It seems that even in late Aug 1940 the two-stage PW engine was having development issues.
The lighter aircraft has no armour or SS tanks: It's not really comparable to a BoB Hurricane but would have been similar to the aircraft that Brown mentions.. This test is for two F4F-4 aircraft at ~7370lb:
http://www.wwiiaircraftperformance.org/f4f/f4f-4-5262.pdf
results:
Gross weight (lbs)7369 / 7370
Airplane critical altitude (ft) 21100 / 19400
Vmax at critical altitude (mph) 318 / 319
so ~330mph seems a bit anomalous when several similar weight F4F-4s were tested (and spec was 318) to ~319mph.
This one at 7975lb managed only 316mph:
http://www.wwiiaircraftperformance.org/f4f/f4f-4-02135.pdf
which met the revised spec for that weight. The F4F-4 specifications were revised downward when production aircraft could not meet the Aug 1941 specifications,.
Climb rate was measured using full throttle with the resulting high fuel consumption at high throttle yet climb was considerably worse than a BoB Hurricane 1 using normal climb power. With SS tanks the F4F-3/4 carried 120IG (F4F-3 at ~7550lb = full ammo and 120IG) versus 97 for a Hurricane 1 but it would burn more fuel during climb and combat while it's more economical low speed cruise would be less of an advantage during the BoB.