Specifications/ Performance
| Engine |
| Bombardier Rotax 912S |
| Cylinders |
4 |
Engine power
|
100 PS |
73,5 kW |
| Max. take off power and max. continuous
power A 210 |
95 PS |
69 kW |
| TBO |
1.500 h/ 12 years |
| Propeller |
mt-propeller 2-blade constant-speed MTV-21-A/175-05,
TBO 1.500 h/ 6 years |
| Performance and airspeeds |
| Max. speed |
165 kts |
190 mph |
| Max. level speed, MSL |
130 kts |
150 mph |
| |
|
|
| |
75%, 5,000 ft,
ISA |
55%, 5,000 ft,
ISA |
| Speed (TAS) |
121 kts |
140 mph |
103 kts |
118 mph |
| Range (+ 45 min rsv) |
535 NM |
990 km |
620 NM |
1,150 km |
| Endurance (+ 45 min rsv) |
4:30 hrs |
6:05 hrs |
| Fuel-flow |
21.5 ltr/h |
5.7 gph |
16.6 ltr/h |
4.36 gph |
| |
|
|
| Stallspeed clean VS1 |
50 ks |
58 mph |
Stallspeed in landing
configuration VS0 |
43 kts |
50 mph |
| Max. demonstrated crosswind |
15 kts |
3.8 m/s |
| Rate of climb, sea level |
750 ft/min |
3,8 m/s |
| Service ceiling |
14,500 ft |
4,450 m |
| Weights and capacities |
| Empty weight, typical |
500 kg |
1,103 lb |
| Max. takeoff weight |
750 kg |
1,654 lb |
| Useful load (at standard equipment) |
250 kg |
551 lb |
| Max. baggage weight |
40 kg |
97 lb |
| Max. wing loading |
71.5 kg/m² |
16.6 lb/sqft |
| Seats |
2 |
Fuel capacity
100LL or Eurosuper 95 |
2 x 60 ltr |
2 x 16 gal (US) |
| Takeoff and landing distances |
| Takeoff distance, ground roll |
250 m |
820 ft |
Takeoff distance over 50 ft
obstacle |
470 m |
1,540 ft |
| Landing distance, ground roll |
200 m |
650 ft |
Landing distance over 50 ft
obstacle |
500 m |
1.640 ft |
These information are also available as PDF file for download:
To view PDF files, you need to have the free Adobe
Reader installed on your computer.
|
