| Approved Type Certificate: Engineering Memorandum 602. |
| Issued April 16, 1936.: |
| Total Built: Six |
| Price: $7,450 (increased to $8,550) |
| Wing span: 32 feet |
| Wing Area: 273 ft2 |
| Wing loading: 11.5 lb./ ft2 |
| Length: 24 feet 5 inches |
| Height: 8 feet 2 inches |
| Basic empty weight: 1,850 lb. |
| Maximum gross weight: 3,150 lb. |
| Engine: Jacobs R-755D (L-4) seven-cylinder, air-cooled radial, 225 hp. |
| Propeller: Curtiss metal, fixed pitch. |
| Power loading: 14.0 lb./hp. |
| Maximum speed: 175 mph |
| Cruise speed: 162 mph. @ 5,000 feet |
| Landing speed: 45 mph. |
| Rate of climb: 850 ft./min. |
| Service ceiling: 15,500 ft. |
| Fuel capacity: 46 gallons standard, 74 gallons with optional tanks |
| Range: 560 statute miles |
| Technical features: Ailerons on lower wings. Drag flaps on undersurface of lower wings. Semi-cantilever empennage. Horizontal stabilizer angle of incidence changed to improve landing characteristics. No tailwheel doors. Wind rib spacing 8 ˝ inches. |
