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.
Estimate how pressure and temperature combine to affect the air your aircraft flies in.
Use the published airfield elevation, current QNH, and outside air temperature at the airfield.
Air density expressed as a standard-atmosphere altitude
QNH is referenced to mean sea level, QFE to the airfield. The dotted QNE datum moves relative to QNH as the pressure setting changes.
Swipe diagram to see all three settings →
Reads 5,500 ft MSL at the airfield.
Reads 5,500 ft pressure altitude at the airfield.
Reads approximately 0 ft at the airfield reference datum.
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.
Density altitude ≈ pressure altitude + 120 × (OAT − ISA temperature) ftEnter 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.
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.
At 0 ft, QNH 1013.25 hPa and 15 °C, both pressure altitude and estimated density altitude are approximately 0 ft.
Higher temperature and lower pressure reduce air density and generally raise density altitude.
No. It uses the common dry-air planning approximation, so humid conditions can make actual density lower than this estimate suggests.
No. Use the approved aircraft handbook and current conditions for takeoff, climb and landing performance.
Density altitude is approximate. Check current weather and calculate takeoff, climb and landing performance with your aircraft’s approved handbook.