The H-1B Racer carried 250 USgal internally, while after modification for the cross-country record attempt it carried 280 USgal. Yes it might have had a reduction in storage if self-sealing tanks were fitted, but assuming it was no more than usual, the H-1 wold still have had more internal fuel than any(?) single-engine USAAC/AAF pursuit plane up until the P-47.
The H-1B Racer was stressed for a 9G pullout from a dive, so this would yield about the same ultimate 12G as the normal pursuit aircraft of the time. I do not have any numbers on the modified cross-country aircraft with the larger wings and additional fuel tankage.
The H-1B was primarily made of wood. The XP-2 airframe (based on the H-1) that Hughes put forward for the 1935 Army Specification X-603 was of all-metal construction, with a larger elliptical wing of greater span, 4x MG (2x in each wing), and all the normal pursuit aircraft equipment. Again, the XP-2 variant was stressed for the normal pursuit airframe G-loads of the time.
This is the abbreviated Detailed Specification for the Hughes XP-2 aircraft as offered to the USAAC:
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Early F4U was notorious for bad pilot's vision over the nose. That's why the cockpit was raised and even the tail wheel strut extended.
True, but the original 1940 F4U prototype had the cockpit much farther forward, and it was moved back to the position of the production version in order to allow a larger fuselage fuel tank on the CoG - despite the reduced visibility. Also, I am only advocating for possible use by the USAAC as a land-based pursuit fighter, where in theory the long nose would not be as much of a problem as on carriers.