AVIO INTERNATIONAL GROUP HOLDING S.A.


Specifications:
Main rotor [Diameter]: 6.70 m
Disc Loading – GW: 13.15 kg/m²
Tail rotor [Diameter]: 1.12 m
Cabin width: 1.30 m
Total length: 6.00 m
Height [cabin roof above ground]: 1.72 m
Height [main rotor above ground]: 2.36 m
Main rotor [100%]: 520 RPM
Fuel tank capacity: 60 liters
Gross weight: 450 Kg
Empty weight: 260 Kg
Useful loading: 190 Kg
Cruise speed @ SL [power 70%]: 78 Kts – 145 Km/h
Max speed @ SL [Vne]: 96 Kts – 177 Km/h
Climbing rate: 6.50 m/s
Hover Ceiling IGE: 3.800 m
Hover Ceiling OGE: 2.250 m
Endurance @ Cruise Speed: 3.5 h
Fuel consumption [power 70%]: ~ 16 liter/h
Max. Range [20’ reserve]: 450 Km
Height speed IAS – 50 ft: 28 Kts – 51,5 Km/h
Auto rotation IAS/min. ROD: 27 Kts – 50 Km/h
Engine
RAP 98-90 I FOUR: 4 cyl., 4 strokes, 2.715 cc
Cylinder bore: 98 mm.
Stroke: 90 mm.
Compression ratio: 11 : 1
Max single engine power: 120 HP @ 3.250 RPM
Cooling system (patented): mixed air/oil
Starter: electric
Fuel: unleaded 95 octane
Ultra Light Rotorcraft
(weight at takeoff under 290kg)
Two side by side seats, dual controls
Piston engine