Crabwise

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How do you compare outside-air temperature with the model ISA temperature?

At 8000 ft pressure altitude the model's ISA temperature is −0.84°C, so an OAT of 2°C is 2.84°C warmer than standard and lifts density altitude.

Standard temperature in the app

Crabwise computes the ISA temperature at a pressure altitude as ISA = 15 − 1.98 × PA ÷ 1000, in °C. The deviation is ΔISA = OAT − ISA: positive on a warmer-than-standard day, negative on a colder one. The same pressure altitude then feeds the density-altitude steps, so the deviation and the density altitude always describe one consistent condition.

The 1.98°C per thousand feet lapse is the rounded standard value the app uses for this display; the density calculation itself uses the pressure ratio and the absolute temperature.

Worked example

At 5200 ft pressure altitude, this approximation gives 4.704°C standard temperature. An entered 30°C is therefore 25.296°C above that comparison temperature.

Model standard temperature (°C)
4.704
Entered temperature above model standard (°C)
25.296

Find the deviation

  1. Get pressure altitude first, from elevation and altimeter setting or directly.
  2. Enter the outside-air temperature in °C.
  3. Read the ISA temperature and the deviation lines in the results.
  4. Keep the sign: +2.84 and −2.84 describe opposite conditions.

A slightly warm day at 8000 ft

At 8000 ft the ISA temperature is 15 − 1.98 × 8 = −0.84°C. With an OAT of 2°C the deviation is 2 − (−0.84) = 2.84°C. The pressure ratio is about 0.742782, the temperature ratio about 0.954885, and density altitude comes out at about 8335.79373 ft, a little above the pressure altitude.

ISA temperature at 8000 ft (°C)
−0.84
ISA deviation (°C)
2.84
Density altitude (ft)
8335.79373
ISA temperature at 12000 ft (°C)
−8.76

At 12000 ft the standard drops to −8.76°C, so the same 2°C OAT would be more than 10°C above standard.

Entered at 12000 ft, the same 2°C reading is 10.76°C above standard and density altitude comes out at about 13246.625304 ft, roughly 1247 ft above the pressure altitude instead of about 336 ft at 8000 ft.

Common mistakes

Scope

The deviation compares two temperatures in a dry standard model; humidity and the aircraft's performance tables are outside it. The FAA handbook and NASA pages below describe the standard atmosphere used.

Educational calculation only. Check current aircraft limits, weather, performance and reserve requirements with approved information.

Primary sources and related work