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Aircraft Systems

Browse Aircraft Systems terms for pilots, air traffic controllers, cabin crew and aviation learners.

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Abgastemperatur

The temperature of gases emitted by the engine exhaust, critical for monitoring engine health and performance.

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Abluftventil

A valve that regulates the discharge of air from the pressurized cabin to maintain desired cabin pressure.

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Air-Data-Inertialreferenzeinheit

An advanced aircraft system combining air data sensors and inertial reference to provide navigation and performance data.

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Air-Data-Referenz

Aircraft module collecting and providing airspeed, altitude, and temperature data from external probes.

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alternative Fahrwerksausfahrt

A backup method to deploy the landing gear using gravity, hydraulic, or manual means if the normal extension system fails.

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Autobremsanlage

A system that automatically applies braking at a selected rate during landing or rejected take-off to optimize stopping distance.

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automatische abhängige Überwachung – Rundfunk

A surveillance technology in which aircraft broadcast position and flight data, allowing real-time tracking by ATC and other aircraft.

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automatische APU-Startsequenz

A programmed series of actions by which the auxiliary power unit starts automatically and safely without crew intervention.

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Außentemperatur

The temperature of the air outside the aircraft, used in performance and anti-ice calculations.

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Avionik-Kühlsystem

A system providing airflow and temperature regulation to prevent overheating of aircraft avionics components.

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Avioniklüfter

A fan dedicated to cooling avionics equipment by circulating air through the electronics bay.

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blaues Hydrauliksystem

One of three Airbus hydraulic systems, providing redundancy for flight controls, landing gear, and other powered components.

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Bodennäherungswarnsystem

An aircraft safety system that warns pilots if the aircraft is at risk of controlled flight into terrain or obstacles.

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Bodenspoiler

Spoiler panels on the wings that fully deploy upon landing to disrupt lift and aid in braking and deceleration.

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Brandmeldeschleife

A continuous sensing circuit that detects overheat or fire in aircraft engines, APU, or cargo bays.

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Bremsentemperaturanzeige

A cockpit display or system that monitors the temperature of the main landing-gear brakes to prevent overheating.

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Bugfahrwerkslenkung

The system that allows pilots to steer the aircraft’s nose landing gear during taxi and ground operations.

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Datenlink-Kommunikation zwischen Fluglotsen und Piloten

A digital communication system enabling direct text-based exchanges between ATC and pilots via data link instead of voice.

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elektronischer Leistungsschalter

A digitally controlled switch that protects an electrical circuit from overload by interrupting power supply electronically.

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elektronischer zentraler Flugzeugmonitor

An Airbus system that displays engine, system, and alert messages for aircraft monitoring and troubleshooting.

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Entfernungsmessgerät

An aircraft navigation system providing slant-range distance to a ground station, often paired with VOR or ILS.

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erforderliche Navigationsleistung

A set of precision standards for aircraft navigation accuracy, integrity, and reliability within defined airspace or procedures.

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Feuerlöscherflasche

A pressurized container storing extinguishing agent for aircraft fire suppression in engines, cargo, or APU compartments.

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Flaperon

A combined flight control surface that functions as both aileron and flap, used on some aircraft to improve control and lift.

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Flugdirektor-Balken

Visual cues on the Primary Flight Display indicating desired pitch and roll to guide manual flight path.

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Flugmanagementsystem

An avionics system integrating navigation, performance, and flight planning for automated aircraft operation.

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Flugsteuerungshydraulikkreis

Hydraulic circuit dedicated to supplying pressure to flight control surfaces such as ailerons, elevators, and rudder.

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Flugunterstützungscomputer

A system on Airbus aircraft that provides additional functions such as yaw damping, rudder trim, and flight envelope protection.

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Flugwarncomputer

A system that processes and displays warnings and cautions to the flight crew in response to abnormal conditions.

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Fly-by-wire-System

An electronic flight control system where pilot inputs are transmitted as electrical signals to computers, which command the flight control surfaces.

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Flügel-Enteisung

A system that prevents or removes ice accumulation on the wing leading edges using bleed air or electrical elements.

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gelbes Hydrauliksystem

One of three independent hydraulic systems on Airbus aircraft, supplying power to specific flight controls, brakes, and cargo doors.

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Geländeaufmerksamkeits- und Warnsystem

Advanced system alerting pilots of hazardous terrain or obstacles using GPS and a terrain database, supplementing GPWS.

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Generator-Steuereinheit

Electronic module that manages and protects an aircraft generator, monitoring voltage, current, and system faults.

