Aviation & Aeronautics
Intermediate

Density Altitude

Pressure altitude corrected for non-standard temperature; higher DA reduces performance.

Formula

DA=PA+120(OATISAtemp)DA = PA + 120(OAT - ISA_{temp})

Variables

DADensity altitude (ft)
PAPressure altitude
OATOutside air temp (°C)
ISA_{temp}Standard temp

Example

On a hot day a runway can feel thousands of feet “higher,” sapping engine and wing performance.

Did You Know?

On a hot day at a high airport, density altitude soars and aircraft performance drops — a known killer in aviation.