Aerotheo

Calculator

Density Altitude
Calculation steps

1. Pressure difference height

(1013.25 − QNH) × 27

(1013.25 − 1002.00) × 27 = 304 ft

2. Pressure altitude

Field elevation + Pressure difference height

1411 + 304 = 1715 ft

3. Standard temperature

15 − (Pressure altitude × 2) / 1000

15 − (1715 × 2) / 1000 = 11.6 °C

4. Temperature difference

OAT − Standard temperature

35.0 − 11.6 = 23.4 °C

5. Temperature height

Temperature difference × 120

23.4 × 120 = 2812 ft

6. Density altitude

Pressure altitude + Temperature height

1715 + 2812 = 4526 ft