Боковая Составляющая Ветра
Wind Component Perpendicular To The Runway Centerline, Affecting Aircraft Lateral Control During Take‑Off And Landing.
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Flight Planning
Browse Flight Planning terms for pilots, air traffic controllers, cabin crew and aviation learners.
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вес на стоянке
The total weight of the aircraft while parked at the ramp, including fuel, payload, and all crew and equipment before engine start or taxi.
View termВзлёт По Гибкой Температуре
Take‑off Using An Assumed Temperature Higher Than Actual To Reduce Thrust And Prolong Engine Life While Meeting Performance Requirements.
View termвторой сегмент набора высоты
Climb segment from gear retraction to acceleration altitude with one-engine inoperative, maintaining prescribed gradient.
View termвысота плотности
Altitude at which the aircraft feels it is flying based on current pressure, temperature, and humidity, affecting performance.
View termвысота принятия решения
Specified altitude in precision approach at which a missed approach must be initiated if runway not in sight.
View termГлубина Водного Загрязнения
Vertical Thickness Of Water, Slush, Or Other Moisture‑Related Contaminants On The Runway Measured In Millimetres For Performance Calculations.
View termградиент набора высоты при посадке
Minimum climb performance required during a go-around or missed approach with all engines operating.
View termдавление высота
Altitude indicated when the altimeter is set to the standard pressure setting of 1013.25 hPa (29.92 inHg).
View termДлина Зоны Остановки
Length Of The Designated Area Beyond The Runway End That Can Be Used To Decelerate During A Rejected Take‑Off, As Part Of ASDA.
View termдлина свободной зоны
A defined rectangular area beyond the runway, free of obstructions, suitable for aircraft to continue take-off in case of engine failure.
View termдлина тормозного участка
The length of a stopway usable in the event of a rejected take-off, beyond the take-off run available.
View termдоступная взлётная дистанция
Declared length of runway plus clearway that is available and suitable for the ground run of an aircraft taking off.
View termдоступная посадочная дистанция
Declared length of runway that is available and suitable for the ground run of an aircraft landing.
View termдоступное расстояние принятия решения
Distance from threshold to point on runway where go‑around decision altitude is reached, allowing a missed‑approach before runway end.
View termдоступный разбег для взлёта
Declared length of runway suitable for the ground run of an aircraft taking off, excluding clearway.
View termкалиброванная воздушная скорость
Indicated airspeed corrected for instrument and position errors, used for accurate performance calculations.
View termКод Состояния ВПП
Numeric Value From 0 To 6 Indicating The Braking Action And Surface Condition Of A Runway As Published In A Runway Condition Report.
View termКомпонент Лобового Ветра
Wind Blowing Opposite To Aircraft Movement, Increasing Lift And Reducing Required Take‑Off Or Landing Distance.
View termКомпонент Попутного Ветра
Wind Blowing In The Same Direction As Aircraft Movement, Reducing Lift And Increasing Required Take‑Off Or Landing Distance.
View termкомпонента встречного ветра
The component of the wind along the runway axis directed opposite to aircraft’s travel, used for performance calculations.
View termкоррекция длины ВПП для уклона и температуры
Adjustment applied to declared runway length to account for runway slope and ambient temperature effects on aircraft performance.
View termМаксимальная Продолжительная Тяга
The highest level of engine thrust that can be used continuously without time limitation under normal operating conditions.
View termМаксимальная Скорость Шины
The highest ground speed a tire can sustain without risking structural failure, defined by aircraft and tire manufacturers.
View termМаксимальная Скорость Энергии Торможения
The highest speed from which an aircraft can stop without exceeding the maximum brake energy limit, used to ensure brake system integrity and safety.
View termмаксимальный демонстрированный боковой ветер
The highest crosswind component at which satisfactory control was demonstrated during aircraft certification flight tests.
View termМатрица Оценки Состояния ВПП
Standardized Tool Used To Assign Runway Condition Codes Based On Surface Type And Contaminant Characteristics, Supporting Aircraft Performance Assessment.
View termМинимальный Градиент Набора Высоты
Lowest climb gradient required to ensure obstacle clearance or meet procedure design criteria.
View termнеобходимая дистанция ускорения-продолжения
Distance needed to accelerate to decision speed, experience an engine failure and continue take-off to 35 ft above runway.
View termнетто-профиль набора высоты
Minimum vertical profile flown after take‑off, reduced from gross climb to ensure obstacle clearance following critical-engine failure
View termосновной эксплуатационный вес
The weight of an aircraft including crew, unusable fuel, and all necessary fluids for operation, excluding payload and usable fuel.
View termОтчёт О Сцеплении При Торможении
Pilot‑reported Assessment Of Actual Aircraft Braking Performance On A Runway Surface.
View termповерхность визуального сегмента
An obstacle‑free area beyond the runway threshold, providing required visual clearance during the final approach segment.
View termповерхность обеспечения препятствий
Imaginary inclined plane established to ensure minimum safe vertical separation between aircraft flight paths and obstacles.
View termрасстояние пробега по земле
The distance from brake-release or acceleration point to airplane lift-off during take‑off roll.
View termсбалансированная длина ВПП
Runway length at which accelerate-go and accelerate-stop distances are equal under specified conditions.
View termскорость безопасности при взлёте
Target airspeed reached after V2 during take‑off, providing sufficient climb gradient with one engine inoperative.
View termСниженная Взлётная Тяга
Reduced engine thrust setting used for take-off to extend engine life, improve fuel efficiency, and meet noise abatement procedures.
View termСниженная Взлётная Тяга
Thrust Less Than Maximum Take‑Off Thrust Applied During Take‑Off To Increase Engine Life And Optimize Operational Efficiency.
View termтемпературный градиент стандартной атмосферы
The rate at which temperature decreases with altitude under standard atmospheric conditions, 2 °C per 1000 ft or 6.5 °C per 1000 m.
View termтопливо до запасного аэродрома в полёте
Fuel required to fly from the destination to an alternate aerodrome en‑route under planned conditions.
View termтопливо переменного резерва
Additional reserve fuel calculated proportionally to flight time beyond the fixed reserve, for unforeseen delays.
View termтопливо руления перед взлетом
Fuel required for engine start, taxi, and contingencies before take-off.
View termтопливо руления после посадки
Estimated fuel required for taxiing after landing, including clearing runway and reaching gate.
View termтопливо фиксированного резерва
Fixed quantity of fuel required to be carried for emergencies as per regulatory minimum reserve rules.
View termТребование Подъема При Заходе На Посадку
The minimum climb gradient that an aircraft must meet during the missed approach phase, considering one engine inoperative.
View termтребуемая посадочная дистанция
Calculated distance an aircraft needs to land and come to a complete stop under existing conditions.
View termфинальный набор высоты после взлёта
Climb segment after acceleration and flap retraction up to en‑route climb altitude with one-engine inoperative.
View termэквивалентная воздушная скорость
Indicated airspeed corrected for compressibility effects at altitude, used for performance comparisons.
View termэксплуатационный пустой вес
The weight of an aircraft including all standard items and operating fluids but excluding payload and usable fuel.
View termэталонная скорость захода
Speed selected for use on final approach segment, ensuring safe control margin above stall but stable profile.
View termэталонная скорость захода на посадку
Target speed established by crew to optimize landing safety and performance, typically VREF plus wind correction.
View term