The National Oceanic and Atmospheric Administration (NOAA) published the following formula for directly converting atmospheric pressure in millibars () to pressure altitude in feet ():
In aviation, pressure altitude is the height above a standard datum plane (SDP), which is a theoretical level where the weight of the atmosphere is 29.921 inches of mercury (1,013.2 mbar; 14.696 psi) as measured by a barometer. It indicates altitude obtained when an altimeter is set to an agreed baseline pressure under certain circumstances in which the aircraft’s altimeter would be unable to give a useful altitude readout. Examples would be landing at a high altitude or near sea level under conditions of exceptionally high air pressure. Old altimeters were typically limited to displaying the altitude when set between and . Standard pressure, the baseline used universally, is hectopascals (), which is equivalent to or inches of mercury (). This setting is equivalent to the atmospheric pressure at mean sea level (MSL) in the ISA. Pressure altitude is primarily used in aircraft-performance calculations and in high-altitude flight (i.e., above the transition altitude).
QNE is an aeronautical code Q code. The term refers to the indicated altitude at the landing runway threshold when or is set in the altimeter's Kollsman window. In other words, it is the pressure altitude at the landing runway threshold.
For example, if the airfield elevation is and the altimeter setting is , then
For example, if the airfield elevation is and the QNH is , then
Aircraft Mode “C” transponders report the pressure altitude to air traffic control; corrections for atmospheric pressure variations are applied by the recipient of the data.
The relationship between static pressure and pressure altitude is defined in terms of properties of the ISA.
- Flight level
- Cabin altitude
- Density altitude
- Standard conditions for temperature and pressure
- Barometric formula
- "Pressure Altitude" (PDF).
- Pilot’s Handbook of Aeronautical Knowledge (FAA-H-8083-25B), 2016, Chapter 4, p 4-4