| Approved Type Certificate: Engineering Memorandum 560. |
| Issued December 4, 1934.: |
| Total Built: One (constructor number 20, NC14408) |
| Price: $9,000 |
| Wing span: 32 feet |
| Wing Area: 273 ft2 |
| Wing loading: 11.5 lb./ ft2 |
| Length: 24 feet 6 inches |
| Height: 8 feet 6 inches |
| Basic empty weight: 1,850 lb. |
| Maximum gross weight: 3,150 lb. |
| Engine: Jacobs R-830-1 (L-5) seven-cylinder, air-cooled radial, 285 hp. |
| Propeller: Curtiss metal, fixed pitch. |
| Power loading: 11.0 lb./hp. |
| Maximum speed: 185 mph |
| Cruise speed: 173 mph |
| Landing speed: 45 mph |
| Rate of climb: 1,100 ft./min. |
| Service ceiling: 18,000 ft. |
| Fuel capacity: 50 gallons standard, 120 gallons with optional tanks |
| Range: 500 statute miles |
| Technical features: Long-length main landing gear shock struts. Ailerons on lower wings. Drag flaps on undersurface of lower wings. Semi-cantilever empennage. No tailwheel doors. Wind rib spacing 7 ˝ inches. |
