So now you are saying that it should have 950hp but you were just saying in this thread that it should have only 850hp? Which is it?
If you start dismissing clear evidence without any real Brewster-specific evidence on your part, you are just making yourself look stupid. Pyro/HTC has the whole document and has modeled the plane accordingly. If you start calling Brewster Corp. on inflation of data you have to be able to prove it.
There could be number of reasons why an engine was run on different boost settings as the time went on. Some got their recommended power settings reviewed. Also 850hp is the continuous setting and as such is mentioned in the literature and in many Internet sources. This case seems to be very clear to more or less anyone but you.
AH is full of planes that weren't supposed to run their max. military setting indefinitely either and they do it in AH. Brewster is no different in this respect. That is how HTC chose to model these planes in general. Deal with it.
This has all been gone over previously and yet you just doesn't seem to grasp it.
Anyway, this is my last word on the subject on this thread as you aren't gonna get any of it anyway and I'm sure the rest of the readers have enough data to make up their own minds.
Yet you cant explain away the 5 other planes that had the same motor that never made the HP the Awesome Finns did.
I would say it maybe had 85% of it original estimated HP....maybe
Your motors were used and came from DC3's in where... India? When did Brewster AC corp test to get these figures since that model of the engine was never put in the Brewster? They Didn't.
That's why your document says Estimated.
Edit: The Martin AC who actually tried the motors was not as generous:
http://www.marylandaviationmuseum.org/pdf/B10_spec.pdf Same with the Grummie's
Function: Carrier-borne fighter
Fuel Type: Fuel Cap.:585 Fuel Cons.: 357 (89pr hour)
Load: 100kg
Veh. Wt.:empty: 1490kg max: 2175kg
Crew:1
MNT:7
Runway Min:take-off: 550m/landing: 550m type:paved (carrier)
Powerplant:1 x Wright R-1820-22 , 708kW (850hp)
Length: 7,06m Height: 2,84m Wingspan: 9,75m
Speed: max:425kph cruise:241kph stall:120kph Tr.Mov:964 Comb.Mov:42 (12)
Ceiling: 10120m Range: 1577km
Armaments:
2 x 7.62mm MG (2 x 500 rnds)
"Though the Navy could no longer dispute the fact the biplane was a lost cause, they still clung to the hope that, at least while the monoplane was being perfected, they could have a two-winged fighter of comparable performance. Since Grumman had been able to improve upon the F2F, they were asked to perform a similar task on the new ship. On March 6, 1936, Grumman received a contract for their fourth biplane fighter design, the XF4F-1. This one was to utilize an experimental Wright XR-1670 engine. Grumman suggested that the performance sought from the new design might be achieved by installing a supercharged 850 hp Wright R- 1820-22 on the F3F."
"With the F3F-1 now in service, and being well liked by its pilots, Grumman proposed that the last aircraft of the order be delivered with a more powerful Wright R-1820-22 Cyclone producing 850 hp."