geoprimsField-grade geospatial math

What is density altitude?

The altitude the airplane feels, why hot and high days lengthen the takeoff roll, and how to work it out exactly.

For pilots · updated 2026-09-23

Planning and education aid. Not for primary navigation. Full disclaimer

Density altitude is the altitude in the standard atmosphere where the air has the same density as the air around your airplane right now. Wings, propellers, and engines respond to air density, not to the number on the altimeter, so density altitude is the altitude the airplane actually performs at.

On a cool day at a sea-level airport, density altitude is close to field elevation. On a hot afternoon at a mountain airport, it can be thousands of feet higher. The airplane then takes off, climbs, and lands as if the runway were that much higher, with a longer takeoff roll, a lower rate of climb, and a faster true airspeed for the same indicated airspeed on approach.

Why it matters

Your pilot’s operating handbook (POH) gives takeoff distance and climb rate by pressure altitude and temperature. Density altitude is the single number that combines both, which is why it is the quickest way to sense how a day will fly. An airplane that is legal and within weight can still fail to clear an obstacle off a short, high runway on a hot afternoon, so it is worth checking before every summer departure from a high field.

Three things raise density altitude:

Pilots remember them as “high, hot, and humid.”

How it is worked out

The exact method has three steps.

  1. Pressure altitude. An altimeter set to the local altimeter setting (QNH) reads field elevation on the ground. Pressure altitude is what it would read with the setting at 29.92 inHg (1013.25 hPa). It equals field elevation plus the pressure altitude of the altimeter setting itself. The pressure altitude tool does this step.
  2. Air density. From the station pressure and the outside air temperature, the ideal gas law gives the air’s density. With a dew point, the tool uses the virtual temperature, which accounts for water vapor.
  3. Density altitude. Find the altitude in the ICAO standard atmosphere that has that density. The standard atmosphere starts at 15 °C and 1013.25 hPa at sea level and cools 1.98 °C per 1,000 ft. The standard atmosphere tool gives its values at any altitude.

A worked example

A 5,000 ft airport, an altimeter setting of 29.80 inHg, and 30 °C on the ramp:

Step Result
Pressure altitude 5,112 ft
Standard temperature at that altitude 4.9 °C
How much warmer than standard 25.1 °C
Density altitude, dry air 7,937 ft

The airplane performs as if it were at almost 8,000 ft, about 2,900 ft above the runway. Add a dew point of 20 °C and density altitude rises to 8,277 ft: humidity alone adds another 340 ft.

The rule of thumb, and how far it drifts

The common shortcut adds about 120 ft to pressure altitude for every degree Celsius above standard temperature. Some references use 118.8 ft. For the example above:

Method Density altitude Error
Exact, dry air 7,937 ft none
118.8 ft per °C 8,098 ft 161 ft high
120 ft per °C 8,128 ft 191 ft high

On a dry day the rule of thumb errs on the safe side, reading a little high. On a humid day it can read low: with the 20 °C dew point it is 150 ft under the exact figure, because the rule knows nothing about moisture.

Common mistakes

Where the numbers come from

The standard atmosphere is defined in ICAO Doc 7488, and the FAA’s Pilot’s Handbook of Aeronautical Knowledge and Aviation Weather Handbook describe how pilots use it. The density altitude tool shows each step with your numbers under “How we got this.” To read the altimeter setting and temperature straight from a weather report, start with the METAR decoder.

Try it: Density altitude

The calculator below is the real tool, running its worked example. Change any value; nothing leaves your device.

7,937ft

Density altitude is 7,937 ft, about 2,900 ft higher than the field. Expect a longer takeoff roll and weaker climb. Assumes dry air.

The 120 ft per °C rule of thumb gives 8,128 ft (191 ft high).

  • Assumes dry air. Add a dew point to include humidity, which raises density altitude.
Above the field
Pressure altitude
ISA temperature
ISA deviation
118.8 ft per °C rule
118.8 rule error
Provenance
Computed by
aviation.altimetry.density-altitude 1.1.0, core 0.1.0
Model
Air density from station pressure and (virtual) temperature, inverted through the layered ISA density profile; Magnus vapor pressure (Alduchov and Eskridge 1996)
Accuracy
Exact to the ISA definition for dry air; with humidity, vapor pressure is within 0.4% from -40 to 50 °C. Planning aid, not certified for navigation.
Notes
1 shown with the answer
Cites
International Civil Aviation Organization, Manual of the ICAO Standard Atmosphere (extended to 80 kilometres (262 500 feet)); Federal Aviation Administration, Pilot's Handbook of Aeronautical Knowledge, FAA-H-8083-25C; Federal Aviation Administration, Aviation Weather Handbook, FAA-H-8083-28B; Alduchov, O. A., and Eskridge, R. E., Journal of Applied Meteorology, Improved Magnus form approximation of saturation vapor pressure

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Sources

Every number on this page comes from the tools above, which cite their sources on their own pages under "How we got this." Found a mistake? Use "Report a problem" at the bottom of the page.