



|
ENGINE | |
|
GAS Turbine with FADEC | |
|
Max continuative power output ISA standard |
130 SHP |
|
DIMENSIONS | |
|
Max Lenght |
8.84 m (29.00 ft) |
|
Max Width |
1.60 m (5.25 ft) |
|
Max Height |
2.40 m (7.87 ft) |
|
Fuselage Width |
1.12 m (3.67 ft) |
|
Fuselage Height |
1.82 m (5.97 ft) |
|
Main rotor diameter |
7.63 m (25.00 ft) |
|
Tail rotor diameter |
1.28 m (4.20 ft) |
|
WEIGHTS | |
|
Empty weight |
290 Kg (639.3 lb) |
|
Empty weight (with floating) |
308 Kg (679.0 lb) |
|
Take off weight |
450 Kg (992.0 lb) |
|
Maximum take off weight |
500 Kg (1102.3 lb) |