| Approved Type Certificate: Engineering Memorandum 602. |
| Issued April 16, 1936.: |
| Total Built: 39 |
| Price: $9,250 |
| Wing span: 32 feet |
| Wing Area: 273 ft2 |
| Wing loading: 11.7 lb./ ft2 |
| Length: 24 feet 5 inches |
| Height: 8 feet 2 inches |
| Basic empty weight: 1,850 lb. |
| Maximum gross weight: 3,150-3.165 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: 177 mph. @ 7,200 feet |
| Landing speed: 45 mph |
| Rate of climb: 1,100 ft./min. |
| Service ceiling: 18,000 ft. |
| Fuel capacity: 74 gallons standard, 166 gallons with optional tanks |
| Range: 680 statute miles |
| Technical features: Ailerons on lower wings. Drag flaps relocated to undersurface of lower wings. Horizontal stabilizer angle of incidence changed to improve landing characteristics. No tailwheel doors. Wind rib spacing 6 ˝ inches. |
