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#1
January 11th 12, 12:48 PM
posted to rec.aviation.soaring
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Measurement of CofG
Hi all,
I’m trying to understand how to determine CofG of my DG-100. In the maintenance manual there is such sentence which I do not understand: “The fuselage must be leveled so that the top of the aft fuselage boom has a tail-down slope of l00 : 3.67.“ I understood that I need to lift up the sailplane tail, but what does 100:3.67 means? To what height? Can you help me with that? BR, Artiom. 
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