| Approved Type Certificate: Engineering Memorandum 566. |
| Issued May 9, 1935.: |
| Total Built: Four |
| Price: $12,980 |
| Wing span: 32 feet |
| Wing Area: 267 ft2 |
| Wing loading: 12.2 lb./ ft2 |
| Length: 24 feet 5 inches |
| Height: 8 feet 2 inches |
| Basic empty weight: 2,000 lb. |
| Maximum gross weight: 3,263-3,615 lb. |
| Engine: Wright R-760E1 seven-cylinder, air-cooled radial, 285 hp. |
| Propeller: Curtiss metal, fixed pitch. |
| Power loading: 11.4 lb./hp. |
| Maximum speed: 185 mph |
| Cruise speed: 173-177 mph |
| Landing speed: 50 mph |
| Rate of climb: 1,200 ft./min. |
| Service ceiling: 18,000 ft. |
| Fuel capacity: 70 gallons standard |
| Range: 680 statute miles |
| Technical features: Ailerons on lower wings. Drag flaps relocated to undersurface of upper wings. Main landing gear shock struts shortened four inches. No tailwheel doors. |
