Garmin GPSMAP 96 Owner's Manual - Page 109

Empty Aircraft, Restore Default, To perform weight and balance, calculations

Page 109 highlights

Weight & Balance Page Empty Aircraft-retains aircraft empty weight and arm figures, retains other arm figures, but zeros all other weight values. Restore Default-restores all settings to zero. Options Menu Main Menu >  To perform weight and balance calculations: 1. From the Aircraft Profile Page, use the ROCKER to select Weight & Balance at the top of the page. 2. Use the ROCKER to highlight a weight field, and press ENTER. 3. Use the ROCKER to enter the weight figure. Press ENTER when finished. 4. Use the ROCKER to highlight the corresponding arm field, and press ENTER. 5. Use the ROCKER to enter the arm figure. Press ENTER when finished. 6. Repeat steps 2 through 5 above until all figures are entered. The calculated moment, weight, and CG figures appear at the bottom of the page. Keep in mind that the "Aircraft" (empty weight/arm) figures must be entered as a reference to calculate a valid moment, weight, and CG. 96/96C Owner's Manual 101

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96/96C Owner’s Manual
²0²
M
AIN
M
ENU
>
Weight & Balance Page
Empty Aircraft
—retains aircraft empty weight and
arm figures, retains other arm figures, but zeros all
other weight values.
Restore Default
—restores all settings to zero.
Options Menu
To perform weight and balance
calculations:
1. From the Aircraft Profile Page, use the
ROCKER
to select
Weight & Balance
at the
top of the page.
2.
Use the
ROCKER
to highlight a weight field,
and press
ENTER
.
3.
Use the
ROCKER
to enter the weight figure.
Press
ENTER
when finished.
4.
Use the
ROCKER
to highlight the
corresponding arm field, and press
ENTER
.
5.
Use the
ROCKER
to enter the arm figure.
Press
ENTER
when finished.
6.
Repeat steps 2 through 5 above until all
figures are entered. The calculated moment,
weight, and CG figures appear at the bottom
of the page. Keep in mind that the “Aircraft”
(empty weight/arm) figures must be entered
as a reference to calculate a valid moment,
weight, and CG.