Jeffrey Bell - Experimental Aircraft Builder's Log

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Date: 8-7-2020
Number of Hours: 3.00
Manual Reference:
Brief Description: Weight & Balance Determination

There was 1 gallon of fuel in each wing, the weight and moment had to be subtracted out Empty Aircraft Weight Arm Moment Right Wheel------------ 498.40--- 68.37----- 34075.61 Left Whee--------------- 501.20--- 68.37----- 34267.04 Tailwheel---------------- 58.20--- 251.5----- 14637.30 Total-----------------------1057.80------------------ 82979.95 CG-------------------------- 78.45

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