| Engines: Lycoming IO-360-A1B6 (200 HP) |
|
|
| Take-off Weight |
2084 kg |
4594 lb |
| Max. Landing Weight |
1980 kg |
4365 lb |
| Basic Empty Mass |
1420 kg |
3130 lb |
| Zero Fuel – Gross Weight |
1890 kg |
4167 lb |
| Max. Useful Load |
680 kg |
1499 lb |
| Usable Fuel |
670 lt |
177 U.S. gal |
| Seats |
6 |
|
| Baggage Compartment |
0,56 m3 |
20 ft3 |
| Maximum Baggage Weight |
181 kg |
400 lbs |
| Cruise Speed at 75% |
301 km/h |
160 Ktas |
| Climb Speed (2 engines m.p. @ MTOW) |
6 m/s |
1100 fpm |
| Climb Speed, 1 engine (MTOW, S.l) |
1 m/s |
200 fpm |
| Stall Speed, 35 kraadi tagatiivad, MTOW |
106 km/h |
57 Kcas |
| Flight Ceiling |
5490 m |
18000 ft |
| Ceiling for one engine |
1520 m |
5000 ft |
| Max.Distance FL 100, 55% Pwr (with 45′ Res) |
2960 km |
1589 nm |
| Take-off Run Ground, MTOW, ISA |
400 m |
1312 ft |
| Landing Distance, MLW |
600 m |
1969 ft |
| Endurance, FL 100, 65%, ISA |
> 10 h |
> 10 h |
