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- May 11, 2010
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Snorting his way across the USA
I'm missing something. It's probably something totally stupid and I'll kick myself after someone points it out. I'm having a brain fart and I can't figure it out. Refer to the sample W&B for a 172R.
We end up with a total weight of 2450 lbs and a moment of 106.2 Kin-lbs. Fine. We go to the moment load envelope graph:
A weight of 2450 lbs and 106.2 Kin-lbs puts us in the normal category. We're done. We're legal to fly.
But we aren't done. Look at the same graph based on CG location and not moment.
Our allowable CG range is from 35" to 47" (and change) from the datum. But where is our total CG arm? We should be able to divide the total weight by the total moment and get it, right?
Wrong. If we divide 2450 by 106.2 we get 23.1" from datum. Not even close. If we extrapolate weight and the utility category line we should be further back than 40.5 inches.
What am I doing wrong? If I take say, my Arrow's W&B calculations and divide total weight by total moment I get the correct CG location. But for whatever reason, not here.
We end up with a total weight of 2450 lbs and a moment of 106.2 Kin-lbs. Fine. We go to the moment load envelope graph:
A weight of 2450 lbs and 106.2 Kin-lbs puts us in the normal category. We're done. We're legal to fly.
But we aren't done. Look at the same graph based on CG location and not moment.
Our allowable CG range is from 35" to 47" (and change) from the datum. But where is our total CG arm? We should be able to divide the total weight by the total moment and get it, right?
Wrong. If we divide 2450 by 106.2 we get 23.1" from datum. Not even close. If we extrapolate weight and the utility category line we should be further back than 40.5 inches.
What am I doing wrong? If I take say, my Arrow's W&B calculations and divide total weight by total moment I get the correct CG location. But for whatever reason, not here.
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