Garmin 496 Manuale Proprietario

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To calculate true airspeed and density altitude:
1.   From the 
E6B tab, 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 PressureTotal 
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.) The calculated figures for 
True 
Airspeed and Density Altitude are shown in the designated 
fields.
E6B Tab
Calculated 
figures
Calculated 
figure
Calculated or 
user-entered 
figure
Barometric 
pressure 
from the 
nearest 
METAR
To calculate winds aloft:
1.   Follow the steps in the previous procedure to determine true 
airspeed.  
OR 
Use the 
ROCKER and ENTER keys to manually enter a true 
airspeed figure in the 
True Airspeed field.
2.  Use the 
ROCKER to highlight the Heading field, and press 
ENTER.
3.  Use the 
ROCKER to enter the aircraft heading shown on 
your directional gyro or compass. Press 
ENTER when 
finished.
  The calculated figures for Head Wind, Wind From, and Wind 
Speed appears.
  NOTE: If a True North reference is currently selected as the 
heading reference on your GPSMAP 496, you must enter 
Heading using a True North reference to determine winds 
accurately.
To restore defaults on the E6B tab:
1.  Open the 
E6B tab on the Main Menu.
2.  Press 
MENU to open the options menu.
3.  Highlight 
Restore Default, and press ENTER.
50 
GPSMAP 496 Owner's Manual
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