| Approved Type Certificate: Engineering Memorandum 779. |
| Issued October 11, 1946.: |
| Total Built: 20 |
| Price: $29,000 (with overhauled engine) |
| Wing span: 32 feet |
| Wing Area: 296.4 ft2 |
| Wing loading: 14.34 lb./ ft2 |
| Length: 26 feet 9 inches |
| Height: 8 feet |
| Basic empty weight: 2,800 lb. |
| Maximum gross weight: 4,250 lb. |
| Engine: Pratt & Whitney R-985 “Wasp Jr.” nine-cylinder, air-cooled radial, 450 hp. |
| Propeller: Hamilton Standard constant-speed |
| Power loading: 9.44 lb./hp. |
| Maximum speed: 212 mph. @ 5,500 feet |
| Cruise speed: 201 mph. @ 10,000 feet |
| Landing speed: 64 mph |
| Rate of climb: 1,250 ft./min. |
| Service ceiling: 20,000 ft. |
| Fuel capacity: 124 gallons standard, 170 gallons with optional tanks |
| Range: 1,000 statute miles @ 10,000 feet |
| Technical features: Lengthened fuselage. Ailerons on upper wings. Plain flaps on lower wings. Tailwheel doors. Toe-operated wheel brakes. New cowling, windshield, engine installation, main gear doors. Vertical stabilizer and rudder area increased slightly. Wing tip area reinforced with additional plywood to prevent flutter. Cantilever empennage. Wing rib spacing 6.0 inches. |