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Gesamtdrucksonde Nummer 2

Sensor measuring total (pitot) pressure at engine station 2 for air data and engine control systems.

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Gierdämpfersystem

An automatic system that prevents unwanted yaw oscillations by commanding the rudder, increasing flight comfort and stability.

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globales Navigationssatellitensystem

A system of satellites providing worldwide navigation, including GPS, GLONASS, Galileo, and BeiDou.

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grünes Hydrauliksystem

One of three independent hydraulic systems on Airbus aircraft, powering primary flight controls, landing gear, and other components.

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Hauptflugcomputer

The Boeing main computer responsible for integrating pilot inputs, aircraft data, and actuating control surfaces.

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Hilfstriebwerk

A self-contained turbine engine providing electrical and pneumatic power to the aircraft while on the ground or as backup in flight.

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Hochdruckrotordrehzahl

Rotational speed of the high-pressure compressor or core in a jet engine, commonly indicated as N₂.

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Hydraulikbehälter

A tank storing hydraulic fluid for aircraft hydraulic systems, ensuring continuous supply during all phases of operation.

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Hydraulikpumpe

A device that moves hydraulic fluid under pressure to operate aircraft systems such as landing gear, brakes, and flight controls.

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Hydraulikspeicher

A pressurized storage device that maintains hydraulic pressure and absorbs system shocks.

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Höhenruder-Querruder-Computer

A dedicated computer on Airbus aircraft that processes inputs and controls elevator and aileron surfaces.

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Höhenruder-Steuereinheit

A hydraulic actuator that converts hydraulic pressure into elevator movement, enabling pitch control of the aircraft.

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Inertialreferenzeinheit

An aircraft system providing position and attitude data by processing gyroscopic and accelerometer inputs.

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Instrumentenlandesystem

A precision approach system providing lateral and vertical guidance to aircraft during landing using radio signals.

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integrierter Antriebsgenerator

A generator that converts variable engine speed to constant frequency AC power for aircraft electrical systems.

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Kabinen-Druckregler

Automatic device that regulates cabin altitude and rate of pressure change by controlling the outflow valve.

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Kabinen-Kommunikationssystem

An integrated system enabling voice communication between cabin crew and cockpit, and among crew stations.

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Klimaanlagen

Air conditioning and pressurization units that cool, condition, and regulate the flow of air into the cabin using bleed air.

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Klimaanlagenventil

A valve that regulates the flow of bleed air into the air conditioning pack.

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Kollisionswarnsystem

An airborne safety system providing pilots with traffic advisories and resolution advisories to avoid mid-air collisions.

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Konstantdrehzahlgetriebe

A transmission device that converts variable engine speed to a constant speed for generator operation.

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Kurzwellenfunk

Radio system operating in the HF band (3–30 MHz), enabling long-distance voice communication between aircraft and ATC.

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Leistungstransfereinheit

A hydraulic unit that enables power transfer between two separate hydraulic systems without mixing their fluids.

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Mach-Trimmsystem

A system that compensates for Mach tuck by automatically adjusting stabilizer trim at high subsonic speeds.

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Master-Caution-System

A central alerting system that warns the flight crew of abnormal but non-critical system status via lights and aural tones.

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Mindestausrüstungsliste

An official list of equipment required for safe operation of an aircraft, specifying items which may be inoperative under specific conditions.

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Mischeinheit

A component that blends recirculated cabin air with conditioned air from the packs before distribution.

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mittlerer Meeresspiegel

An altitude or elevation reference based on the average sea level used as a standard for aviation altimetry.

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Mode-S-Transponder

An aircraft transponder providing selective, data-rich responses to ATC interrogations, supporting identification and surveillance functions.

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Navigationsanzeige

Electronic display showing route, waypoints, navigation aids, weather, and traffic information.

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Niederdruckrotordrehzahl

Rotational speed of the low-pressure compressor or fan in a jet engine, often indicated as N₁.

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Pitotrohr

A forward-facing tube that measures dynamic air pressure, providing critical input for airspeed indication.

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Primärfluganzeige

The main instrument display showing attitude, speed, altitude, heading, and flight director information.

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Querrudertrimmung

A flight-control adjustment that sets ailerons to correct lateral imbalance and maintain wings-level flight.

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reduziertes vertikales Trennminimum

A set of airspace procedures allowing aircraft to be separated by 1,000 feet vertically above FL290, increasing airspace capacity.

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Satellitenkommunikation

A long-range communication system using satellites, enabling cockpit and company contact beyond VHF and HF range.

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Schubautomatiksystem

A system that automatically sets and maintains engine thrust based on flight parameters and autopilot commands.

