Different animal Crom. The Blackbird had fuel cells that were specifically engineered to be under "sealing" tolerance at static operating (fueling) temperatures. When operating at Mach 3.4 to 3.6 (yes not 3.2 as common quoted, I meant to say that), areas of the fuselage would often encounter up to 900F temps and internally the fuel cells would expand and seal.
They also used a proprietary low flash point fuel.
But back to the Spad... I have read that they often went through 32gals of oil in a single mission. I suspect that was a tradeoff of huge horsepower vs minimizing maintenance. The tolerances necessary to prevent oil loss on such a powerful radial engine would likely result in VERY short MTBO figures.