ghibli160-01.html - 2009
Updated: 2010, 1st of January

The Desert Kit is composed by:
AIR EXTRA FILTERS - EXTRA RADIATOR - COCKPIT COVER -
Internal Fan - SPECIAL DOORS - MAIN ROTOR CANOPY
- AIR INTAKE COVER - CABIN CANOPY -
Classification
- Light Sport Aircraft - LSA - with a MTOW of 700 Kg. - Italy : ULM
Seats
Max. Power
Standard Rated Horspower @ 4250 RPM
Engine
STROKE - FUEL TYPE
Max Torque @ 3950 RPM
Operational RPM ( Calibrate with rotor RPM )
Idle RPM
Bore, inches
Stroke, inches
Displacement, cubic inches
Compression Ratio
Flywheel Rotation ( viewed from above )
Controls
Standard Fuel Capacity
Fuel Flow
Recommended Fuel
Service Ceiling
Main Rotor Blades
Main Rotor RPM
Tail Rotor Blades
Tail Rotor RPM
Cabin Width
Max Airspeed at sea Level, Standard Dy ( VNE )
Max. Air Speed in Turbolent Air
Max. Sideways, Rearwards Airspeed
Endurance min./Max. Hours
Range min. Max. Km
Equipped Useful Load MTOW
Gross Weight - MTOWA - Max Weight
Maximum Cabin Weight
Minimum Pilot Weight ( solo operations )
HIGE
HOGE
Height Total
Rate of Climb
Length - OVERALL
Status
2
167 HP
147 HP
RI 600 S Turbo
4 - Unleaded Gasoline
191 ft.lb
4250
1750-2000
4.00
3.228
162
9 : 4.1 HP
Clockwise
FADEC ( Fully Automotad Digital Electronic Control ) ACIS ( Altitude Compensation Induction System )
64 l 17 U.S. Gallon
8 gph Gallon
92 Octane or 100 low lead AV gas ( 100 LL)
3000 m - 10,000 feet
2 Blades - 7,60 m Diam - 25'
520
2 Blades - 120 cm Diam ( 50" 1/4" )
2600
1,10 m
Cruise Speed
160 Km/h - 100 mph - 87 knots
120 mph - 193 Km/h
75 mph - 65 Knots - 120 Km/h
20 mph - 17 Knots - 32 Km/h
2H 30'
190 Miles - ( 2 H ) 300 - 320 Km
Empty Weight
438 Kg - 965 lbs
243 Kg - 535 lbs
680 Kg - 1500 lbs
204 Kg - 450 lbs
68 Kg - 150 lbs
2286 m - 7500 ft
1828 m - 6000 ft
Lenght Nose to Tail
6,7 m - 22'
2,6 m - 103"
- 300 m/min - 1000 fpm
9 m - 30' approx
Operative
Included operations and installed instruments
Rigged, balanced and flight tested 20 hours - EFIS Glass cockpit -
Compass - GPS - Engine's Gauges and Indicators