Hey everyone! Today I was reading up about the P-38L ... according to my sources, the L variant had internal cockpit heating, windsheild defrosters and engine problems at high altitude were all fixed. Is any of this actually true? I've been checking on countless sites and still havent found truly reliable information.
Also, I've been lead to believe that the P-38's actual climb rate under 5000' exceeded 4,500'/min. However in AHII, the climb is 1000'/min less.