I was wondering about camber on Cessna taildraggers. I've owned three of them now, the first two (esp my 170) had very obvious positive camber (top of wheel out). My 180 is set up with pretty close to zero or neutral camber, at least to the naked eye. My series 100 service manual says that (on the old greased plates, of course) with tanks & cabin empty, there should be approx. 4 to 6 degrees of positive camber. This will give approx. neutral camber at gross weight.
I see each side has a extremely tapered axle shim that if removed should give me a nice positive camber.I'm getting ready to pull off the wheels & repack the bearings as part of the annual, so this would be the ideal time to address this. I do plan on carefully measuring the shims, hopefully they're just tapered in the one direction so that by removing them I won't be screwing up the toe-in. I don't wanna do that because the airplane handles really well as it is.
Besides doing it just cuz the book says so, it seems like you want more rubber on the road as you approach gross weight. Plus, if you're lightly loaded much of the time, positive camber tends to concentrate tire wear on the outside half. You can flip the tire on the wheel every year or two and get twice as much mileage out of them.
Thoughts?


..... Find a good Cessna mechanic and prevail upon them (or bully them) to check gear alignment.