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Aviation Unit Converter

Instantly convert speed (knots, km/h, mph, Mach), altitude (feet, meters, flight levels), and temperature (°C, °F, Kelvin) — all in one place for pilots, AMEs and dispatchers.

Speed Converter

KT
km/h
mph
m/s
ft/min
Mach
FL / ft
Mach conversion uses ISA temperature at the given altitude. Speed of sound ≈ 661 kt at sea level (15°C).

Altitude / Flight Level Converter

ft
m
FL
km
nm
Flight Level Note
FL is pressure altitude in hundreds of feet (QNH 1013.25 hPa / 29.92 inHg). FL350 = 35,000 ft pressure altitude.

Temperature Converter

°C
°F
K
°R
Aviation Reference Temps
ISA Sea Level15°C / 59°F / 288.15 K
ISA Tropopause (36,089 ft)−56.5°C / 216.65 K
Water freezing point0°C / 32°F / 273.15 K
Jet A-1 freeze point−47°C

Common Speed References

Speed Context Knots (kt) km/h mph
Typical approach (light AC - e.g. C172) 65 120 75
Typical approach (jet - Vref) 140 259 161
Typical cruise (turboprop) 280 519 322
Typical cruise (narrow-body) 450 833 518
Mach 0.80 @ FL350 (Standard Temp) 459 850 528
Speed of sound (Sea Level, ISA) 662 1,225 761

Common Altitude References

Altitude Context Feet (ft) Metres (m) Flight Level (FL)
Transition altitude (EASA typical) 6,000 1,829 FL060
Typical turboprop cruise 25,000 7,620 FL250
Typical narrow-body cruise 35,000 10,668 FL350
Typical wide-body cruise 39,000 11,887 FL390
Tropopause (ISA) 36,089 11,000 FL361
Service ceiling (B747-400) 45,100 13,747 FL451

Frequently Asked Questions

IAS (Indicated Airspeed) is what the airspeed indicator reads. TAS (True Airspeed) is the actual speed through the air mass, accounting for altitude and temperature. GS (Ground Speed) is TAS corrected for wind. This converter works with TAS/GS values.

Mach = TAS ÷ Local Speed of Sound. The local speed of sound depends on temperature: a = 38.967 × √T (K) in knots. In ISA conditions, the lapse rate is −1.98°C per 1,000 ft up to the tropopause.

A Flight Level is a pressure altitude expressed in hundreds of feet, with the altimeter set to standard pressure (1013.25 hPa / 29.92 inHg). FL350 = 35,000 ft pressure altitude. FLs are used above the transition altitude to ensure vertical separation between aircraft.