I don't know why they added the additional Lord Dyna-focal mounts to the engine mount. However I found it ironic that when I attempted to comment on the additional Lord Dyna-focal mounts I was shut down by the person who told me and I quote "C'mon Johnny, this isn't a bunch of cowboys doing stuff without engineering, Stu and Nelson engineered that addition. Unlike when you guys built the first mount." Ironic because of the fact that the Lord Dyna-focal mount engineering representative to Lockheed was the guy that did the calculations based on a theoretical 4,500 horsepower. At the time we were told additional mounts would make the system too rigid and could lead to stress cracks. So much for who were the cowboys and who had the engineering.
In addition while the over the nose scoop may look cool, Bill Hickle told me in his opinion it was not the best design, in addition to that there is a thought line that the inlet scoops at the base of the wing tricked the airflow into thinking the wing root was thinner by processing the carburetor inlet air. I was told that someone has pictures that show this effect based on the Bear having followed another airplane around the course that was losing a good amount of oil. That part I can understand from pictures that we took after the Super Corsair oiled it down one year. We had very interesting pictures of the real life airflow around the airplane.