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Schubhebelwinkel

The position or angle of the thrust lever, directly corresponding to engine power demand.

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Schubumkehr

A device used to redirect engine thrust forward to assist with deceleration after landing.

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Seitenrudertrimmung

A flight-control adjustment that offsets rudder position to maintain coordinated flight and correct for yaw.

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Sicherheitsventil

A valve designed to automatically relieve excess pressure or vacuum to protect the aircraft structure.

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Sichtweite auf der Landebahn

The distance over which a pilot of an aircraft on the centre line of a runway can see the runway surface markings or lights.

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Spanndetektor

A sensor in an engine or gearbox that detects metallic particles, indicating wear or damage to internal components.

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Speedbrake-Hebel

A cockpit control that arms or actuates spoiler panels to reduce speed or rate of descent during flight and landing roll.

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Spoiler-Höhenruder-Computer

An Airbus computer managing spoilers, elevator backup, and other flight control surfaces for redundancy and flight envelope protection.

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Spoilerklappe

A hinged surface on the upper wing that disrupts airflow, reducing lift and increasing drag for roll control or descent.

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Sprengsatz-Auslöser

A small pyrotechnic device used to rapidly release fire-extinguishing agent by rupturing a fire bottle seal.

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Statikport

An external opening on an aircraft that senses ambient atmospheric pressure for use by the pitot-static system.

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Staudruckturbine

A small turbine deployed in flight to provide emergency hydraulic or electrical power using airflow.

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Steer-by-wire

A digital control system where electronic signals, not mechanical linkages, direct the nose-gear steering.

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Stellglied-Steuerelektronik

Boeing system managing flight control actuator signals for surface movement, including redundancy and fault isolation.

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System-Synoptikanzeige

A cockpit display providing a schematic overview of aircraft systems’ status, such as hydraulics, electrics, fuel, and air conditioning.

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Total-Lufttemperaturfühler

A sensor on the aircraft that measures total air temperature, providing critical input for engine and air-data systems.

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Transponder-Bedienfeld

Cockpit panel used for selecting, setting, and controlling aircraft transponder modes and codes.

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Triebwerksanzeige- und Crew-Warnsystem

A Boeing system that displays engine and system data and alerts for operational and abnormal conditions.

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Triebwerksanzeigenanzeige

The cockpit display panel showing all vital engine parameters, including N1/N2, temperature, oil pressure, fuel flow, and vibrations.

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Triebwerksdruckverhältnis

Ratio of total pressure at the engine exhaust to that at the engine inlet, used as a primary engine thrust indicator.

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Triebwerksenteisung

A system that prevents or removes ice formation on engine inlets, typically using hot bleed air.

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Triebwerksöldruck

The pressure of oil circulating through an aircraft engine, essential for lubrication and cooling of moving components.

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Trimm des Höhenleitwerks

The adjustment of the horizontal stabilizer angle to balance the aircraft in pitch for all flight phases.

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Trimm-Luft

A system that adds small amounts of hot bleed air to the mixed supply to fine-tune cabin temperature zones.

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Trägheitsnavigationssystem

A self-contained navigation system using accelerometers and gyros to compute aircraft position, independent of external signals.

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UKW-Drehfunkfeuer

A ground-based radio navigation system providing azimuth guidance to aircraft using VHF signals.

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Ultrakurzwellenfunk

Radio system in the VHF band (118–137 MHz) used for primary ATC voice communication within line-of-sight range.

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Umluftventilator

A fan that recirculates cabin air, mixing it with conditioned air to improve efficiency and reduce bleed air demand.

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unkgerichtetes Funkfeuer

A ground-based radio transmitter used for navigation, providing direction by reference only.

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verstellbare Leitschaufeln

Adjustable compressor guide vanes that control airflow angle and optimize engine efficiency across operating conditions.

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verstellbare Zapfluftventile

Adjustable engine valves that regulate bleed air extraction to maintain compressor stability and prevent stall.

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vollständige digitale Triebwerkssteuerung

An electronic system that provides complete automated control of all engine parameters for optimum performance.

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Zapfluft

High-pressure air extracted from an aircraft engine's compressor stage and used for environmental control, pressurization, anti-ice, and pneumatic systems.

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Zapfluftabschaltung

Automatic closure of bleed air supply due to over-temperature or over-pressure, protecting the system from damage.

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Zapfluftüberdruck

A condition where the bleed air pressure exceeds safe limits, causing automatic shutdown or system warnings.

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über Grund

An altitude or height measured with reference to the underlying ground surface directly beneath the aircraft.

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