Brett, would you please explain the adjustment process for the vent tube?
Usually, if you make it rigid, you can rotate the tube in the stopper, so the far end moves up and down. The position of the far end of the vent tube is the reference for the entire tank. So instead of shimming the entire tank up or down, you move just the end of the tube. Once you find the right spot, you can solder a piece of brass in between the 3 tubes to hold it in place permanently.
Of course, the usual procedure for determining how to adjust it applies. Fly upright, get an accurate lap time (take off, fly level for several laps, then time 3 laps, then divide by 3), flip over inverted, repeat. If it is faster upright, move the vent tube (or entire tank) higher, if it's faster inverted, move the vent tube lower. It can be pretty sensitive, so I usually shim in 1/32" increments until it's close, then 1/64 or a few layers of masking tape.
Note that this should be done, ideally, *entirely* on the upright/inverted level flight lap times. Many will recommend shimming it based on inside/outside loops, and setting it based on where in the arc of the loop it breaks into a 2-stroke. Like, it breaks at the 90 degree mark upright and at the 120 degree mark inverted, move the tank up. You can do that in a pinch, but recheck in level flight. If the level flight tank position needs to be significantly different from the maneuvering tank position (like more than 1/32"), there's some other issue with the engine.
This effect has plagued my buddies and I for years because the effect seems to be grossly exaggerated in dry sea level air. I have had engines that ran 5 seconds upright and 6 seconds inverted, with 1/4" shim, that still ran faster on outsides. We (and really, Ted, before I even moved here) discovered this in the late 70's when schneurle engines were tried. This is why wre hung on with baffle-piston engines until the bitter end - none of could get acceptable run symmetry with schneurle engines, despite the fantastic increase in power, it still wasn't worth it. The effect can sometimes disappear completely or be greatly reduced in humid and relatively thin air and many of the midwest/southeast engine reworkers have claimed it's nonsense. Some engines are far more prone to it than others and appear hopeless, but any of the normal engines (PA or RO-Jett) are capable of a symmetrical run most of the time with changes to the intake and fuel supply system.
Note that there are many other small details of engine run that matter a lot. Like this thread:
http://stunthanger.com/smf/index.php/topic,28567.msg275948.html#msg275948 Paul and I were discussing this at Golden State, with regard to the lower bound for the Igor feedback control system. It can be made to overdo the airspeed control, and back off in spots you don't necessarily want. This is exactly the same effect I was discussing in the thread above about engine feedback based on the oil content. This is why it is so complex to get these engines, even the really excellent systems we have now, running exactly the right way. And also why most of what you hear about it is utter and complete bullshit.
Brett