Altimeter Setting (QNH vs QNE)
Calculate difference between indicated altitude and pressure altitude based on local QNH.
At standard 1013 hPa / 29.92 inHg, indicated equals pressure altitude.
Fast, practical pilot utilities to resolve conversions, compute top-of-descent points, and calculate crosswind components.
Calculate difference between indicated altitude and pressure altitude based on local QNH.
At standard 1013 hPa / 29.92 inHg, indicated equals pressure altitude.
Estimate air density from pressure altitude and outside air temperature (OAT).
ISA: 9,0°C (Δ 16,0°C)
Calculate cloud base height using the standard rule of thumb: Spread / 2.5 × 1,000 ft.
Spread T - Td = 8,0°C
Estimate true airspeed using the +2% per 1,000 ft altitude rule.
Fator: +12,0%
Calculate the ideal descent point using the standard 3:1 vertical descent rule.
Perda total de 7.500 ft
Perfil padrão para 140 kt
Calculate en-route fuel burn and total aircraft endurance based on hourly fuel flow.
Reserva restante: 63,0 L
Baseado em fluxo constante de 38 L/h
Check hemispheric cruise level: Odd thousands for 000°–179°, Even for 180°–359°.
Ex: FL055, FL075, FL095 (VFR) / FL050, FL070 (IFR)
Determine the target vertical speed (VS) in feet per minute to stay on a 3-degree glide path.
Standard rule: GS × 5 = target vertical speed in ft/min.
Precision universal coordinated time clock for flight planning and METAR/TAF time checks.
UTC Date: August 28, 2026
Resolve wind vector into crosswind and headwind/tailwind components for takeoff and landing.
Right crosswind
Vento de proa favorável
These flight calculation tools are intended solely for academic study and desktop flight simulation. For real-world flight operations, always consult certified aircraft pilot operating handbooks (POH/AFM).