Garmin GPSMAP 96 Owner's Manual - Page 103
Total Air Temperature, Heading, True Airspeed, Head Wind, Wind From, Wind Speed, Density Altitude
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Total Air Temperature-required entry for density altitude/true airspeed calculation. Total Air Temperature (TAT) is the temperature of the air including the heating effect caused by speed. Heading-required entry for winds aloft calculation. Use heading from the aircraft's heading indicator or directional gyro. True Airspeed (calculated figure or user entered)- from entry of calibrated airspeed, baro pressure, and total air temperature. Also can be entered directly for winds aloft calculations. Head Wind (calculated figure)-from entry of heading and true airspeed. Wind From (calculated figure)-from entry of heading and true airspeed. Wind Speed (calculated figure)-from entry of heading and true airspeed. Density Altitude (calculated figure)-from entry of indicated altitude, baro pressure and total air temperature. 96/96C Owner's Manual Main Menu > To calculate true airspeed and density altitude: 1. From the E6B Page, use the ROCKER to highlight the Indicated Altitude field at the top of the page, and press ENTER. 2. Use the ROCKER to enter the altitude shown on your altimeter. Press ENTER when finished. 3. Repeat steps 1 and 2 to enter the Calibrated Airspeed, Baro Pressure, and Total Air Temperature. (For Calibrated Airspeed, use the speed shown on your airspeed indicator. Use the current altimeter setting for Baro Pressure. Total Air Temperature is the temperature of the outside air including the heating effect caused by speed. For most aircraft, this is the temperature reading on a standard outside air temperature gauge.) 4. The calculated figures for True Airspeed and Density Altitude are shown in the designated fields. 95