So what exactly am I going to find out by reading it? Will it have the answer to my question about the P-38 using a yoke or are those just stories written by pilot and what they done? All I want to "learn" about it is why did it have a yoke? Widewing explained one reason but that's only for the early models. If you will tell me that that text explains why the L models had yokes I'll go and read all that stuff. But if you really read it I don't see why you can't just explain it.
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Exactly why I said read it yourself. Either you want to find and read the truth, or you don't. If you merely want someone to "tell you", as it appears, then you'll simply decide, as you already have, that it does not fit what you want to believe.
It's simple. Warren Bodie was a Lockheed engineer, and wrote the definitive work on the P-38, plain and simple. Tony Levier was one of the premier Lockheed test pilots. Those are two of the "go to guys" on the P-38. You can either read what they wrote, and accept it as fact, or you can continue to believe what you want to believe.
What Widewing explained to you about the pre J-25-Lo models explains it for all models. You assume the hydraulic boost systems do not work. In a combat aircraft especially, you design it to fly with as many systems in "failure mode" as is possible, so that those systems being damaged in combat do not lead to aircraft loss. So, despite the J-25-Lo and later models having hydraulic boost assist, the plane must be easily flyable without hydraulic assist, so the yoke remains, in order to assure that is indeed the case.