sales.html - 2007, May - 27th -
Updated: 2010, January 4th

PRICE
As it is: 80.000 Euro with 145 HP Rotorway Engine and instruments
Delivery place : Italy or Tunisia

Year of construction: 1995
Flight hours: 70
Frame : 70 h- certified -
Engine hours: 70
Engine year of construction: 1995
Max output: 145 HP
Status: ready and operational

Flag
- Italian

Classification
- Italy : ULM

Seats
2

Max. Power
145 HP

Standard Rated Horspower @ 4250 RPM
120 HP

Engine
RI 600

STROKE - FUEL TYPE
4 - Unleaded Gasoline - Use Av/Gas 100 Low lead -
Use standard premium gasoline with octane-booster, like MOROSO. If MOROSO is used, add 1/4 gallon
of octane-booster to 20 gallons of gasoline.
MOROSO and 2 or 3 other types of octane-boosters are available at most auto stores and seepd shops.
With all high octane gasoline and gasolines with octane-boosetr, carbon build up on spark plug electrodes should be carefully monitored.

Max Torque @ 3950 RPM
191 ft.lb

Operational RPM ( Calibrate with rotor RPM )
4500

Idle RPM
1600-1800

Bore, inches
4.00

Stroke, inches
3.228

Displacement, cubic inches
162

Compression Ratio
9.6: 1

Flywheel Rotation ( viewed from above )
Clockwise

Engine Dry Weight Lbs
170 lb ( 77 Kg ) including upper bearing mount, drive pulley flywheel, water manifolds, carburetors, throttle lingage, magneto, ignition harness, spark plugs and starter

Standard Fuel Capacity
64,3 lt - 17 U.S. Gallon

Fuel Flow at Max Cruise
51 Lbs/h - 23,13 Kg/h

Fuel Flow at Max Range Cruise
48 Lbs/h - 21,77 Kg/h

Recommended Fuel
"premium gasoline" - Av/Gas 100 low lead.

Service Ceiling
3000 m - 10,000 feet

Rate of Climb
304 m/min - 1,000 fpm

Main Rotor Blades
2 Blades - 7,62 m Diam - 25'

Main Rotor RPM
520

Tail Rotor Blades
2 Blades - 122 cm Diam ( 48" )

Tail Rotor RPM
2600

Cabin Width
1,10 m

Normal Cruise Speed
95 mph - 152 Km/h

MAX. Cruise Speed
110 mph - 177 Km/h

Max Airspeed at sea Level, Standard Dy ( VNE )
120 mph - 193 Km/h

Max. Air Speed in Turbolent Air
75 mph - 65 Knots - 120 Km/h

Max. Sideways, Rearwards Airspeed
20 mph - 17 Knots - 32 Km/h

Endurance min./Max. Hours
2 hrs

Range min. Max. Km
180 Miles - ( 2 H ) 289 Km / 234 ml ( 376 Km ) @ 2.2 hrs

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Empty Weight
385 Kg - 850 lbs

Equipped Useful Load MTOW
215 Kg - 475 lbs

Gross Weight - MTOWA - Max Weight
598 Kg - 1320 lbs

Pilot and Passenger Load
181 Kg - 400 lbs

Maximum Cabin Weight
204 Kg - 450 lbs

Minimum Pilot Weight ( solo operations )
68 Kg - 150 lbs

HIGE - Hover in Ground Effect -
2133 m - 7000 ft - ( Gross Weight )

HOGE - Hover out Ground Effect-
1371 m - 4500 ft

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Lenght Nose to Tail
6,7 m - 22'

Height Total
2,6 m - 103"

Rate of Climb
- 300 m/min - 1000 fpm

Length - OVERALL
9 m - 30' approx

Skid Distance
1,65 m - 65" approx

Status
Operative

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