TRUE AIRSPEED (TAS) CALCULATOR

<-- Enter Indicated Altitude Feet    Meters

<-- Enter Altimeter Setting Inches    hPa

<-- Enter Temperature °C    °F

<-- Enter Indicated or Calibrated Airspeed (KTS or MPH)

CALCULATED RESULTS

True Airspeed (TAS):

Density Altitude (DA):

Pressure Altitude (PA):

Note: standard pressure is 29.92126, if you're trying to test for zero.

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