ghibli260-01.html - 2009
Updated: 2012, 2nd of February

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 -
Seats
LS7 - Max. Power - Helicopter use -
LS7 - Economy configuration - Power output - Helicopter use
LS7 - Special confiuration - Max. Power - Helicopter use
LS7 - Engine - Max. admitted Power - Automotive use ( Corvette )
LS7 - Max. Torque -
4
280 HP @ 3250 rpm - Torque: 430 lb-ft - 582 Nm
260 HP @ 3050 rpm - Torque: 420 lb-ft - 569 Nm
300 HP @ 3500 rpm - Torque: 440 lb-f - 595 Nm
505 HP ( 377 Kw ) @ 6300 rpm - Torque: 405 lb-f - 548 Nm
470 lb-ft / 637 Nm @ 4800 rpm - 450 HP ( 337 Kw )
| HP | Kw | r.p.m. | lb-ft | Nm | REMARK |
| 450 | 337 | 4800 | 470 | 637 | MAX Torque |
| 260 | 195 | 3050 | 420 | 569 | Cruis. power |
| 280 | 210 | 3250 | 430 | 582 | Max Standard Conf. Power - Helic. |
| 300 | 225 | 3500 | 440 | 595 | Max. Helic. Power |
| 505 | 377 | 6300 | 420 | 569 | MAX. Eng. Power |
STROKE - FUEL TYPE
4 - Automobile fuel - Unleaded Gasoline
Controls
FADEC ( Fully Automotad Digital Electronic Control ) Electronic Throttle Governor
Standard Fuel Capacity
215 l - 57 U.S. Gallon
Service Ceiling
3,600 m - 12,000 feet
Main Rotor Blades
3 Blades - 10 m Diam - 33'
Main Rotor Blades r.p.m
220 r.p.m standard max.
Tail Rotor Blades
2 Blades - 175 cm Diam ( 5' 9" )
Cabin Width
1,52 m - 5'
Max. Speed - V.N.E.
177 Km/h - 110 mph
Endurance min./Max. Hours
with LS7 Engine : 6H @ 140 Km/h - 75 kts
with Lycoming VO-435-A1F6H : 4.3 H @ 140 Km/h - 75 kts
Consumption
LS 7 Engine: 9 - 10 US Gall/h - 34 - 38 lt/h -
Lycoming VO-435-A1F: 14 US Gall/h - 54 - 55 lt/h -
Range
with LS7 Engine : 840 - 864 Km / 453- 466 nml
with Lycoming VO-435-A1F engine : 600 - 620 Km / 324-334 nml
Useful Load MTOW
430 Kg - 950 lbs
Gross Weight - MTOWA - Max Weight
1224 Kg - 2700 lbs
Height Total
2,62 m - 8' 7"
Status
Operative
The ARMORED configuration - Click on:Armored model