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ALTITUDE CALCULATIONS

Density altitude calculator

Estimate how pressure and temperature combine to affect the air your aircraft flies in.

Instant resultsPressure altitude shown as a stepNo account needed

Airfield & weather

Live calculation

Use the published airfield elevation, current QNH, and outside air temperature at the airfield.

ft MSL
Use −1,500 to 20,000 ft.
hPa
Use 800–1,100 hPa.
°C
Use −80 to 60 °C.
Pressure units

Density altitude

LIVE RESULT
Temperature-adjusted estimate8,008 ft

Air density expressed as a standard-atmosphere altitude

Pressure altitude 5,500 ftISA temperature at pressure altitude 4.1 °COAT versus ISA +20.9 °C
THREE ALTIMETER REFERENCES

QNH, QNE & QFE at a glance.

QNH is referenced to mean sea level, QFE to the airfield. The dotted QNE datum moves relative to QNH as the pressure setting changes.

How it works
QNE · DOTTED DATUMAIRFIELD5,500 ft MSLQNH · SEA LEVEL1013.25 hPaOCEAN · MEAN SEA LEVELQNE · STANDARD SETTING1013.25 hPaQFE · AT AIRFIELD827.42 hPaAltimeter reads ≈ 0 ft here

Swipe diagram to see all three settings →

Illustrative terrain; vertical distances are not to scale. The dotted QNE line shows the implied standard-pressure datum, not a physical pressure layer. QFE is estimated from QNH and elevation.
QNH1013.25 hPa

Reads 5,500 ft MSL at the airfield.

QNE1013.25 hPa

Reads 5,500 ft pressure altitude at the airfield.

QFE827.42 hPa

Reads approximately 0 ft at the airfield reference datum.

THE METHOD

From pressure to density.

We first calculate pressure altitude from airfield elevation and QNH. Then we compare outside air temperature with standard ISA temperature at that pressure altitude. Warmer-than-standard air raises density altitude; colder-than-standard air lowers it.

Planning approximationDensity altitude ≈ pressure altitude + 120 × (OAT − ISA temperature) ft

Enter QNH in hPa or inHg and temperature in °C. Pressure values display to two decimal places and altitude to the nearest foot; calculations retain full precision. This dry-air estimate excludes humidity.

WORKED EXAMPLES

Density altitude in practice.

01

Warm high airfield

At 5,500 ft, QNH 1013.25 hPa and 25 °C, pressure altitude is 5,500 ft and estimated density altitude is 8,008 ft.

02

Standard sea level

At 0 ft, QNH 1013.25 hPa and 15 °C, both pressure altitude and estimated density altitude are approximately 0 ft.

Density altitude questions

What makes density altitude increase?+

Higher temperature and lower pressure reduce air density and generally raise density altitude.

Does this calculator include humidity?+

No. It uses the common dry-air planning approximation, so humid conditions can make actual density lower than this estimate suggests.

Can I use density altitude as takeoff performance data?+

No. Use the approved aircraft handbook and current conditions for takeoff, climb and landing performance.

A planning aid. Use approved performance data.

Density altitude is approximate. Check current weather and calculate takeoff, climb and landing performance with your aircraft’s approved handbook.