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You are here: home->amg->C01->C.8.1.5.3.A.1

8153
When computing weight and balance, an airplane is considered to be in balance when
A) all moment arms of the plane fall within CG range.
B) the average moment arm of the loaded airplane falls within its CG range.
C) the movement of the passengers will not cause the moment arms to fall outside the CG range.

 

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