Garmin GPSMAP 96 Owner's Manual - Page 102

E6B Flight Computer, Indicated Altitude, Calibrated Airspeed, Baro Pressure

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Main Menu >  To Create a User Waypoint on a Saved Track: 1. With a saved track shown on the map, use the ROCKER to move the Panning Arrow to the point on the track that you want to mark as a user waypoint. Press ENTER to show the Mark Waypoint Page. 2. To customize the user waypoint explained on page 38, then highlight OK, and press ENTER to save. E6B Flight Computer The E6B Flight Computer in the Main Menu calculates Density Altitude, True Airspeed, and Winds Aloft (Head Wind, Tail Wind, Wind From, and Wind Speed), based upon information you enter. To open the E6B Page of the Main Menu: 1. Press MENU twice to open the Main Menu. 2. Highlight the E6B icon from the vertical list of tabs using ROCKER, and press ENTER to show the setup page. E6B Flight Computer Indicated Altitude-required entry for density altitude/true airspeed calculation. Enter the aircraft's altimeter reading. Calibrated Airspeed-required entry for density altitude/true airspeed calculation. Enter the aircraft's airspeed indicator reading. Baro Pressure-required entry for density altitude/ true airspeed calculation. Use current altimeter setting (barometric pressure). 94 96/96C Owner's Manual

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9µ
96/96C Owner’s Manual
M
AIN
M
ENU
>
To Create a User Waypoint on a Saved
Track:
1. With a saved track shown on the map, use the
ROCKER
to move the Panning Arrow to the
point on the track that you want to mark as a
user waypoint. Press
ENTER
to show the Mark
Waypoint Page.
2.
To customize the user waypoint explained on
page
38
, then highlight
OK
, and press
ENTER
to save.
E6B Flight Computer
The E6B Flight Computer in the Main Menu
calculates Density Altitude, True Airspeed, and Winds
Aloft (Head Wind, Tail Wind, Wind From, and Wind
Speed), based upon information you enter.
To open the E6B Page of the Main Menu:
1.
Press
MENU
twice to open the Main Menu.
2.
Highlight the
E6B
icon from the vertical list of
tabs using
ROCKER
, and press
ENTER
to
show the setup page.
E6B Flight Computer
Indicated Altitude
—required entry for density
altitude/true airspeed calculation.
Enter the aircraft’s
altimeter reading.
Calibrated Airspeed
—required entry for density
altitude/true airspeed calculation.
Enter the aircraft’s
airspeed indicator reading.
Baro Pressure
—required entry for density altitude/
true airspeed calculation.
Use current altimeter
setting (barometric pressure).