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Boeing system managing flight control actuator signals for surface movement, including redundancy and fault isolation.
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Incele Aircraft Systems terms for pilots, air traffic controllers, cabin crew and aviation learners.
Boeing system managing flight control actuator signals for surface movement, including redundancy and fault isolation.
Terimi gorA precision approach system providing lateral and vertical guidance to aircraft during landing using radio signals.
Terimi gorA backup method to deploy the landing gear using gravity, hydraulic, or manual means if the normal extension system fails.
Terimi gorRotational speed of the low-pressure compressor or fan in a jet engine, often indicated as N₁.
Terimi gorA central alerting system that warns the flight crew of abnormal but non-critical system status via lights and aural tones.
Terimi gorA programmed series of actions by which the auxiliary power unit starts automatically and safely without crew intervention.
Terimi gorAdvanced system alerting pilots of hazardous terrain or obstacles using GPS and a terrain database, supplementing GPWS.
Terimi gorAn official list of equipment required for safe operation of an aircraft, specifying items which may be inoperative under specific conditions.
Terimi gorAn aircraft system providing position and attitude data by processing gyroscopic and accelerometer inputs.
Terimi gorA self-contained navigation system using accelerometers and gyros to compute aircraft position, independent of external signals.
Terimi gorA fan dedicated to cooling avionics equipment by circulating air through the electronics bay.
Terimi gorA system providing airflow and temperature regulation to prevent overheating of aircraft avionics components.
Terimi gorAdjustable engine valves that regulate bleed air extraction to maintain compressor stability and prevent stall.
Terimi gorAdjustable compressor guide vanes that control airflow angle and optimize engine efficiency across operating conditions.
Terimi gorA set of airspace procedures allowing aircraft to be separated by 1,000 feet vertically above FL290, increasing airspace capacity.
Terimi gorThe Boeing main computer responsible for integrating pilot inputs, aircraft data, and actuating control surfaces.
Terimi gorThe main instrument display showing attitude, speed, altitude, heading, and flight director information.
Terimi gorThe adjustment of the horizontal stabilizer angle to balance the aircraft in pitch for all flight phases.
Terimi gorA flight-control adjustment that offsets rudder position to maintain coordinated flight and correct for yaw.
Terimi gorA fan that recirculates cabin air, mixing it with conditioned air to improve efficiency and reduce bleed air demand.
Terimi gorA valve that regulates the discharge of air from the pressurized cabin to maintain desired cabin pressure.
Terimi gorThe temperature of the air outside the aircraft, used in performance and anti-ice calculations.
Terimi gorThe temperature of gases emitted by the engine exhaust, critical for monitoring engine health and performance.
Terimi gorA digitally controlled switch that protects an electrical circuit from overload by interrupting power supply electronically.
Terimi gorAn Airbus system that displays engine, system, and alert messages for aircraft monitoring and troubleshooting.
Terimi gorA digital control system where electronic signals, not mechanical linkages, direct the nose-gear steering.
Terimi gorA hydraulic actuator that converts hydraulic pressure into elevator movement, enabling pitch control of the aircraft.
Terimi gorA dedicated computer on Airbus aircraft that processes inputs and controls elevator and aileron surfaces.
Terimi gorA valve designed to automatically relieve excess pressure or vacuum to protect the aircraft structure.
Terimi gorA generator that converts variable engine speed to constant frequency AC power for aircraft electrical systems.
Terimi gorA combined flight control surface that functions as both aileron and flap, used on some aircraft to improve control and lift.
Terimi gorA cockpit display or system that monitors the temperature of the main landing-gear brakes to prevent overheating.
Terimi gorA set of precision standards for aircraft navigation accuracy, integrity, and reliability within defined airspace or procedures.
Terimi gorA hydraulic unit that enables power transfer between two separate hydraulic systems without mixing their fluids.
Terimi gorAn advanced aircraft system combining air data sensors and inertial reference to provide navigation and performance data.
