Density altitude calculator
Estimate how pressure and temperature combine to affect the air your aircraft flies in.
Airfield & weather
Live calculationUse the published airfield elevation, current QNH, and outside air temperature at the airfield.
Density altitude
LIVE RESULTAir density expressed as a standard-atmosphere altitude
QNH, QNE & QFE at a glance.
QNH is referenced to mean sea level, QFE to the airfield, and QNE is the standard altimeter setting.
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.
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.
Density altitude ≈ pressure altitude + 120 × (OAT − ISA temperature) ftThis is a simplified dry-air estimate. It does not account for humidity and should not replace aircraft-specific performance data.
Start with pressure altitude.
The pressure altitude calculator focuses on the standard altimeter setting and explains QNH, QNE and QFE in the reference diagram.
Open pressure altitude calculator →Reference: FAA density altitude approximation
Density altitude is approximate. Check current weather and calculate takeoff, climb and landing performance with your aircraft’s approved handbook.