I don't gnats ass the on-speed A/S calculation. I know what the airspeed should be at max trap. Other than that, I just sanity check it. I know that I should be looking at 8* NU with 0* FPA on-speed on downwind (0 VSI), and I use that as my primary sanity check.
What cool-aid man is alluding to is that in the Hornet the AOA is measured in actual degrees using the aircraft waterline, rather than some artificially-derived "units" like in most other aircraft. I think on-speed in the T-45 was something like 19 or 20 "units," correct? I also remember hearing rumors that the onspeed for the goshawk was intentionally made a little faster to add in a safety margin to prevent stalls.