Enter your field elevation, altimeter setting, and temperature — get density altitude instantly with plain-English warnings about exactly how high DA will affect your takeoff performance.
Use your current METAR or ATIS. Temperature is the most critical variable.
Approximate figures for a normally aspirated trainer at max gross. Always consult your aircraft's POH performance charts.
| Condition | Density alt (ft) | DA vs field | Runway × factor |
|---|
Density altitude is pressure altitude corrected for non-standard temperature — it's the altitude your aircraft "thinks" it's at based on air density. High density altitude means thin air: less lift, less thrust, less engine power, and longer takeoff/landing distances.
As a rough rule: every 1,000 ft of density altitude costs about 3% of engine power in a normally aspirated engine, and takeoff ground roll increases roughly 10% per 1,000 ft of DA above sea level. At 8,000 ft DA, you need approximately 80% more runway than at sea level.
Turbocharged and FADEC-equipped engines maintain power better at altitude. Check your specific aircraft's performance charts — a turbo Cessna 182 behaves very differently from a naturally aspirated 172 at the same density altitude.