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Aircraft Systems

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

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अनिवार्य नेविगेशन प्रदर्शन

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

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आउटफ्लो वाल्व

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

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इंजन इंस्ट्रूमेंट डिस्प्ले

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

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इंजन एंटी-आइस

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

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इंजन ऑयल प्रेशर

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

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इंजन प्रेशर अनुपात

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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इंजन संकेत और क्रू अलर्टिंग सिस्टम

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

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इंटीग्रेटेड ड्राइव जेनरेटर

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

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इंस्ट्रूमेंट लैंडिंग सिस्टम

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

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इनर्शियल नेविगेशन सिस्टम

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

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इनर्शियल रेफरेंस यूनिट

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

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इलेक्ट्रॉनिक केंद्रीकृत एयरक्राफ्ट मॉनिटर

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

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इलेक्ट्रॉनिक सर्किट ब्रेकर

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

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एक्चुएटर कंट्रोल इलेक्ट्रॉनिक्स

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

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एग्जॉस्ट गैस तापमान

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

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एपीयू स्वचालित स्टार्ट अनुक्रम

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

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एयर-डाटा इनर्शियल रेफरेंस यूनिट

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

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एयर-डाटा रेफरेंस

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

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एलिवेटर पावर-कंट्रोल यूनिट

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

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एलिवेटर-ऐलरॉन कंप्यूटर

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

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एवियोनिक्स कूलिंग सिस्टम

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

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एवियोनिक्स फैन

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

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ऐलरॉन ट्रिम

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

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ऑक्सिलरी पावर यूनिट

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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ऑटो-ब्रेक सिस्टम

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

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ऑटोथ्रॉटल सिस्टम

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

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ऑटोमैटिक डिपेंडेंट सर्विलांस–ब्रॉडकास्ट

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

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कंट्रोलर–पायलट डाटा लिंक कम्युनिकेशन

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

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कुल दाब नंबर 2 प्रोब

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

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कुल-वायु-तापमान जांच

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

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कैबिन इंटरकम्युनिकेशन सिस्टम

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

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कैबिन प्रेशर कंट्रोलर

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

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कॉन्स्टेंट-स्पीड ड्राइव

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

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ग्राउंड प्रॉक्सिमिटी वार्निंग सिस्टम

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

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ग्राउंड लेवल से ऊपर

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

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ग्राउंड स्पॉइलर

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

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ग्रीन हाइड्रोलिक सिस्टम

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

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घटित ऊर्ध्वाधर पृथक्करण न्यूनतम

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

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चिप डिटेक्टर

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

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जनरेटर कंट्रोल यूनिट

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

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टेरेन अवेयरनेस और वार्निंग सिस्टम

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

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ट्रांसपोंडर कंट्रोल पैनल

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

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ट्रिम एयर

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

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ट्रैफिक टकराव बचाव प्रणाली

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

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डिस्टेंस मेजरिंग इक्विपमेंट

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

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थ्रस्ट रिवर्सर

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

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थ्रस्ट-लीवर कोण

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

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नेविगेशन डिस्प्ले

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

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नॉन-डायरेक्शनल बीकन

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

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नोज-गियर स्टीयरिंग

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

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न्यूनतम उपकरण सूची

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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परिवर्तनीय ब्लीड वाल्व

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

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परिवर्तनीय स्टेटर वेन

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

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पावर ट्रांसफर यूनिट

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

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पिटोट प्रोब

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

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पैक्स यूनिट

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

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पैक्स वाल्व

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

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प्राइमरी फ्लाइट कंप्यूटर

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

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प्राइमरी फ्लाइट डिस्प्ले

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

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फायर एक्सटिंग्विशर बॉटल

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

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फायर-डिटेक्शन लूप

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

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फुल अथॉरिटी डिजिटल इंजन कंट्रोल

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

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फ्लाइट ऑगमेंटेशन कंप्यूटर

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

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फ्लाइट मैनेजमेंट सिस्टम

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

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फ्लाइट-कंट्रोल हाइड्रोलिक सर्किट

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

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फ्लाइट-डायरेक्टर बार्स

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

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फ्लाइट-वार्निंग कंप्यूटर

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

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फ्लाई-बाय-वायर

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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फ्लैपरॉन

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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बाहरी वायु तापमान

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

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ब्रेक तापमान मॉनिटर

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

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ब्लीड एयर

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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ब्लीड ओवरप्रेशर

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

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ब्लीड ट्रिप

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

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ब्लू हाइड्रोलिक सिस्टम

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

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माख-ट्रिम सिस्टम

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

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मास्टर कॉशन सिस्टम

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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मिक्सिंग यूनिट

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

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मीन सी लेवल

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

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मोड S ट्रांसपोंडर

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

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येलो हाइड्रोलिक सिस्टम

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

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यॉ-डैम्प सिस्टम

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

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रडर ट्रिम

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

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रनवे विजुअल रेंज

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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राम-एयर टरबाइन

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

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रीसर्क फैन

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

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लो-प्रेशर रोटर स्पीड

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

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विंग एंटी-आइस

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

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विस्फोटक चार्ज स्क्विब

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

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वीएचएफ ओम्निडायरेक्शनल रेंज

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

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वेरी-हाई-फ्रीक्वेंसी रेडियो

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

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वैकल्पिक लैंडिंग-गियर विस्तार

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

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वैश्विक नेविगेशन सैटेलाइट सिस्टम

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

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सिस्टम सिनॉप्टिक डिस्प्ले

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

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सेफ्टी वाल्व

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

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सैटेलाइट कम्युनिकेशन

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

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स्टीयर-बाय-वायर

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

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स्टेबलाइज़र ट्रिम

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

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स्टैटिक पोर्ट

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

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स्पीड-ब्रेक लीवर

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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स्पॉइलर पैनल

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

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स्पॉइलर-एलिवेटर कंप्यूटर

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

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हाइड्रोलिक एक्यूम्युलेटर

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

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हाइड्रोलिक पंप

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

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हाइड्रोलिक रिजर्वायर

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

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हाई-प्रेशर रोटर स्पीड

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

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हाई-फ्रीक्वेंसी रेडियो

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

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