I just reread the first page again, and Krusty was absolutely spot on with his anaylsis. tango your 1st post is the one with the flawed logic, as I pointed out. you seem confused over who was correctly "called out" here. 
First logic 101 - an argument that is "absolutely spot on" in it's logic is still wrong if any of it's premises are false. 2nd I was hoping you would sort it out RTHolmes. I fear chasing White Rabbits down various rabbit holes into aero la-la land but if you must here are responses for your shotgun blast of protests of my flawed logic.
1) The SeafireII is heavier than the Spitfire Mk V.Using Pyro's words, which is heavier, a pound of lead or pound of feathers? 6622 pounds of Seafire or 6622 pounds of Spitfire Mk V? Just because the Seafire II could be heavier than the Spitfire Mk V doesn't mean it is at a given instant. It is called aeroDYNAMICS for a reason because the variables are changing. Make faulty assumptions about these changing variables at your peril.
2) The CoG is further back.Please tell me, how does this effect speed or climb performance in our specific case? Really, I can't think of why moving CG horizontally with respect to the thrust line would make a difference.
3) The SeafireII is draggier (sling points & hook assembly).I left this one for last because this is the most rabbity-hole of the rabbit-holes

. First the specifics. Are the sling points removable (the "catapult spools" appear to be)? HTC could have simply modeled the SeafireII with them off. Bye-bye draggy catpult spools. What about the arrestor hook assembly? The arrestor hook looks like it's stowed and not flapping out in the wind when not deployed. Could I be wrong? You bet.
But this is where it really gets good. Let's say I'm wrong & we do need to account for the drag they add. Just exactly how much impact would the drag have? 10%? 1%? .1%? To claim it's wrong because we've left them out of the physics without knowing the quantifiable impact of leaving them out leads us down a path of aero infinite regress lala land. All our fundamental aero maths are based on reasonable approximations where stuff get's left out all the time. Just because something is left out doesn't mean we don't have a reasonable approximation. Otherwise we might as well go back to cave drawings in aero because none of our aero science is any good.
Cheers,