Equipped empty weight: 420 kg (925 lb)
Maximum gross weight: 700 kg (1542 lb)
Maximum level speed @ 100% (s.l. ISA): 100 kt (185 km/h)
Cruise speed @ 85%: 90 kt (166 km/h)
Vne (s.l.): 130 kt (240 km/h)
IGE hovering ceiling (@ 700 kg): 5000 ft
Hovering ceiling (2×77 kg + fuel 2 hrs): 7500 ft
Range @ 85 % (15 min reserve): 380 NM (700 km)
Maximum endurance @ 50 kt (no reserve): 5 hr 40
Noise level @ 100% (certified): 75.7 dB SEL

Type: Articulated, soft-in-plane
Number of blades: 3
Diameter: 7.2 m (23.6 ft)
Blade width: 180 mm (7.1 in)
Speed: 530 RPM

Type: Fenestron®
Number of blades: 7
Diameter: 0.6 m (23.6 in)
Blade width: 42 mm (1.6 in)
Speed: 5148 RPM

Primary transmission: Belt with a reduction ratio of 0.855/1
Main gearbox: Bevel spiral gear with a reduction ratio of 11/47
Tail gearbox: Bevel spiral gear with a multiplication ratio of 25/11

Engine model: Textron Lycoming O360-J2A with STC EASA E.S.01001
Type: Horizontally-opposed, four-cylinder, air-cooled, carburetted,
double-ignition with one magneto and one electronic ignition.
Displacement: 361 cu.in (5.9 litres)
Max continuous power: 145 shp @ 2585 – 2700 tr/min (108 kW)
Nominal speed: 2650 RPM
Cooling: Direct-drive squirrel-cage blower

Magneto: Bendix
Electronic ignition: LSE Plasma II – HG,
condenser discharge, variable spark advance

Max capacity: 170 litres (45 US Gal)
Unusable quantity: 1.5 litres (0.4 US Gal)
Approved fuel type: Avgas 100 LL

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