Pressure Altitude Calculator
Calculate pressure altitude from field elevation and altimeter setting. Foundation for density altitude and performance calculations.
Inputs
ft MSL
Sea level to ~14,000 ft for US airports
inHg
Typical: 29.82–30.12 inHg
Results
Pressure Altitude
5,000 ft
≈ 5 Eiffel Towers
Pressure Correction0 ft
ISA Temperature at PA105.8°F
Atmospheric Pressure843 hPa
How to Use This Calculator
- Enter your airport's field elevation from the sectional chart or airport directory.
- Enter the current altimeter setting from ATIS, AWOS, or METAR.
- The result is your pressure altitude — use it in POH performance charts.
How the result changes with Altimeter Setting (QNH)
| Altimeter Setting (QNH) | Pressure Altitude |
|---|---|
| 29.92 | 0 ft |
| 29.52 | 5,400 ft |
| 30.42 | 4,500 ft |
What each input means
- Field Elevation
- Airport elevation above mean sea level. Found on sectional charts or airport facility directory (AFD).
- Altimeter Setting (QNH)
- Current altimeter setting in inches of mercury from ATIS, AWOS, or METAR. Standard is 29.92 inHg.
What each result means
- Pressure Altitude
- Use this value for POH performance chart lookups.
- Pressure Correction
- Altitude correction applied for non-standard pressure.
- ISA Temperature at PA
- Standard temperature at this pressure altitude.
- Atmospheric Pressure
- Estimated atmospheric pressure at this pressure altitude.
How this is calculated
Worked example, using the default values
- Pressure CorrectionCorrection = (29.92 − Altimeter Setting) × 1000(29.92 − 29.92) × 1000 = 0 ft
- Pressure AltitudePA = Field Elevation + Correction5,000 + 0 = 5,000 ft
- ISA Temperature at PAISA Temp = 15°C − 2°C × (PA ÷ 1000)15 − 2 × (5,000 ÷ 1000) = 5.0°C (41.0°F)
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