Terimi gorAircraft module collecting and providing airspeed, altitude, and temperature data from external probes.
Terimi gorA pressurized storage device that maintains hydraulic pressure and absorbs system shocks.
Terimi gorA tank storing hydraulic fluid for aircraft hydraulic systems, ensuring continuous supply during all phases of operation.
Terimi gorA device that moves hydraulic fluid under pressure to operate aircraft systems such as landing gear, brakes, and flight controls.
Terimi gorA cockpit control that arms or actuates spoiler panels to reduce speed or rate of descent during flight and landing roll.
Terimi gorAir conditioning and pressurization units that cool, condition, and regulate the flow of air into the cabin using bleed air.
Terimi gorA valve that regulates the flow of bleed air into the air conditioning pack.
Terimi gorA system that adds small amounts of hot bleed air to the mixed supply to fine-tune cabin temperature zones.
Terimi gorThe position or angle of the thrust lever, directly corresponding to engine power demand.
Terimi gorA device used to redirect engine thrust forward to assist with deceleration after landing.
Terimi gorElectronic module that manages and protects an aircraft generator, monitoring voltage, current, and system faults.
Terimi gorAutomatic device that regulates cabin altitude and rate of pressure change by controlling the outflow valve.
Terimi gorAn integrated system enabling voice communication between cabin crew and cockpit, and among crew stations.
Terimi gorA system that prevents or removes ice accumulation on the wing leading edges using bleed air or electrical elements.
Terimi gorA flight-control adjustment that sets ailerons to correct lateral imbalance and maintain wings-level flight.
Terimi gorA component that blends recirculated cabin air with conditioned air from the packs before distribution.
Terimi gorA digital communication system enabling direct text-based exchanges between ATC and pilots via data link instead of voice.
Terimi gorA system of satellites providing worldwide navigation, including GPS, GLONASS, Galileo, and BeiDou.
Terimi gorA system that compensates for Mach tuck by automatically adjusting stabilizer trim at high subsonic speeds.
Terimi gorOne of three Airbus hydraulic systems, providing redundancy for flight controls, landing gear, and other powered components.
Terimi gorAn aircraft navigation system providing slant-range distance to a ground station, often paired with VOR or ILS.
Terimi gorAn aircraft transponder providing selective, data-rich responses to ATC interrogations, supporting identification and surveillance functions.
Terimi gorRatio of total pressure at the engine exhaust to that at the engine inlet, used as a primary engine thrust indicator.
Terimi gorA system that prevents or removes ice formation on engine inlets, typically using hot bleed air.
Terimi gorThe cockpit display panel showing all vital engine parameters, including N1/N2, temperature, oil pressure, fuel flow, and vibrations.
Terimi gorA Boeing system that displays engine and system data and alerts for operational and abnormal conditions.
Terimi gorHigh-pressure air extracted from an aircraft engine's compressor stage and used for environmental control, pressurization, anti-ice, and pneumatic systems.
Terimi gorA condition where the bleed air pressure exceeds safe limits, causing automatic shutdown or system warnings.
Terimi gorAutomatic closure of bleed air supply due to over-temperature or over-pressure, protecting the system from damage.
Terimi gorThe pressure of oil circulating through an aircraft engine, essential for lubrication and cooling of moving components.
Terimi gorElectronic display showing route, waypoints, navigation aids, weather, and traffic information.
Terimi gorAn altitude or elevation reference based on the average sea level used as a standard for aviation altimetry.
Terimi gorA surveillance technology in which aircraft broadcast position and flight data, allowing real-time tracking by ATC and other aircraft.
Terimi gorA system that automatically applies braking at a selected rate during landing or rejected take-off to optimize stopping distance.
Terimi gorA system that automatically sets and maintains engine thrust based on flight parameters and autopilot commands.
Terimi gorA sensor in an engine or gearbox that detects metallic particles, indicating wear or damage to internal components.
