spec-price-01.html - 2007, July 8th -
updated: 2008, 13rd of June

Dimensions
Cabin Total Length : 6.360 mm
Cabin Internal Height: 1.200 mm
Rotors Diameter: 7.900 mm / 8.000 mm
Main Rotor Chord Length : 203 mm

Weights and Capacities
Gross Weight: 2.000 Kg ( 4409 Lbs )
Empty Weight: 1.000 Kg ( 2202 Lbs )
Payload: 1.000 Kg ( 2202 Lbs )
Fuel Capacity: 300 l ( 79,25 US Gallons ) Standard - unleaded gasoline -
Oil Capacity: 40 l ( 10,4 US Gallons ) Standard
Radiator capacity: 50 l - ( 13.3 US Gallons ) Standard

Performances
Maximum Speed: 100 MPH - 87 Kts - 160 Km/h
Cruise Speed : 85 MPH - 74 Kts - 153 Km/h
Maximum Range: 250 + Miles ( 400 Km ) Standard configuration
Consumption @ 75% power - 5.000 rpm : 70 - 80 l/h ( 18,49 - 21,13 US Gallons/h)- unleaded gasoline -
Maximum Rate of Climb : 1,000 FPM - 300 m/min.
Service Ceiling: 10,000 ft - 3,000 m
Hover IGA: 7,000 Feet - 2,100 m

Engine
Power: n° 2 x 220 HP each - Max : 2 x 300 Hp each
Single engine Standard output : 200 HP @ 5.000 r.p.m.
Fuel:- unleaded gasoline -
Cycle: Four - Double Turbo - Double injection
Coolong: Water + oil
Max Torque: 220 Nm@5000 r.p.m.

Structure
4130 Chromo alloy steel aircraft tubing airframe
Aluminium sheet metal cabin for long life @ durability
Oil bath geared transmission housings
Maintinance free auto-engagement clutch assembly
Corrosion protection from salt air environments
Titanium used in both rotor heads and transmission shafts

Controls and Avionics
Dual controls
Cabin heat and air conditioning system
Sand proof cabin
Garmin updated avionics
Engine controls
Transponder