I don't compare the Finnish Brew to the F2A. I compare it to what is in the MA and how it performs relative to those aircraft. I feel the plane should and does turn sharp enough to hit itself in the butt. Where I always find myself scratching my head is its apparent ability to make those turns with little to no loss in energy. It pulls off turns that make a Spit16 pilot jealous. The HP to Weight ratio doesn't bear out how quickly it seems to accelerate after making those hard turns. Since we are all (I hope) in the same virtual enviornment, this leads me to believe something is wrong with the drag model of the aircraft. I haven't done any wind tunnel testing but, looking at the plane, I wouldn't think it is what you would call a "slick" bird. I feel the plane accerates very similar to a spit which has a MUCH better HP/weight ratio when it should accelerate much like a FM2.
I did a little digging and found some HP numbers off the Internet (I know) so pleas correct if I got them wrong. Then I went to the hangar and loaded the planes with 25-30 minutes of fuel (MA 2.0 burn) and came up with the following "combat" weights to try to keep things even. Now I know this doesn't take all kinds of other factors into account (drag, wing loading, prop efficiency and so on) but it's a good indicator of what a plane should be able to do. There's no replacement for sheer power.
Brew-950hp. 5401lbs. 5.68lbs per HP
FM2-1350hp. 7286lbs 5.39lbs per HP
Spitfire 16-2200hp 8574lbs 3.89lbs per HP
Based on my MA experience while flying various Jugs for probably close to a decade, I find it as difficult to pull away from a manuvering Brew as I do a Spit16. While pulling away from a manuvering FM2 seems to be no problem.
What does this prove? Nothing really. But it hasn't helped me stop scratching my head or cursing to myself when a Brew does a 90-180 degree turn and stays latched to my 6 for ten plus seconds before I can start to pull away.
There's something "fishy" about the Brew and there is a large part of the community that thinks so.