| Approved Type Certificate: Engineering Memorandum 641. |
| Issued May 22, 1937.: |
| Total Built: One |
| Price: $9,090 |
| Wing span: 32 feet |
| Wing Area: 296.4 ft2 |
| Wing loading: 11.3 lb./ ft2 |
| Length: 25 feet 11 inches |
| Height: 8 feet 2 inches |
| Basic empty weight: 2,080 lb. |
| Maximum gross weight: 3,350 lb. |
| Engine: Jacobs R-755D (L-4) seven-cylinder, air-cooled radial, 225 hp. |
| Propeller: Curtiss metal, fixed pitch. |
| Power loading: 14.8 lb./hp. |
| Maximum speed: 173 mph |
| Cruise speed: 166 mph. |
| Landing speed: 48 mph |
| Rate of climb: 850 ft./min. |
| Service ceiling: 15,000 ft. |
| Fuel capacity: 34 gallons standard, 64 gallons with optional tanks |
| Range: 500 statute miles |
| Technical features: Lengthened fuselage. Ailerons on upper wings. Plain flaps on lower wings. Semi-cantilever empennage. Tailwheel doors. Wing rib spacing 8 inches. |
