| Approved Type Certificate: Engineering Memorandum 615. |
| Issued August 13, 1936.: |
| Total Built: Two (Twenty in Japan under license) |
| Price: Approximately $9,300 |
| Wing span: 32 feet |
| Wing Area: 273 ft2 |
| Wing loading: 13.1 lb./ ft2 |
| Length: 24 feet 5 inches |
| Height: 8 feet 2 inches |
| Basic empty weight: 2,050 lb. |
| Maximum gross weight: 3,600-3,615 lb. |
| Engine: Wright R-760E1 seven-cylinder, air-cooled radial, 285 hp. |
| Propeller: Curtiss metal, fixed pitch. |
| Power loading: 12.6 lb./hp. |
| Maximum speed: 185 mph |
| Cruise speed: 173 mph. @ 5,000 feet |
| Landing speed: 48 mph |
| Rate of climb: 1,200 ft./min. |
| Service ceiling: 18,500 ft. |
| Fuel capacity: 98 gallons standard, 121 gallons with optional tanks |
| Range: 865 statute miles |
| Technical features: Ailerons on lower wings. Drag flaps on undersurface of upper wings. Semi-cantilever empennage. No tailwheel doors. |