Steve - in answer to your question about C of G: I found a great site at http://www.adamone.rchomepage.com/cg_calc.htm on which you can calculate C of G. The only difficult factor I have found is that the Spitfire does not have a "wing tip chord" as it effectively comes to a point. However, I measured everything at the end of the aileron and also at the very end of the wing tip and here are the two results: With Static Margin (SM) at 10% (must be between 5% and 15%) the C of G is back from the leading edge by 4.75 inches using aileron-end measurements or 5.25 inches using end-of-wing measurements. 5 inches is therefore the average and looks to be spot on! I only did the calculations AFTER setting the plane up! About 4 inches would equate to a 15% SM which the web page says is best for greater stability BUT makes the plane nose heavy. Seems to match practical experience.