Hallo(Hajimemashite)! I posted here for the first time!
I'm from Tokyo Japan(Hachiouji-City). I'm Japanese.
This is the testdata of Ki-84a(the "S17" codenamed by U.S.A.F) by
U.S T.A.I.U(Technical Air Intelligence Unit) in the spring of 1945.
And in Japan, people generally regard this result of flight-testing as it powered by 140-octane gasoline, but in my opinion, the gasoline used in this test was regular and more normal AN-F-28(100/130)gas for USAF. Empty weight of Ki-84a is 2660-2698kg. And full loaded weight is 3770-3890kg. The weight of the aircraft in this test was about 3600kg, and this could be regarded as its normal combat weight.
DATA
Max Speed: 689(or687)km/h/6100m
Cruising Speed: 410km /h/unknown
Climbing Performance: 3000m/2min48sec
6100m/5min48sec
Service Ceiling: 11800m
Range: 1650km(normal)
2920km(with two droptanks)
On the other side, another captured Ki-84a("T2-302" coded by US) went through more rigorous testing at the Middletown Air Depot in Pennsylvania in April and May of 1946. The Ki-84a proved superior in early climbing performance, maneuverability and overall handling to the both P-47N and P-51H. Max Speed was slightly inferior to those two aircraft, and the range of the Ki-84a was nearly equal to those of P-51H. But it received negative marks for numerous exhaust pipe problems during testing. According to "Japanese Aircraft of the Pacific War" by Rene J Francillon, in this flight-testing, The speed of The HAYATE at the combat weight with its war emargency power exceeded that of the P-51D-25-NA and P-47D-35-RA at the same altitude(20,000ft) by 3mph and 22mph respectively.
For your Information ---
Sorry for my bad English and thanks for reading! BYE!