Indicated Airspeed (IAS) Calc
(Back)

TAS

Alt (enter as decimal; 1.0 for 1,000)




TAS =
Alt =0
IAS = 0











True Airspeed (TAS) Calc

IAS

Alt (enter as decimal; 1.0 for 1,000)




IAS =
Alt =0
TAS = 0











Density Altitude Calc

Pressure Altitude

Outside Air Temp (OAT)





Pressure Alt=
Outside Air Temp=
STD temp=15
Density Altitude=-1800


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