Garmin GTN 625Xi, Pilot'S Manual

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Planning
190-02327-03 Rev. C Pilot’s Guide 4-17
DALT/TAS/Wind Statistics
Compute and display density altitude and current wind conditions. Calculations are
based on current input values.
This information is for planning purposes only.
Density altitude and true airspeed calculations are dependent on indicated altitude, barometric pressure,
and total air temperature. Total air temperature includes temperature and the heating effect of speed, as
read on a standard outside temperature gauge.
Wind data calculations are dependent on aircraft heading and track, true airspeed, and ground speed.
Wind direction is dependent on the NAV Angle system unit setting.
If wind speed is zero, wind direction displays as dashes.
GTN 650Xi SERIES
GTN 750Xi SERIES
Data calculates automatically upon entry. Statistics for the selected leg or route
display on the lower half of the page.
INVALID INPUT DATA INDICATION
Density Altitude Wind Data
•
Pressure altitude corrected for
nonstandard temperature
•
Units display in increments of ten
•
Wind direction and speed
•
Headwind
•
True air speed
To calculate density altitude and wind data, enter all required
input values and then tap
Compute Data .
Statistics display on a dedicated
data page.
To return to the data entry
page, tap
Edit Input Data .
Dashes indicate when input values are invalid.