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English |
Metric |
| Dimensions |
| Length |
26 ft |
7.92 m |
| Height |
8 ft 11 in |
2.71 m |
| Wingspan |
38 ft 4 in |
11.68 m |
| Cabin Length |
130 in |
330 cm |
| Cabin Width |
49 in |
124 cm |
| Cabin Height |
50 in |
127 cm |
| Design Weights and Loading* |
| Maximum Gross Weight |
3050 lbs |
1386 kg |
| Standard Empty Weight |
2080 lbs |
945 kg |
| Useful Load |
970 lbs |
441 kg |
| Usable Fuel Capacity |
56 gal/336 lbs |
212 litre/153 kg |
| Full Fuel Payload |
634 lbs |
288 kg |
| Performance** |
| Takeoff |
1478 ft |
450 m |
| Takeoff Over 50 ft Object |
2221 ft |
677 m |
| Climb Rate |
828 ft/min |
252 m/min |
| Stall Speed with Flaps |
56 KCAS |
56 KCAS |
| Cruise Speed (75% Power) |
155 KTAS |
155 KTAS |
| Cruise Range with Reserve |
627 nm |
1161 km |
| Maximum Range with Reserve (55% pwr) |
785 nm |
1454 km |
| Landing Ground Roll |
853 ft |
260 m |
| Landing Over 50 ft Object |
2636 ft |
803 m |
| Engine |
| Manufacturer |
Continental |
| Model |
IO-360-ES |
| Horsepower |
200 |
*Takeoff/climb performance @ 3050 lb gross wt, sea level, ISA
| * |
Weights and loading calculated on base configuration. Actual Useful Loads and individual aircraft weights will vary depending on options installed on aircraft. Always consult specific aircraft weight and balance data for flight planning.
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