| DIMENSIONS | |||||
| Wing Span | 41'-2" | ||||
| Overall Length | 28'-8.5" | ||||
| Height at Cabin | 6'-9" | ||||
| Height at Rudder | 10'-10" | ||||
| Cabin Width | 4'-5" | ||||
| Cabin Height Inside | 4'-5" | ||||
| WEIGHTS | |||||
| Empty Weight | 3,000 | lbs | |||
| Fuel (110 gal) | 660 | lbs | |||
| Oil (6 gal) | 22 | lbs | |||
| 5 Passengers at 170 lbs | 850 | lbs | |||
| Baggage | 250 | lbs | |||
| Instruments and Radio | 143 | lbs | |||
| Gross Weight | 4,925 | lbs | |||
| Extended Weight | 5,400 | lbs | |||
| PERFORMANCE | |||||
| Maximum Speed | 200 | mph | |||
| Cruising Speed | 180 | mph | |||
| Landing Speed | 15 | mph | |||
| Rate of Climb | 2,500 | ft per min | |||
| Service Seiling | 20,000 | feet | |||
| Range | 1,150 | miles | |||
| Take-off Distance | 200 or fewer | feet | |||
| ENGINES | |||||
| 2 Continental IO-470D Engines; 260 hp at 2625 rpm | |||||
| STANDARD EQUIPMENT | |||||
| 2 Controllable Pitch Propellers | |||||
| OTHER | |||||
| Airfoil Size | 4412 | ||||
| Fuel tanks located back center of wing spahr | |||||
Home