ENGINE
| BRP-Rotax 915 iSc C24 | ||
| Cylinders | 4 | |
| Max. Take-Off Power / Rated power | 141 HP | 104 kW |
| Max. Continuous Power | 135 HP | 99 kW |
| TBO | 1.200 h | 15 years |
PROPELLER
| MT-Propeller 3-blade constant-speed-propeller MTV-6-A-190-69, TBO 2.000 h/ 6 years |
PERFORMANCE
| Max. speed | 185 kts | 213 mph | ||
| Max. level speed, MSL | 141 kts | 163 mph | ||
| Max. level speed, FL100 | 154 kts | 177 mph | ||
| Stallspeed in landing configuration VS0 | 45 kts | 52 mph | ||
| Rate of climb, MTOW in sea level | >700 ft/min | >3.5 m/s | ||
| Service ceiling | 18,000 ft | 5,486 m |
WEIGHTS & CAPACITIES
| Empty weight, typical | from 700 kg | from 1,543 lb |
| Max. take-off weight | 1100 kg | 2,425 lb |
| Useful load (at standard equipment) | 400 kg | 882 lb |
| Max. baggage weight | 60 kg | 132 lb |
| Max. wing loading | 86.6 kg/m² | 17.7 lb/sqft |
| Seats | 4 | |
| Fuel capacity 100LL or Eurosuper 95 | 180 ltr | 47.6 gal (US) |
