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Flight Planning

Browse Flight Planning terms for pilots, air traffic controllers, cabin crew and aviation learners.

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Abstellgewicht

The total weight of the aircraft while parked at the ramp, including fuel, payload, and all crew and equipment before engine start or taxi.

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Anflug‑Referenzgeschwindigkeit

Speed selected for use on final approach segment, ensuring safe control margin above stall but stable profile.

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ausgeglichene Bahnlänge

Runway length at which accelerate-go and accelerate-stop distances are equal under specified conditions.

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betriebsbedingtes Leergewicht

The weight of an aircraft including all standard items and operating fluids but excluding payload and usable fuel.

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Bodenrollstrecke

The distance from brake-release or acceleration point to airplane lift-off during take‑off roll.

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Bremswirkungsbericht

Pilot‑reported Assessment Of Actual Aircraft Braking Performance On A Runway Surface.

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Dichtedruckhöhe

Altitude at which the aircraft feels it is flying based on current pressure, temperature, and humidity, affecting performance.

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Druckhöhe

Altitude indicated when the altimeter is set to the standard pressure setting of 1013.25 hPa (29.92 inHg).

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Endgültiger Steigflug nach dem Start

Climb segment after acceleration and flap retraction up to en‑route climb altitude with one-engine inoperative.

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Entscheidungshöhe

Specified altitude in precision approach at which a missed approach must be initiated if runway not in sight.

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En‑Route‑Alternativ‑Treibstoff

Fuel required to fly from the destination to an alternate aerodrome en‑route under planned conditions.

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erforderliche Beschleunigungs-Fortsetzungsstrecke

Distance needed to accelerate to decision speed, experience an engine failure and continue take-off to 35 ft above runway.

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erforderliche Landestrecke

Calculated distance an aircraft needs to land and come to a complete stop under existing conditions.

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Fix‑Reserve‑Treibstoff

Fixed quantity of fuel required to be carried for emergencies as per regulatory minimum reserve rules.

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Flex‑Temperatur‑Start

Take‑off Using An Assumed Temperature Higher Than Actual To Reduce Thrust And Prolong Engine Life While Meeting Performance Requirements.

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Frontwind‑Komponente

The component of the wind along the runway axis directed opposite to aircraft’s travel, used for performance calculations.

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Gegenwindkomponente

Wind Blowing Opposite To Aircraft Movement, Increasing Lift And Reducing Required Take‑Off Or Landing Distance.

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Grundbetriebsgewicht

The weight of an aircraft including crew, unusable fuel, and all necessary fluids for operation, excluding payload and usable fuel.

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Hindernisfreifläche

Imaginary inclined plane established to ensure minimum safe vertical separation between aircraft flight paths and obstacles.

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Kalibrierte Fluggeschwindigkeit

Indicated airspeed corrected for instrument and position errors, used for accurate performance calculations.

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Länge der Freifläche

A defined rectangular area beyond the runway, free of obstructions, suitable for aircraft to continue take-off in case of engine failure.

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Länge der Stoppstrecke

The length of a stopway usable in the event of a rejected take-off, beyond the take-off run available.

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maximal nachgewiesener Seitenwind

The highest crosswind component at which satisfactory control was demonstrated during aircraft certification flight tests.

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Maximale Bremsenergiegeschwindigkeit

The highest speed from which an aircraft can stop without exceeding the maximum brake energy limit, used to ensure brake system integrity and safety.

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Maximale Reifengeschwindigkeit

The highest ground speed a tire can sustain without risking structural failure, defined by aircraft and tire manufacturers.

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Maximaler Dauer‑Schub

The highest level of engine thrust that can be used continuously without time limitation under normal operating conditions.

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Minimaler Steiggradient

Lowest climb gradient required to ensure obstacle clearance or meet procedure design criteria.

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Netto‑Steigflugbahn

Minimum vertical profile flown after take‑off, reduced from gross climb to ensure obstacle clearance following critical-engine failure

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Norm‑Atmosphäre Temperaturgradient

The rate at which temperature decreases with altitude under standard atmospheric conditions, 2 °C per 1000 ft or 6.5 °C per 1000 m.

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Pistenlängen‑Korrektur für Neigung und Temperatur

Adjustment applied to declared runway length to account for runway slope and ambient temperature effects on aircraft performance.

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Pistenzustandscode

Numeric Value From 0 To 6 Indicating The Braking Action And Surface Condition Of A Runway As Published In A Runway Condition Report.

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Reduzierter Startschub

Reduced engine thrust setting used for take-off to extend engine life, improve fuel efficiency, and meet noise abatement procedures.

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Reduzierter Startschub

Thrust Less Than Maximum Take‑Off Thrust Applied During Take‑Off To Increase Engine Life And Optimize Operational Efficiency.

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Referenzlandungsgeschwindigkeit

Target speed established by crew to optimize landing safety and performance, typically VREF plus wind correction.

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Rollbahnzustandsbewertungsmatrix

Standardized Tool Used To Assign Runway Condition Codes Based On Surface Type And Contaminant Characteristics, Supporting Aircraft Performance Assessment.

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Rückenwindkomponente

Wind Blowing In The Same Direction As Aircraft Movement, Reducing Lift And Increasing Required Take‑Off Or Landing Distance.

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Seitenwindkomponente

Wind Component Perpendicular To The Runway Centerline, Affecting Aircraft Lateral Control During Take‑Off And Landing.

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Sekundär‑Steigabschnitt

Climb segment from gear retraction to acceleration altitude with one-engine inoperative, maintaining prescribed gradient.

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Start‑Sicherheitgeschwindigkeit

Target airspeed reached after V2 during take‑off, providing sufficient climb gradient with one engine inoperative.

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Steiggradient bei der Landung

Minimum climb performance required during a go-around or missed approach with all engines operating.

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Steigleistungsanforderung Im Anflug

The minimum climb gradient that an aircraft must meet during the missed approach phase, considering one engine inoperative.

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Stopway‑Länge

Length Of The Designated Area Beyond The Runway End That Can Be Used To Decelerate During A Rejected Take‑Off, As Part Of ASDA.

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Taxi‑In‑Treibstoff

Estimated fuel required for taxiing after landing, including clearing runway and reaching gate.

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Taxi‑Out‑Treibstoff

Fuel required for engine start, taxi, and contingencies before take-off.

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Variable‑Reserve‑Treibstoff

Additional reserve fuel calculated proportionally to flight time beyond the fixed reserve, for unforeseen delays.

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Verfügbare Entscheidungsstrecke

Distance from threshold to point on runway where go‑around decision altitude is reached, allowing a missed‑approach before runway end.

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verfügbare Landestrecke

Declared length of runway that is available and suitable for the ground run of an aircraft landing.

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verfügbare Startlaufstrecke

Declared length of runway suitable for the ground run of an aircraft taking off, excluding clearway.

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verfügbare Startstrecke

Declared length of runway plus clearway that is available and suitable for the ground run of an aircraft taking off.

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Visuelles Segmentflächen

An obstacle‑free area beyond the runway threshold, providing required visual clearance during the final approach segment.

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Wassertiefe Der Kontamination

Vertical Thickness Of Water, Slush, Or Other Moisture‑Related Contaminants On The Runway Measured In Millimetres For Performance Calculations.

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Äquivalente Fluggeschwindigkeit

Indicated airspeed corrected for compressibility effects at altitude, used for performance comparisons.

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