Recently, Mxsmanic posted:

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?

The calculations are simple math. Why would you need a pointer to anything
but an elementary math book?

Neil