Hello I am looking for additional information on the F8F-1 using the Pratt & Whitney R-2800-34W Double Wasp 18 cyl radial piston engine.
Is there any concrete evidence that the pilots were able to use WEP in the early F8F-1 and not only the later F8F-1B model?
In these two documents the WEP is listed but I can't find anything on the usage of WEP in the handbook besides "On entering Cockpit" - "WEP switch - OFF".
But no clear instruction when and on which specific model WEP switch should and could be switched to ON?
http://www.wwiiaircraftperformance.org/F8F/F8F-1-2.pdf
http://www.wwiiaircraftperformance.org/F8F/F8F-1_Standard_Aircraft_Characteristics.pdf
Is there any concrete evidence that the pilots were able to use WEP in the early F8F-1 and not only the later F8F-1B model?
In these two documents the WEP is listed but I can't find anything on the usage of WEP in the handbook besides "On entering Cockpit" - "WEP switch - OFF".
But no clear instruction when and on which specific model WEP switch should and could be switched to ON?
http://www.wwiiaircraftperformance.org/F8F/F8F-1-2.pdf
http://www.wwiiaircraftperformance.org/F8F/F8F-1_Standard_Aircraft_Characteristics.pdf
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