TECHNICAL SPECIFICATION

ITEM VALUE
Engine:Rotax 912 ULS2 / S2
Power:73.5 kW, 100 HP at 5800 RPM
Fuel:Mogas RON 95, Avgas 100 LL, EN 228
Propeller:Woodcomp Klassic 170/3/R
Sensenich Fixed 3-blade (*)
Wingspan:8.6 m (28.22 ft)
Length:6.62 m (21.72 ft)
Height:2.315 m (7.60 ft)
Wing surface area:12.3 m² (132.4 sq ft)
Cockpit width:1.17 m (3.85 ft)
MTOW:600 kg (1,320 lbs)
Empty weight (Classic with standard configuration):388 kg (855.4 lbs)
Max. baggage weight in cockpit compartment:18 kg (40 lbs)
Max. baggage weight in each wing locker:10 kg (22 lbs)
Cruise speed at 75% power:105 KIAS (195 km/h)
Max. horizontal speed:119 KIAS (220 km/h)
VNE :138 KIAS (255 km/h)
Stall speed VS0:31 KIAS (55 km/h)
Climb rate:825 ft/min (4.2 m/s)
Take-off distance to 50 ft (15 m):
Concrete:1,270 ft (387 m)
Grass:1,499 ft (457 m)
Braking distance:
Concrete:479 ft (146 m)
Grass:364 ft (111 m)
Range (30 min. reserve): 516 NM (953 km)516 NM (953 km)
Endurance:5 hours 25 min
Fuel capacity:114 l (30 US gal.)
Average fuel consumption:17.5 l/h (4.6 US gal./1 hour)