MISSION CONTROL

Flight Tools & Calculators

Fast, practical pilot utilities to resolve conversions, compute top-of-descent points, and calculate crosswind components.

01

Altimeter Setting (QNH vs QNE)

Calculate difference between indicated altitude and pressure altitude based on local QNH.

RESULT+0 pés

At standard 1013 hPa / 29.92 inHg, indicated equals pressure altitude.

02

Density Altitude

Estimate air density from pressure altitude and outside air temperature (OAT).

RESULT4.920 pés

ISA: 9,0°C (Δ 16,0°C)

03

Convective Cloud Base

Calculate cloud base height using the standard rule of thumb: Spread / 2.5 × 1,000 ft.

RESULT3.200 pés AGL

Spread T - Td = 8,0°C

04

True Airspeed (TAS)

Estimate true airspeed using the +2% per 1,000 ft altitude rule.

RESULT123 kt TAS

Fator: +12,0%

05

Top of Descent (TOD)

Calculate the ideal descent point using the standard 3:1 vertical descent rule.

CRZ 10000 ft
Distância: 22,5 NMRazão: 700 ft/min
ALVO 2500 ft
Distance to begin descent22,5 NM

Perda total de 7.500 ft

Recommended rate for 140 kt GS700 ft/min

Perfil padrão para 140 kt

06

Fuel Consumption & Endurance

Calculate en-route fuel burn and total aircraft endurance based on hourly fuel flow.

Estimated burn57,0 L

Reserva restante: 63,0 L

Total endurance3h 09m

Baseado em fluxo constante de 38 L/h

07

Semicircular Flight Level Rule

Check hemispheric cruise level: Odd thousands for 000°–179°, Even for 180°–359°.

RESULTNível ÍMPAR (000°–179°)

Ex: FL055, FL075, FL095 (VFR) / FL050, FL070 (IFR)

08

ILS 3° Glide Slope Descent Rate

Determine the target vertical speed (VS) in feet per minute to stay on a 3-degree glide path.

RESULT600 ft/min

Standard rule: GS × 5 = target vertical speed in ft/min.

09

Live UTC / Zulu Clock

Precision universal coordinated time clock for flight planning and METAR/TAF time checks.

--:--:--UTC / ZULU

UTC Date: August 28, 2026

10

Crosswind & Headwind Components

Resolve wind vector into crosswind and headwind/tailwind components for takeoff and landing.

10
28
Ângulo Relativo: 40° (Direita)
Intensidade: 15 nós
RESULT9,6 kt crosswind

Right crosswind

RESULT11,5 kt headwind

Vento de proa favorável

Aviation Safety Disclaimer

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).