| Type |
2-seat conventional low wing monoplane |
| Engine |
M-14 360 hp |
| Propeller |
2-blade metal 9,16 ft dia |
| Landing gear |
tailweel |
| Length |
31,9 ft |
| Wing Span |
49,5 ft |
| Wing Area |
334 sq.ft |
| Wing Aspect Ratio |
7,4 |
| Airfoil |
Clark-YH |
| Vertical Tail Area |
25 sq.ft |
| Rudder Area |
13,9 sq.ft |
| Horizontal Tail Area |
50,2 sq.ft |
| Elevator Area |
31 sq.ft |
| Empty Weight |
2555 lb |
| Gross Weight |
4900 lb |
| Wing Loading |
14,6 lb / sq.ft |
| Power Loading |
13,6 lb / hp |
| Fuel Capacity |
9,3 gal |
| Top Speed |
137 mph |
| Stall Speed |
40 mph |
| Takeoff Roll |
n.a. |
| Rate of Climb |
1200 fpm |
| Bldg. Materials |
Wing: metal
Tail: metal
Fuselage: metal |
|
|
