| Approved Type Certificate: Engineering Memorandum 649. |
| Issued July 16, 1937.: |
| Total Built: 68 |
| Price: $16,490 in 1937, increased to $18,870 by April 1940 |
| Wing span: 32 feet |
| Wing Area: 296.5 ft2 |
| Wing loading: 14.17 lb./ ft2 |
| Length: 26 feet 10.6 inches |
| Height: 8 feet |
| Basic empty weight: 2,540 lb. |
| Maximum gross weight: 4,200 lb. |
| Engine: Pratt & Whitney R-985 “Wasp Jr.” nine-cylinder, air-cooled radial, 450 hp. |
| Propeller: Hamilton Standard controllable pitch. |
| Power loading: 9.33 lb./hp. |
| Maximum speed: 212 mph |
| Cruise speed: 202 mph. |
| Landing speed: 50 mph |
| Rate of climb: 1,500 ft./min. |
| Service ceiling: 25,000 ft. |
| Fuel capacity: 100 gallons standard, 174 gallons with optional tanks |
| Range: 670 statute miles |
| Technical features: Lengthened fuselage. Ailerons on upper wings. Plain flaps on lower wings. Modified windshield. Tailwheel doors. Toe-operated wheel brakes. Wing tip area reinforced with additional plywood to prevent flutter. Cantilever empennage. Wing rib spacing 6.5 inches. |
