Garmin 696 Manuale Utente

Pagina di 276
Garmin GPSMAP 695/696 Owner’s Manual
190-00919-00  Rev. F
Appendix F
228
Overview
GPS Navigation
Flight Planning
Hazar
d A
voidance
Additional F
eatur
es
Appendices
Index
E6B CALCULATOR
The E6B Calculator in the Main Menu calculates Density Altitude, True Airspeed, and 
Winds Aloft (Head Wind, Tail Wind, Wind From, and Wind Speed), based on information 
you enter.
Accessing the E6B calculator:
1)  Press the MENU Key twice to open the Main Menu. 
2)  Turn or move the FMS Joystick to highlight ‘E6B Calculator’, and press the 
ENT Key.  The E6B Calculator Page is displayed.
E6B Calculator Page
Calculated 
Figures
Barometric 
Pressure 
from  the  
Nearest 
METAR
Calculated 
or User-
entered 
Figure
•  I
ndicated Altitude—required entry for density altitude/true airspeed calcula-
tion.  Enter the aircraft’s altimeter reading.  A suggested indicated altitude will be 
displayed based on the GPS altitude.
•  Baro Pressure—when the unit is receiving SiriusXM weather information, the field 
automatically updates to the barometric pressure of the nearest METAR.  If SiriusXM 
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