOR/ILS, Tactical Air Navigation.

A

VOR:
When tuned to a VOR frequency and receiving signals from ground station, it gives bearing and ident information for display on controls and display

ILS:
When tuned to ILS frequency, receives signla form ground station, give localiser, glide slope and ident information for display on the controls and displays.

Tactical Air Navigation:
When tuned to aired VOR/ILS frequency, gives range, time to go and ident information for DME station operating on paired frequency

17
Q

3 Components of Alerting System

A
  • EICAS (Engine Indicating and Crew Alerting System)
  • DWP (Dedicated Warning Panel)
  • RIOC (Remote-Input-Output-Concentrator)