P-75 Eagle

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Fisher XP-75 43-46950 in flight

First XP-75 43-46950 in flight

P-75A 44-44549

Fisher P-75A Eagle 44-44549 September 1944

Fisher XP-75A Eagle 44-32166

Fisher XP-75A Eagle 44-32166

Fisher XP-75A Eagle 44-32166

Fisher XP-75A Eagle serial 44-32166

Fisher XP-75A Eagle serial 44-32166 2

Fisher XP-75A Eagle serial 44-32166 2

XP-75A-1 44-44550

Fisher XP-75A-1 44-44550

Fisher P-75A Eagle 44-44553

P-75A Eagle 44-44553

Fisher XP-75A Eagle 44-32166

XP-75 44-32166

XP-75 Eagle 43-46950 1944

XP-75 Eagle 43-46950 1944

First XP-75 Eagle assembly 1943

XP-75 Eagle assembly 1943

XP-75A

XP-75A

P-75 Eagle was a fighter aircraft for which the Fisher Body Division of General Motors Corporation in September 1942 submitted a proposal to meet a United States Army Air Forces requirement for a fighter possessing an extremely high rate of climb. The proposal was for an aircraft that used the most powerful liquid-cooled engine then available, the Allison V-3420, and components from existing aircraft (SBD, P-51, F4U and P-40). Total production: 14