Enter your field elevation and altimeter setting — in inHg or hPa — and get pressure altitude instantly. The formula and worked examples are below.
Pressure altitude is your field elevation corrected for non-standard pressure: the altitude your altimeter reads with 29.92 inHg (1013.25 hPa) set. It's the starting point for density altitude and the number most POH performance charts are built around. This tool uses the standard aviation formula and updates the moment you type — no button to press.
The calculator above uses the formula every pilot learns:
Pressure Altitude = Field Elevation + (29.92 − Altimeter Setting) × 1,000
The altimeter setting is in inches of mercury. If your setting is below 29.92, the term is positive and pressure altitude sits above field elevation; if it's above 29.92, pressure altitude drops below field elevation. Working in hPa? Convert first with inHg = hPa × 0.02953 (so 1013.25 hPa = 29.92 inHg), then apply the same formula — the calculator does this conversion for you when you switch the unit toggle.
A field at 5,000 ft with an altimeter setting of 29.42 inHg (a low-pressure day):
PA = 5,000 + (29.92 − 29.42) × 1,000 = 5,000 + 500 = 5,500 ft
The half-inch of low pressure adds 500 ft: the airplane's altimeter and performance behave as if the field were 500 ft higher than it is. Switch the tool to hPa and enter 996 hPa for the same field — you'll get the same answer, because 996 hPa is essentially 29.42 inHg.
On its own, pressure altitude rarely decides a flight — but it's the mandatory first step to the number that does: density altitude. Density altitude takes pressure altitude and corrects it for temperature, giving the altitude the airplane actually performs at. Get pressure altitude wrong and every downstream performance figure is wrong too. It's also the reference for flight levels, altimetry above the transition altitude, and most takeoff and landing charts in your POH. In short: pressure altitude is the clean, temperature-free baseline, and density altitude is what you plan the takeoff around.
Next step — add temperature for Density Altitude
To understand how these two numbers relate, read Pressure Altitude vs Density Altitude. For the full density-altitude method with examples, see How to Calculate Density Altitude, and for what high numbers do to your runway, how density altitude affects takeoff and climb.