People who want to have a FIGHTER plane that has a very high power to weight ratio and is exceptionally nimble and manueverable while still being very stable and forgiving at low speeds are completely ignorant of the laws of physics and aerodynamics. Nimble and maneuverable FIGHTER planes handle that way because they are more directionally unstable. Adding a high power to weight ratio only makes it worse.
I suppose we could make the case that HTC is biased against the P-38:
1. The P-38L is modeled with the Allison -17 engines and NOT the -30 engines, robbing it of over 250HP.
2. Widewing has had a couple of guys we know who flew real P-38's in here, and they say it has a serious lack of elevator authority.
3. The P-38 has autoretract flaps here in AH. It didn't have them, ever.
4. The P-38 stall and spin model does NOT match the test pilot reports by ANY of the Lockheed test pilots. In fact, it isn't even close.
5. The effects of compression are modeled well below 20,000 feet, while no pilot ever interviewed says it was a problem. Most P-38 pilots say you could dive a pre J-25-Lo model from 20,000 feet with impunity, and a post J-25-Lo model from over 25,000 feet easily.
Now, any number of long term hardcore P-38 flyers have argued these points for years. There have been VERY heated disagreements between Dale and several of the aforementioned P-38 flyers over all of the above points. However, I have yet to see anyone of any consequence seriously claim that HTC has some sort of conspiracy going on to handicap the P-38.
The other thing I haven't seen is P-38 flyers continually, repeatedly, and constantly spamming channel 200 all night and every night about the HTC conspiracy against the P-38. I can't say that for the LW contingent. The other night, I listened for TWO HOURS about how the FW 190 was completely porked. The whole time I was FLYING an FW 190 D9 and landing kills.