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#1
January 6th 07, 02:47 PM
posted to rec.aviation.piloting,rec.student.aviation
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Procedure for calculating weight and balance
The manual for my aircraft gives figures for MOM and ARM at various
stations, but it doesn't actually explain how to use these to calculate weight and balance. I want to place the load so that the aircraft neither pitches down nor pitches up. Can someone provide me with a pointer to an explanation of the procedure on the Web somewhere? -- Transpose mxsmanic and gmail to reach me by e-mail. 
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