ok this seems to have become a spitfire thread! lol
GO AWAY!!!

na seriously what i really wanted us to discuss is what is said by this pilot concerning the loops characteristics etc.He seems to feel the 190a4 outperforms the spitfire 61 but not the 66 which i think is very interesting.
What i have also discovered is the 190a5 has increased in weight by some 850lbs over the 190a4 which i think you must agree is a HUGE weight gain.Imagine the reduction in acceleration for one thing.
Another point is later in the book there is a reference to the speed the 190 can dive at and its handling in the pull out. I have to say it doesnt quite match AH's 190s although speeds seem to be VERY near (if not spot on!).here it is:
" The Fw190 has a high rate of dive, the initial acceleration being excellent.The maximum speed so far obtained in a dive is 580mph True at 16,000 ft and at this speed the controls, although slightly heavier, are still remarkably light.One very good feature is that no alteration of trim from level flight is required either during the entry or during the pull-out."
Testing online i saw 580 on the clock and the plane was shaking badly but it wasnt so light on the controls(at least not what id describe as 'remarkably light

). Roll was very laboured and pull out was poor but i cant honestly say this isnt correct as 'remarkably light' has no context does it? this pilot might have forearms like a grizzly bear!!

such a shame these tests dont give us examples of what they think is heavy or light.
one last thing theres a note which reads: "
Note: interrogation of Focke-Wulf personnel after the war revealed that the Fw190 had been dived to mach 0.80, a marked nose down trim change occuring at Mach 0.78 for which the variable incidence tailplane was extremely useful in assisting recovery"
anyone out there describe what they mean here? Again its a shame we have no info on height, airpressure, engine settings etc as without them this 'note' is meaningless really.