<?xml version="1.0"?>

<!--	CG:
	[1] Chapter 2 - CG Limitations
		datum plane: leading edge at root rib (x=0m)
		limits:
		front:	x=0.318m
		rear:	x=0.430m
	[1] Chapter 6 - Mass and balance 
		6.8 - example:
		empty CG:	x=0.366m	(moment/mass)
-->
<mass_balance>
	<ixx unit="SLUG*FT2">   2113.56 </ixx>
	<iyy unit="SLUG*FT2">    746.76 </iyy>
	<izz unit="SLUG*FT2">   2672.67 </izz>
	<emptywt unit="KG" >   590 </emptywt>
	<location name="CG" unit="M">
		<x>   0.366 </x>
		<y>   0.00 </y>
		<z>  -0.10 </z> <!-- guess -->
	</location>
	<pointmass name="Pilot">
		<weight unit="KG"> 80 </weight>
		<location name="POINTMASS" unit="M">
			<x>  0.143 </x> <!-- arm from 6.7.2-->
			<!-- guesses: -->
			<y> -0.23 </y>
			<z> -0.05 </z>
		</location>
	</pointmass>
	<pointmass name="Copilot">
		<weight unit="KG"> 0 </weight>
		<location name="POINTMASS" unit="M">
			<x>  0.143 </x> <!-- arm from 6.7.2-->
			<!-- guesses: -->
			<y> -0.23 </y>
			<z> -0.05 </z>
		</location>
	</pointmass>
	<pointmass name="Baggage">
		<weight unit="KG"> 0 </weight>
		<location name="POINTMASS" unit="M">
			<x>  0.727 </x> <!-- arm from 6.7.3.-->
			<!-- guesses: -->
			<y>  0.00 </y>
			<z>  0.00 </z>
		</location>
	</pointmass>
</mass_balance>
