| Approved Type Certificate: Engineering Memorandum 548. |
| Issued August 8, 1934.: |
| Total Built: One (constructor number 5, NC12583) |
| Price: $25,000 |
| Wing span: 34 feet 6 inches |
| Wing Area: 292.44 ft2 |
| Wing loading: 14.6 lb./ ft2 |
| Length: 24 feet 3 inches |
| Height: 8 feet 10 inches |
| Basic empty weight: 3,285 lb. (useful load: 1,915 lb.) |
| Maximum gross weight: 5,200 lb. |
| Engine: Wright R-1820F11 "Cyclone" nine-cylinder, air-cooled radial, 690 hp. |
| Propeller: Hamilton Standard, controllable pitch |
| Power loading: 7.73 lb./hp. |
| Maximum speed: 215 mph |
| Cruise speed: 205 mph |
| Landing speed: 70 mph |
| Rate of climb: 1,500 ft./min. |
| Service ceiling: 25,000 ft. |
| Fuel capacity: 155 gallons |
| Range: 820 statute miles |
| Technical features: Ailerons on lower wings. Narrow-chord drag flaps on undersurface of upper wings. Landing gear track increased 18 inches. Full-swiveling tailwheel. Semi-cantilever empennage. Rudder and elevator trim tabs replaced empennage trim system. |