Weights
| Maximum takeoff weight | 600.0 kg | 1323 lb |
| Maximum landing weight | 600.0 kg | 1323 lb |
| Maximum empty weight | 350 kg | 772 lb |
| Minimum useful load | 250 kg | 552 lb |
| Minimum load per seat | 55.0 kg | 121 lb |
| Maximum load per seat | 120.0 kg | 265 lb |
| Maximum total front baggage weight | 2 x 10.0 kg | 2 x 22 lb |
| Maximum total rear baggage weight | 2 x 20.0 kg | 2 x 44 lb |
Top Speeds at Sea Level
| IAS | KIAS | ||
| Top speeds at sea level | At 5800 rpm | 240 | 130 |
| At 5500 rpm | 230 | 124 |
Cruise Speeds at Altitudes and Power Setting
| Presurre altitude | Engine speed | MAP | Cruise speeds | |
| ft | rpm | inHg | IAS | KIAS |
| 2000 | 5500 | 24.2 | 223 | 120 |
| 4000 | 5500 | 24.4 | 216 | 117 |
| 6000 | 5500 | 22.6 | 211 | 114 |
| 8000 | 5500 | 21.4 | 201 | 109 |
| 10000 | 5500 | 19.9 | 192 | 104 |
Fuel Operating Ranges
| Endurances and ranges at altitude 2000 ft ISA | |||||||
| Engine speed | rpm | 4300 | 4500 | 4800 | 5000 | 5500 | |
| Fuel consumption | l/h | 14.5 | 15.5 | 17.2 | 18.5 | 21.3 | |
| IAS | km/h | 165 | 175 | 190 | 200 | 223 | |
| KIAS | knots | 89 | 94 | 103 | 108 | 120 | |
| CAS | km/h | 163 | 172 | 185 | 194 | 215 | |
| KCAS | knots | 88 | 93 | 100 | 105 | 116 | |
| TAS | km/h | 172 | 183 | 196 | 206 | 228 | |
| KTAS | knots | 93 | 99 | 106 | 111 | 123 | |
| Usable fuel (l) | 119 | hh:mm | 8:12 | 7:40 | 6:55 | 6:25 | 5:35 |
| km | 1411 | 1404 | 1356 | 1325 | 1273 | ||
| 100 | hh:mm | 6:53 | 6:27 | 5:48 | 5:24 | 4:41 | |
| km | 1186 | 1180 | 1139 | 1113 | 1070 | ||
| 80 | hh:mm | 5:31 | 5:9 | 4:39 | 4:19 | 3:45 | |
| km | 948 | 944 | 911 | 890 | 856 | ||
| 60 | hh:mm | 4:8 | 3:52 | 3:29 | 3:14 | 2:49 | |
| km | 711 | 708 | 683 | 668 | 642 | ||
| 40 | hh:mm | 2:45 | 2:34 | 2:19 | 2:9 | 1:52 | |
| km | 474 | 472 | 455 | 445 | 428 | ||
| 20 | hh:mm | 1:22 | 1:17 | 1:9 | 1:4 | 0:56 | |
| km | 237 | 236 | 227 | 222 | 214 | ||
Rate of Climb
| IAS | KIAS | |
| Best angle of climb airspeed VX (at SL) | 100 IAS | 54 KIAS |
| Rate of climb at VX (at SL) | 985 fpm | |
| Best rate of climb airspeed VY (at SL) | 127 IAS | 69 KIAS |
| Rate of climb at VY (at SL) | 1085 fpm | |
Stall Speeds
| IAS | KIAS | |
| Cruise, FLAPS 0 (0°) | 78 | 42 |
| Takeoff, FLAPS 1 (15°) | 68 | 37 |
| Landing – normal, FLAPS 2 (24°) | 64 | 35 |
| Landing – emergency, FLAPS 3 (35°) | 61 | 33 |
TECHNICAL SPECIFICATION
Dimensions
| Wing area | 10.500 m2 | 112.98 ft2 |
| Wing span | 8.926 m | 29.28 ft |
| Overall length | 6.460 m | 21.19 ft |
| Maximum height | 1.850 m | 6.07 ft |
| Wheel base | 1.400 m | 4.59 ft |
| Main landing gear track | 2.240 m | 7.35 ft |
| Maximum propeller diameter | 1.750 m | 68.90 in |
| Mean aerodynamic chord (MAC) | 1.172 m | 3.84 ft |
Engine
| Number of engines | 1 |
| Number of cylinders | 4 |
| Engine manufacturer | BRP-Rotax GmbH & Co KG |
| Engine model number | Rotax 912 ULS2 |
| Engine type | Horizontally opposed, geared, normally aspirated, spark ignition |
| Cooling | Combined liquid and air |
| Maximum takeoff power at 5800 rpm (max. 5 min.) | 73.5 kW / 100 hp |
| Maximum continuous power at 5500 rpm | 69.0 kW / 92.5 hp Propeller |
Propeller
| Number of propellers | 1 |
| Propeller manufacturer | PRODUCTION EVRA, Creil, France |
| Propeller model number | EVRA PerformanceLine 175/xxx/805.5 |
| Number of blades | 3 |
| Propeller diameter | 1.750 m (68.90 in) |
| Propeller type | Fixed pitch, ground adjustable |
| Pitch setting (measured 200 mm from blade tip) | 23° |
Three View Drawing
