Quote:
Originally Posted by Zero4Zulu
I'm working on rebuilding a RV6A. The engine is a O320 B3B (Conical Mnt.) I have changed the sump to the more forward carb. location from the far aft type sump. The builder had 3/8" spacers behind the engine mounts to make room for the FAB and nose gear interference with the previous sump.
This plane has a Hartzell constant speed prop. I'm also replacing the spinner and bulkheads to fix a poor job there also.
Between these two issues, it means I'll need to move the cowlings aft at least 3/8". I am redoing the cowl attachments anyway so I don't mind that.
Question is..............how much will moving the engine back 3/8" effect the CG and is this a good thing since it is a constant speed prop with more weight up front?
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The change in empty CG location will be:
(distance the weight is moved) x (amount of weight moved) / (empty weight)
E.g., if you figure that engine, prop, etc weigh 400 lb, and your empty weight is 1000 lb, then moving the engine back 3/8" will move the aircraft's CG back 3/8 x 400 / 1000 = 0.15"