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The highest crosswind component at which satisfactory control was demonstrated during aircraft certification flight tests.
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Browse Flight Planning terms for pilots, air traffic controllers, cabin crew and aviation learners.
The highest crosswind component at which satisfactory control was demonstrated during aircraft certification flight tests.
View termFuel required to fly from the destination to an alternate aerodrome en‑route under planned conditions.
View termFixed quantity of fuel required to be carried for emergencies as per regulatory minimum reserve rules.
View termAdditional reserve fuel calculated proportionally to flight time beyond the fixed reserve, for unforeseen delays.
View termEstimated fuel required for taxiing after landing, including clearing runway and reaching gate.
View termFuel required for engine start, taxi, and contingencies before take-off.
View termThe total weight of the aircraft while parked at the ramp, including fuel, payload, and all crew and equipment before engine start or taxi.
View termThe weight of an aircraft including all standard items and operating fluids but excluding payload and usable fuel.
View termThe weight of an aircraft including crew, unusable fuel, and all necessary fluids for operation, excluding payload and usable fuel.
View termThe highest level of engine thrust that can be used continuously without time limitation under normal operating conditions.
View termThrust Less Than Maximum Take‑Off Thrust Applied During Take‑Off To Increase Engine Life And Optimize Operational Efficiency.
View termReduced engine thrust setting used for take-off to extend engine life, improve fuel efficiency, and meet noise abatement procedures.
View termLowest climb gradient required to ensure obstacle clearance or meet procedure design criteria.
View termMinimum climb performance required during a go-around or missed approach with all engines operating.
View termMinimum vertical profile flown after take‑off, reduced from gross climb to ensure obstacle clearance following critical-engine failure
View termDistance from threshold to point on runway where go‑around decision altitude is reached, allowing a missed‑approach before runway end.
View termDeclared length of runway suitable for the ground run of an aircraft taking off, excluding clearway.
View termDeclared length of runway plus clearway that is available and suitable for the ground run of an aircraft taking off.
View termDeclared length of runway that is available and suitable for the ground run of an aircraft landing.
View termCalculated distance an aircraft needs to land and come to a complete stop under existing conditions.
View termDistance needed to accelerate to decision speed, experience an engine failure and continue take-off to 35 ft above runway.
View termThe distance from brake-release or acceleration point to airplane lift-off during take‑off roll.
View termThe highest speed from which an aircraft can stop without exceeding the maximum brake energy limit, used to ensure brake system integrity and safety.
View termTarget airspeed reached after V2 during take‑off, providing sufficient climb gradient with one engine inoperative.
View termThe highest ground speed a tire can sustain without risking structural failure, defined by aircraft and tire manufacturers.
View termTarget speed established by crew to optimize landing safety and performance, typically VREF plus wind correction.
View termSpeed selected for use on final approach segment, ensuring safe control margin above stall but stable profile.
View termIndicated airspeed corrected for compressibility effects at altitude, used for performance comparisons.
View termIndicated airspeed corrected for instrument and position errors, used for accurate performance calculations.
View termVertical Thickness Of Water, Slush, Or Other Moisture‑Related Contaminants On The Runway Measured In Millimetres For Performance Calculations.
View termSpecified altitude in precision approach at which a missed approach must be initiated if runway not in sight.
View termAltitude at which the aircraft feels it is flying based on current pressure, temperature, and humidity, affecting performance.
View termAltitude indicated when the altimeter is set to the standard pressure setting of 1013.25 hPa (29.92 inHg).
View termNumeric Value From 0 To 6 Indicating The Braking Action And Surface Condition Of A Runway As Published In A Runway Condition Report.
View termWind Blowing Opposite To Aircraft Movement, Increasing Lift And Reducing Required Take‑Off Or Landing Distance.
View termWind Blowing In The Same Direction As Aircraft Movement, Reducing Lift And Increasing Required Take‑Off Or Landing Distance.
View termThe component of the wind along the runway axis directed opposite to aircraft’s travel, used for performance calculations.
View termWind Component Perpendicular To The Runway Centerline, Affecting Aircraft Lateral Control During Take‑Off And Landing.
View termAdjustment applied to declared runway length to account for runway slope and ambient temperature effects on aircraft performance.
View termThe rate at which temperature decreases with altitude under standard atmospheric conditions, 2 °C per 1000 ft or 6.5 °C per 1000 m.
View termPilot‑reported Assessment Of Actual Aircraft Braking Performance On A Runway Surface.
View termTake‑off Using An Assumed Temperature Higher Than Actual To Reduce Thrust And Prolong Engine Life While Meeting Performance Requirements.
View termStandardized Tool Used To Assign Runway Condition Codes Based On Surface Type And Contaminant Characteristics, Supporting Aircraft Performance Assessment.
View termA defined rectangular area beyond the runway, free of obstructions, suitable for aircraft to continue take-off in case of engine failure.
View termRunway length at which accelerate-go and accelerate-stop distances are equal under specified conditions.
View termLength Of The Designated Area Beyond The Runway End That Can Be Used To Decelerate During A Rejected Take‑Off, As Part Of ASDA.
View termThe length of a stopway usable in the event of a rejected take-off, beyond the take-off run available.
View termClimb segment after acceleration and flap retraction up to en‑route climb altitude with one-engine inoperative.
View termClimb segment from gear retraction to acceleration altitude with one-engine inoperative, maintaining prescribed gradient.
View termImaginary inclined plane established to ensure minimum safe vertical separation between aircraft flight paths and obstacles.
View termAn obstacle‑free area beyond the runway threshold, providing required visual clearance during the final approach segment.
View termThe minimum climb gradient that an aircraft must meet during the missed approach phase, considering one engine inoperative.
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