OK on a more serious note I have been to the Zenith factory n Mexico Missouri ..actually just went up there last week and spent a $1000.00 on some aluminum for a project,..while I was there ..I got a tour ..they have a nice set up,..I am also a member of an EAA chapter that is building a 601,..what got me asking myself questions about the CH's after seeing the wing construction ..some of the bays between the ribs are 22 inches apart ,.and from I was told ...020 6061 T-6 is used for the skins and basically the whole wing construction,..some that own CH's have said the wing beer cans,..meaning the surface actually moves in and out like a beer can if you had squeezed it ..in flight due to thermals and or rough air etc..
The CH that was parked out on the ramp actually showed sign of this with the top flying surface looking like a dented can between the ribs,..I'm sure in flight while the wing is creating lift ..the surface is pulled out so the wing is uniform,..and 6061 T-6 is pretty resilient ,..the 601's actually use the top skin of the wing as the aeleron hinge,..advantage no need for gap seals on top or hinges for the control surface,..the CH's I believe actually use hinges.
I'm not trying to force judgement..just giving a heads up on what I did see concerning the wing construction..you can make your own analysis,.
along with the strut design,.it not being a solid strut ..but split on both leading and trailing struts at the jury strut location and not having an adjustment on either end of the strut.
This evidently is all fine,..or the FAA would ground the CH's as they did the 601's concerning wing construction until the AD's where completed.
the 601's AD was the bellcrank support inside the wing for the aeleron.
you might also want to research recent aircraft accidents in Eldon MO 2 with in 2 weeks of each other,..1 for sure was a CH
Chase