TOPIC 1: TYPICAL ELECTRONIC/DIGITAL AIRCRAFT SYSTEM

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Vocabulary flashcards covering key avionics concepts and equipment from the lecture notes.

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35 Terms

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Avionics

The field of aviation electronics, i.e., the electronic systems used in aircraft.

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Digital avionics

The part of avionics that deals with digital, computerized technologies in aircraft.

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Glass cockpit

Cockpit displays presented on monitors (LCD/CRT) rather than traditional mechanical dials.

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Fly-by-wire (FBW)

A flight control concept where manual controls are replaced by electronic interfaces and computer control.

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LCD/CRTs

Display technologies used to present cockpit information on screens.

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Autopilot

An automated system that controls the aircraft to reduce pilot workload.

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Central Air Data Computer (CADC)

The first onboard computer that computes altitude, airspeed, and rate of climb from barometric data.

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ARINC 429

A standard data bus/protocol for avionics data exchange between aircraft systems.

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ARINC 739 CDU

A cockpit data interface used with flight management/display units (CDUs/MCDUs).

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CDU (Control Display Unit)

Input/output unit used to interact with flight management systems.

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MCDU (Multipurpose/Multifunction CDU)

Display/input unit used with the Flight Management Computer for flight planning data.

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AIDS (Aircraft Integrated Data System)

A networked data system that collects and distributes avionics data.

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ACARS (Aircraft Communications Addressing and Reporting System)

System for data messaging and communications between aircraft and ground/air networks.

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VOR (VHF Omnidirectional Range)

A navigation beacon used by aircraft to determine bearing to a station.

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DME (Distance Measuring Equipment)

A navigation aid that provides slant-range distance to a VOR/DME station.

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FMC (Flight Management Computer)

Integrated computer that manages flight planning, navigation, and performance data.

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CMU (Communications Management Unit)

Unit that manages aircraft communications control.

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DFDAU (Digital Flight Data Acquisition Unit)

Device that collects flight data for recording and systems monitoring.

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PFD (Primary Flight Display)

Main display showing essential flight information (airspeed, attitude, altitude, etc.).

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ND (Navigation Display)

Display showing navigational information and flight plan data.

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EFIS (Electronic Flight Instrument System)

Integrated cockpit displays (often including PFD and ND) driven by electronic data.

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MCP (Mode Control Panel)

Panel to select autopilot/flight-director modes and guidance parameters.

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EICAS (Engine Indicating and Crew Alerting System)

System that displays engine data and crew alerts.

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ECAM (Electronic Centralized Aircraft Monitor)

Airbus system for centralized monitoring of aircraft systems and alerts.

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MFD (Multifunction Display)

Display capable of showing various types of information from multiple systems.

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DSP (Display Selector Panel)

Panel to select which information source is shown on a display.

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OIT (Onboard Information Terminal)

Terminal that provides access to onboard information and data.

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RMP (Radio Management Panel)

Panel that controls aircraft radio tuning and management.

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BITE (Built In Test Equipment)

Onboard self-testing system that monitors health of avionics and reports faults.

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BIT (Built In Test)

Self-test process that checks components and subsystems.

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BIST (Built In Self Test)

Self-diagnostic test that can operate automatically within the system.

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LRU (Line Replacement Unit)

Modular component designed for quick replacement during maintenance.

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ARINC 615

Dataloader standard for maintenance data transfer and programming.

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Non-volatile memory

Memory that retains data when power is removed, used for fault logs and configurations.

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LAE (Operational Test)

Startup operational checks that verify system inputs, protection, and control circuitry.