| Approved Type Certificate: Engineering Memorandum 604. |
| Issued May 6, 1936.: |
| Total Built: 17 |
| Price: $14,500 |
| Wing span: 32 feet |
| Wing Area: 273 ft2 |
| Wing loading: 14.2 lb./ ft2 |
| Length: 24 feet 5 inches |
| Height: 8 feet 2 inches |
| Basic empty weight: 2,250 lb. |
| Maximum gross weight: 3,900-3,915 lb. |
| Engine: Wright R-975E2 nine-cylinder, air-cooled radial, 420 hp. |
| Propeller: Curtiss metal, fixed pitch. |
| Power loading: 9.2 lb./hp. |
| Maximum speed: 211 mph. |
| Cruise speed: 202 mph. @ 10,000 feet, 195 mph. @ 5,000 feet |
| Landing speed: 60 mph |
| Rate of climb: 1,400 ft./min. |
| Service ceiling: 21,500 ft. |
| Fuel capacity: 98 gallons standard, 173 gallons with optional tanks |
| Range: 800 statute miles |
| Technical features: Ailerons on lower wings. Drag flaps relocated to undersurface of upper wings. Semi-cantilever empennage. Tailwheel doors. |
