Garmin aera 500 Series Pilot’s Guide
190-01117-02 Rev. C
Appendix G
184
Overview
GPS Navigation
Flight Planning
Hazar
d A
voidance
Additional F
eatur
es
Appendices
Index
E6B CALCULATOR
The E6B Calculator calculates Density Altitude, True Airspeed, Tail Wind, Wind From,
and Wind Speed, based on information you enter.
Accessing the E6B calculator:
From the '
Home
' Screen, touch
Tools
>
E6B Calc
.
Calculated
Figures
E6B Calculator
Barometric Pressure
from the Nearest
METAR
•
I
ndicated Altitude
—required entry for density altitude/true airspeed calculation.
Enter the aircraft’s altimeter reading.
•
Baro Pressure
—when the unit is receiving XM weather information, the field auto-
matically updates to the barometric pressure of the nearest METAR. If XM weather
information is not available you need to enter the current barometric pressure.
•
Calibrated Airspeed
— required entry for density altitude/true airspeed calculation.
Enter the aircraft’s airspeed indicator value.
•
Total Air Temp
— 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. The temperature reading on a standard outside air temperature gauge found
on most piston aircraft is TAT.
•
Heading
— required entry for winds aloft calculation. Use heading from the aircraft’s
heading indicator or directional gyro.
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