The single XSO2U-1 was built in 1939 and many of the features of the OS2U-1 were used, while it was powered by a 550 hp Ranger XV-770-4 twelve-cylinder air-cooled inverted V-engine as specified by the Navy. Duly flown in competition to the Curtiss Model 82 XSO3C-1, the Curtiss design was declared winner and was ordered into production as the SO3C-1."
Span: 38 ft 2 in (11.63 m)
Length: 34 ft 2 in (10.41 m)
Height: 15 ft 1 in (4.60 m)
Gross weight: 5,186 lb (2,352 kg)
Max speed: 201 mph (323 kmh)
Service ceiling: 22,200 ft (6,767 m)