Terimi gorA small pyrotechnic device used to rapidly release fire-extinguishing agent by rupturing a fire bottle seal.
Terimi gorThe distance over which a pilot of an aircraft on the centre line of a runway can see the runway surface markings or lights.
Terimi gorA forward-facing tube that measures dynamic air pressure, providing critical input for airspeed indication.
Terimi gorA small turbine deployed in flight to provide emergency hydraulic or electrical power using airflow.
Terimi gorA transmission device that converts variable engine speed to a constant speed for generator operation.
Terimi gorOne of three independent hydraulic systems on Airbus aircraft, supplying power to specific flight controls, brakes, and cargo doors.
Terimi gorA cockpit display providing a schematic overview of aircraft systems’ status, such as hydraulics, electrics, fuel, and air conditioning.
Terimi gorA hinged surface on the upper wing that disrupts airflow, reducing lift and increasing drag for roll control or descent.
Terimi gorAn Airbus computer managing spoilers, elevator backup, and other flight control surfaces for redundancy and flight envelope protection.
Terimi gorAn external opening on an aircraft that senses ambient atmospheric pressure for use by the pitot-static system.
Terimi gorAn electronic system that provides complete automated control of all engine parameters for optimum performance.
Terimi gorSensor measuring total (pitot) pressure at engine station 2 for air data and engine control systems.
Terimi gorA sensor on the aircraft that measures total air temperature, providing critical input for engine and air-data systems.
Terimi gorAn airborne safety system providing pilots with traffic advisories and resolution advisories to avoid mid-air collisions.
Terimi gorA long-range communication system using satellites, enabling cockpit and company contact beyond VHF and HF range.
Terimi gorA system on Airbus aircraft that provides additional functions such as yaw damping, rudder trim, and flight envelope protection.
Terimi gorHydraulic circuit dedicated to supplying pressure to flight control surfaces such as ailerons, elevators, and rudder.
Terimi gorAn electronic flight control system where pilot inputs are transmitted as electrical signals to computers, which command the flight control surfaces.
Terimi gorA system that processes and displays warnings and cautions to the flight crew in response to abnormal conditions.
Terimi gorAn avionics system integrating navigation, performance, and flight planning for automated aircraft operation.
Terimi gorVisual cues on the Primary Flight Display indicating desired pitch and roll to guide manual flight path.
Terimi gorCockpit panel used for selecting, setting, and controlling aircraft transponder modes and codes.
Terimi gorA ground-based radio navigation system providing azimuth guidance to aircraft using VHF signals.
Terimi gorAn automatic system that prevents unwanted yaw oscillations by commanding the rudder, increasing flight comfort and stability.
Terimi gorA continuous sensing circuit that detects overheat or fire in aircraft engines, APU, or cargo bays.
Terimi gorA pressurized container storing extinguishing agent for aircraft fire suppression in engines, cargo, or APU compartments.
Terimi gorA self-contained turbine engine providing electrical and pneumatic power to the aircraft while on the ground or as backup in flight.
Terimi gorAn altitude or height measured with reference to the underlying ground surface directly beneath the aircraft.
Terimi gorAn aircraft safety system that warns pilots if the aircraft is at risk of controlled flight into terrain or obstacles.
Terimi gorOne of three independent hydraulic systems on Airbus aircraft, powering primary flight controls, landing gear, and other components.
Terimi gorA ground-based radio transmitter used for navigation, providing direction by reference only.
Terimi gorRotational speed of the high-pressure compressor or core in a jet engine, commonly indicated as N₂.
Terimi gorRadio system operating in the HF band (3–30 MHz), enabling long-distance voice communication between aircraft and ATC.
Terimi gorSpoiler panels on the wings that fully deploy upon landing to disrupt lift and aid in braking and deceleration.
Terimi gorRadio system in the VHF band (118–137 MHz) used for primary ATC voice communication within line-of-sight range.
Terimi gorThe system that allows pilots to steer the aircraft’s nose landing gear during taxi and ground operations.
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