General characteristics
Crew: 1
Length: 22 ft 6 in (6.86 m)
Wingspan: 37 ft 6 in (11.43 m)
Height: 10 ft 11 in (3.33 m)
Wing area: 252 ft² (23.42 m²)
Empty weight: 1,980 lb (900 kg)
Max. takeoff weight: 3,171 lb (1,441 kg)
Powerplant: 1 × Pratt & Whitney R-1340 Wasp 9-cylinder air-cooled radial engine, 410 hp (306 kW)
Performance
Maximum speed: 155 mph (134 knots, 250 km/h) at sea level
Range: 360 mi (313 nmi, 580 km)
Service ceiling: 22,900 ft (6,980 m)
Climb to 5,000 ft (1,520 m): 2.5 min
Armament
Guns: 2 × fixed .30 in (7.62 mm) Browning machine guns in the forward fuselage
EDIT: the spec provided above are for the F6C-4 below are the specs for the P-1C which may be closer to the F6C-3
General characteristics
Crew: one, pilot
Length: 23.0 ft (7.01 m)
Wingspan: 31.5 ft (9.6 m)
Height: 8.75 ft (2.67 m)
Wing area: 252 ft² (23.41 m²)
Airfoil: Clark Y
Empty weight: 2,195 lb (996 kg)
Max. takeoff weight: 2,937 lb (1,349 kg)
Powerplant: 1 × Curtiss V-1150-3 liquid-cooled V12 engine, 435 hp (324 kW)
Performance
Maximum speed: 155 mph (249 km/h)
Cruise speed: 123 mph (198 km/h)
Range: 300 mi (483 km)
Service ceiling: 20,800 ft (6,340 m)
Rate of climb: 1,460 ft/min (7.42 m/s)
Armament
2 × .30 in (7.62 mm) fixed forward-firing Browning machine guns
note this blue print is of the Curtiss P-1 which is a close cousin of the F6C(could not find plans for the F6C-3)