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9 Services from aviation-calc.x402tookit.com

aviation-calc.x402tookit.comAviation Calculators – Fuel, Time & Distance (E6B)x402

Solves E6B flight computer arithmetic for any two of distance, groundspeed, and time, plus fuel burn, reserve fuel, and range calculations.

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aviation-calc.x402tookit.comAviation Glide Ratio Calculatorx402

Calculates glide distance, time, and sink rate from altitude above ground, glide ratio, and optional airspeed and wind components.

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aviation-calc.x402tookit.comAviation Calculators – True Airspeed, Mach & Equivalent Airspeedx402

Calculates true airspeed (TAS), Mach number, and equivalent airspeed (EAS) from calibrated airspeed, pressure altitude, and outside air temperature.

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aviation-calc.x402tookit.comAviation Density Altitude Calculatorx402

Calculates density altitude (exact and rule-of-thumb) from field elevation, altimeter setting, and outside air temperature, with a performance flag.

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aviation-calc.x402tookit.comAviation Wind Triangle Calculator (E6B)x402

Computes E6B wind triangle solutions: wind correction angle and heading/groundspeed for a given course, or track and groundspeed for a given heading flown.

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aviation-calc.x402tookit.comAviation Turn & Hold Pattern Calculatorx402

Computes turn rate, radius, bank angle, and load factor from true airspeed, plus holding pattern leg length, width, and time.

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aviation-calc.x402tookit.comAviation Wind Components Calculatorx402

Calculates headwind/tailwind and left/right crosswind components from wind direction, speed, and runway heading, including gust components and crosswind limit comparison.

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aviation-calc.x402tookit.comAviation Calculators – ISA Atmospherex402

Returns International Standard Atmosphere properties at a given pressure altitude: temperature, pressure, density, speed of sound, and optional ISA deviation from actual OAT.

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aviation-calc.x402tookit.comAviation Pressure Altitude Calculatorx402

Calculates pressure altitude from field elevation and altimeter setting (inHg or hPa), returning both the exact ISA result and the 1000 ft/inHg rule-of-thumb approximation.

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