content_image/545054.jpg content_image/545055.jpg content_image/545056.jpg content_image/545050.jpg content_image/545049.jpg
<img src='content_image/545054.jpg'>

The airplane in this example was weighed to determine its basic empty weight (BEW) and empty weight center of gravity (EWCG). The weighing conditions and results are: 

Weight with fuel drained and oil full: 

<img src='content_image/545055.jpg'>

## Determine the Loaded CG 

First, add the weights indicated by the individual scales and then subtract the tare weights to determine the BEW. Next, using the BEW and EWCG, the loaded weight and CG of the aircraft can be determined with data from Figure 6-2,  using a chart such as the one in Figure 6-3 . 

The aircraft is loaded as shown: 

<img src='content_image/545056.jpg'>

## Chart Method Using Weight, Arm, and Moments 

Make a chart showing the weight, arm, and moments of the airplane and its load. 

<img src='content_image/545050.jpg'>

<img src='content_image/545049.jpg'>

