| WEIGHTS | |
|---|---|
| Max. take-off weight (utility) | 1490 kg |
| Max. take-off weight (aerobatic) | 1440 kg |
| Max. zero fuel weight (utility) | 1345 kg |
| Max. zero fuel weight (aerobatic) | 1315 kg |
| Max. landing weight | 1440 kg |
| Max. usable fuel capacity | 182 kg / 252 Ltr |
| Max. crew / boarding weight | 220 kg |
| Max. baggage weight | 50 kg |
| POWER PLANT | |
|---|---|
| Engine Textron Lycoming AEIO-540-D4D5 |
260 SHP / 2700 rpm |
| Propeller Hartzell 3-blade | 1,98 m |
| MISCELLANEOUS | |
|---|---|
| Max. load factors aerobatic | +6 / -4G |
| Max. operating altitude | 18.000 ft |
| Operation: VFR day/night, IFR, non-icing conditions |
| PERFORMANCE | |
|---|---|
| Operating speed range | |
| Max. structural cruising speed VNO | 172 kias |
| Never exceed speed VNE up to 13,100 ft | 235 kias |
| Stall speed VS (MLW, flaps full, utility) | 56 kias |
| Take off and landing field length (MSL, ISA, utility) | |
| Take off distance over 50 ft (MTOW, no wind, no slope) | 707 m |
| Landing distance over 50 ft (MLW, no wind, no slope) | 562 m |
| Cruise speeds, rate of climbs (ISA, MTOW) | |
| Max. cruise speed (MSL) | 172 ktas |
| Max. cruise speed at 75% power (5,000 ft) | 166 ktas |
| Rate of climb (MSL, aerobatic) | 1280 ft/min |
| Range / Endurance (ISA, MTOW, 45 min reserve fuel, maximum fuel, utility) | |
| Range (5,000 ft, 75% power) | 635 NM |
| Range (10,000 ft, 45% power) | 730 NM |
| Endurance (10,000 ft, max. endurance power) | 6.35 Hrs |