| Approved Type Certificate: Engineering Memorandum 579. |
| Issued July 22, 1935.: |
| Total Built: 15 |
| Price: $14,500 |
| Wing span: 32 feet |
| Wing Area: 267 ft2 |
| Wing loading: 13.4 lb./ ft2 |
| Length: 24 feet 5 inches |
| Height: 8 feet 2 inches |
| Basic empty weight: 2,238 lb. |
| Maximum gross weight: 3,600-3,615 lb. |
| Engine: Wright R-975E2 nine-cylinder, air-cooled radial, 420 hp. |
| Propeller: Curtiss metal, ground-adjustable pitch. |
| Power loading: 8.5 lb./hp. |
| Maximum speed: 210 mph. |
| Cruise speed: 202 mph. @ 9,000 feet, 195 mph. @ 5,000 feet |
| Landing speed: 55 mph |
| Rate of climb: 1,600 ft./min. |
| Service ceiling: 22,000 ft. |
| Fuel capacity: 93 gallons standard, 170 gallons with optional tanks |
| Range: 760 statute miles |
| Technical features: Ailerons on lower wings. Drag flaps on undersurface of upper wings. Installation of Hamilton Standard controllable-pitch propeller required 25 lb. of ballast in the tail fairing to maintain proper weight and balance. No tailwheel doors. |
