| Approved Type Certificate: Engineering Memorandum 713. |
| Issued November 7, 1939.: |
| Total Built: Eight |
| Price: $14,750 in 1937, increased to $16,350 by April 1940 |
| Wing span: 32 feet |
| Wing Area: 296.5 ft2 |
| Wing loading: 14.17 lb./ ft2 |
| Length: 26 feet 7.8 inches |
| Height: 8 feet |
| Basic empty weight: 2,570 lb. |
| Maximum gross weight: 4,200 lb. |
| Engine: Wright R-760E2 nine-cylinder, air-cooled radial, 350 hp. |
| Propeller: Hamilton Standard controllable pitch. |
| Power loading: 13.1 lb./hp. |
| Maximum speed: 180 mph |
| Cruise speed: 170 mph. |
| Landing speed: 50 mph |
| Rate of climb: 1,100 ft./min. |
| Service ceiling: 15,500 ft. |
| Fuel capacity: 98 gallons standard, 170 gallons with optional tanks |
| Range: 820 statute miles |
| Technical features: Lengthened fuselage. Wing tip area reinforced with additional plywood to prevent flutter. Ailerons on upper wings. Plain flaps on lower wings. Cantilever empennage. Tailwheel doors. Wing rib spacing 6.5 inches. |
