Travel calculators

Density Altitude Calculator

Updated Sep 1, 2026 By Jehan Wadia
Rate Formulas
STAGE 1 Pressure Altitude
Elevation unit
The airport / station elevation above mean sea level.
Altimeter unit
This is the value displayed in your altimeter's Kollsman window — not raw station pressure.
Pressure Altitude (Stage 1 output)
0 ft | 0 m
STAGE 2 Density Altitude
Pressure altitude unit
Auto-filled from Stage 1 — you may override.
Temperature unit
Current air temperature at the field.
Moisture input method
%
Relative humidity, 0% = dry air baseline.
DENSITY ALTITUDE
0 ft
0 m
Excellent: Air density is near standard.
Absolute (Station) Pressure
29.92 inHg
1013.2 hPa
Air Density
1.2250 kg/m³
0.07647 lb/ft³
Relative Air Density
100.0%
of ISA sea-level (1.225 kg/m³)
ISA Temperature Deviation
ISA +0.0°C
ISA temp at PA: 15.0°C
Estimated AWOS / ASOS Density Altitude
Step-by-Step Solution
Density Altitude vs. Outside Air Temperature

Introduction

Density altitude is the altitude at which the air around you actually "feels" like it behaves, based on its true thickness. Hot, humid, or low-pressure air is thinner than normal. Thin air means airplane wings produce less lift, engines make less power, and propellers grab less air. This makes takeoff rolls longer and climb rates slower. Pilots, flight instructors, and dispatchers need to know the density altitude before every flight to stay safe.

This free density altitude calculator works in two clear stages. In Stage 1, you enter your field elevation and altimeter setting to find pressure altitude. In Stage 2, you add the outside air temperature and humidity to get the final density altitude. The tool also shows you air density, station pressure, ISA temperature deviation, and a full step-by-step solution so you can see exactly how each number was found. A built-in chart plots how density altitude changes as temperature rises or falls, giving you a quick visual reference for flight planning.

How to Use Our Density Altitude Calculator

Enter your airport conditions below to find the density altitude at your location. The calculator will return your density altitude in feet and meters, along with air density, station pressure, ISA deviation, and a full step-by-step solution.

Field / Station Elevation: Type the elevation of your airport or weather station above sea level. You can switch between feet and meters using the unit buttons.

Altimeter Setting: Enter the current altimeter setting shown in the Kollsman window of your altimeter. This is not raw station pressure. You can enter it in inHg or hPa.

Pressure Altitude: This field fills in automatically from the elevation and altimeter setting you entered above. You can type over it if you already know your pressure altitude. Click "Re-sync from Stage 1" to restore the auto value.

Outside Air Temperature (OAT): Enter the current air temperature at your location. You can choose between °F, °C, or Kelvin.

Moisture Input: Pick either Relative Humidity or Dew Point. If you choose Relative Humidity, enter a value from 0 to 100 percent. If you choose Dew Point, enter the dew point temperature. Set this to 0% humidity if you want a dry-air result that matches most AWOS reports.

Press the Calculate button to see your results. Press Reset / Clear All to start over with standard day values.

What Is Density Altitude?

Density altitude is how the air around you "feels" to an airplane. It tells you how thick or thin the air really is at your location. When the air is thin, wings produce less lift and engines make less power. This means your plane needs more runway to take off and climbs slower than normal.

Density altitude is not a true height above the ground. It is the altitude in the standard atmosphere where the air density matches what you have right now. For example, if you are sitting at a field that is 2,000 feet above sea level but the density altitude is 5,000 feet, your airplane will perform as if it were at 5,000 feet.

What Changes Density Altitude?

Three main things raise density altitude and make air thinner:

  • High temperature: Hot air is less dense than cold air. On a hot summer day, density altitude can be thousands of feet higher than the actual field elevation.
  • Low air pressure: When the barometric pressure drops, the air becomes thinner. Your altimeter setting directly reflects this.
  • High humidity: Moist air is lighter than dry air. Water vapor molecules weigh less than the nitrogen and oxygen molecules they replace. Many pilots forget this factor, and most AWOS and ASOS stations do not include it in their density altitude reports.

Why Density Altitude Matters for Pilots

Every pilot needs to know the density altitude before flying. It affects takeoff distance, climb rate, engine power output, and true airspeed. High density altitude is one of the leading causes of takeoff and landing accidents, especially at high-elevation airports during summer months. Alongside density altitude, pilots should also evaluate crosswind components and estimated flight times as part of thorough preflight planning.

