C.G. Details
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Select the “C.G. Details” tab in the Manage Aircraft Weight & Balance page.
Enter the following in the multiline.
Weighing Configuration |
The weighing configuration used for weighing the aircraft. |
Forward Limit |
The forward points within which the Center of Gravity must be located during flight. |
The multiline displays the following.
UOM |
The unit of measurement for the forward limit. |
Enter the following in the multiline.
Aft limit |
The aft points within which the Center of Gravity must be located during flight. |
The multiline displays the following.
UOM |
The unit of measurement for the Aft limit. |
Enter the following in the multiline.
Manual Reference # |
The reference manual in which the weight and balance details of the aircraft are recorded. |
To Proceed further
Select the “Reference Details” tab.
Select the “Manage Weighing Conditions” tab.
Select the “Component Weighing Details” tab.
Select the “Aircraft Weighing Details” tab.
Select the “Component Replacements” tab.
