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Originally Posted by rodrv6
The nose gear wouldn't be supporting any more or less weight than with a Lycoming or any other engine up front. If the Subaur installation was significantly heavier to the point of adding excessive weight to the nosewheel, then the fwd C of G would be too far forward and out of limits. The pilot reports a light fuel load, 80 lbs in the baggage compartment, and two reasonably sized people on board. Not exactly a forward C of G condition.
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I don't think we can be so sure of that.
The empty C.G. could be outside the limit but the airplane wasn't empty.
An RV-7A with an empty weight of 1199 Lbs! This Subaru installation is advertised to be comparable in weight to an IO-360 Lycoming. The Lyc produces empty weights that are typically around 1135 lbs or so for an average on an RV-7A. This particular airplane was probably at least 50 lbs heavier than most RV-7A's.
Just because there was weight in the back doesn't mean it was light on the nose. It is possible that with all that weight the C.G. was somewhere near the mid point or even further fwd than that. I know of one Egg. Subaru equiped RV-9A that when weighed was about 100 lbs heavier than an average weight for an RV-9A with an O-320 Lyc. Pretty much the entire additional weight was on the nose wheel when positioned in a level flight attitude on the digital scales (which is worse case compared to sitting in a three point attitude on the ground, but still a lot of extra weight on the nose).
Scott