As a general rule, a density altitude below 1,000 feet means near-standard conditions. Between 1,000 and 3,000 feet, expect slight performance loss. Above 3,000 feet, pilots should carefully check their aircraft performance charts. Above 6,000 feet, performance drops significantly and extra caution is needed.

How This Calculator Works

This calculator uses a two-stage process. In Stage 1, it converts your field elevation and altimeter setting (the Kollsman window value) into pressure altitude. In Stage 2, it combines that pressure altitude with the outside air temperature and moisture level to find the true density altitude. It uses the virtual temperature method, which accounts for humidity, a step simpler calculators skip.

The results also show you the actual station pressure, air density in both metric and imperial units, relative air density compared to sea level, and the ISA temperature deviation. A full step-by-step solution with formulas is provided so you can verify every number yourself.


Formulas used

Station (Absolute) Pressure from Altimeter Setting
P_{sta} = P_{alt} \times \left(1 - 6.8756 \times 10^{-6} \times E\right)^{5.2559}
Pressure Altitude from Station Pressure
PA = 145366.45 \left(1 - \left(\frac{P_{sta}}{29.921}\right)^{0.190284}\right)
Saturation Vapor Pressure (Tetens Formula)
e_s = 6.1078 \times 10^{\frac{7.5\,T}{237.3 + T}}
Virtual Temperature (Moisture Correction)
T_v = \frac{T}{1 - 0.378 \dfrac{e}{P}}
Air Density
\rho = \frac{P}{R_d \cdot T_v}
Density Altitude from Air Density
DA = 145442.5 \left(1 - \left(\frac{\rho}{1.225}\right)^{0.234969}\right)

Frequently asked questions

What is pressure altitude and how is it different from field elevation?

Field elevation is the actual height of your airport above sea level. It never changes. Pressure altitude is what your altimeter reads when you set it to the standard pressure of 29.92 inHg (1013.25 hPa). It changes with the weather. When air pressure is lower than standard, pressure altitude is higher than field elevation. When pressure is higher than standard, pressure altitude is lower. This calculator finds pressure altitude for you in Stage 1.

What is the Kollsman window value and where do I find it?

The Kollsman window is the small window on your altimeter that shows the barometric pressure setting. When you turn the altimeter knob, the number in this window changes. You set it to the current altimeter setting given by ATC, ATIS, AWOS, or ASOS. Enter that number into the Altimeter Setting field. Do not enter raw station pressure. They are different values.

Should I enter relative humidity or dew point?

Use whichever value you have. If you know the relative humidity, pick that option and type it in. If your weather report gives a dew point temperature, pick the Dew Point option instead. Both methods give the same final answer. Dew point is often easier to find on a METAR weather report.

Why does humidity raise density altitude?

Water vapor is lighter than the nitrogen and oxygen it replaces in the air. When air holds more water vapor, the overall air mixture weighs less per cubic foot. Lighter air means lower air density. Lower air density means a higher density altitude. The effect is small in cool weather but can add a few hundred feet on hot, humid days.

What does the ISA temperature deviation mean?

ISA stands for International Standard Atmosphere. It defines a "normal" temperature for every altitude. At sea level, the ISA temperature is 15°C (59°F), and it drops about 2°C for every 1,000 feet of altitude. The ISA deviation tells you how much warmer or cooler the actual air is compared to this standard. A positive number like ISA +10°C means the air is 10 degrees warmer than standard, which raises density altitude.

What is the Pressure Altitude override and when should I use it?

The Pressure Altitude field in Stage 2 is auto-filled from Stage 1. If you already know your exact pressure altitude from another source, such as your altimeter set to 29.92 or from a flight plan, you can type over it. A badge will appear to show the value has been overridden. Click the Re-sync button to go back to the auto-calculated value.

What density altitude is too high to fly safely?

There is no single cutoff for all aircraft. As a general guide, below 1,000 ft is excellent. Between 1,000 and 3,000 ft, expect minor performance loss. Between 3,000 and 6,000 ft, takeoff rolls get noticeably longer and climb rates drop. Above 6,000 ft, performance drops a lot and careful weight and distance planning is needed. Always check your aircraft's performance charts for the specific numbers.

How does temperature affect density altitude the most?

Temperature has the biggest impact on density altitude. Hot air expands and becomes thinner. A 10°C increase in temperature can raise density altitude by roughly 600 to 700 feet. On a hot summer afternoon, the density altitude at a low-elevation airport can easily climb thousands of feet above the actual field elevation.

Does wind affect density altitude?

No. Wind does not change air density, so it does not change density altitude. However, wind does affect takeoff and landing performance separately. A headwind shortens your takeoff roll and a tailwind lengthens it. You should account for wind and density altitude separately during flight planning.