| Approved Type Certificate: Engineering Memorandum 689. |
| Issued August 26, 1938.: |
| Total Built: 60 |
| Price: $13,980 |
| Wing span: 32 feet |
| Wing Area: 296.5 ft2 |
| Wing loading: 11.97 lb./ ft2 |
| Length: 25 feet 11 ˝ inches |
| Height: 8 feet |
| Basic empty weight: 2,155 lb. |
| Maximum gross weight: 3,550-3,590 lb. |
| Engine: Jacobs R-915A3 (L-6) seven-cylinder, air-cooled radial, 330 hp. |
| Propeller: Hamilton Standard, controllable pitch. |
| Power loading: 10.75 lb./hp. |
| Maximum speed: 195 mph |
| Cruise speed: 182 mph. |
| Landing speed: 46 mph |
| Rate of climb: 1,300 ft./min. |
| Service ceiling: 18,000 ft. |
| Fuel capacity: 76 gallons standard, 125 gallons with optional tanks |
| Range: 600 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. |