Technical Specifications
|
Unit |
Value |
| Length |
ft |
30' 4" |
| Heigth |
ft |
8' 9" |
| Cabin width |
ft |
4' 5" |
| Main rotor diameter |
ft |
25' 2" |
| Blade number |
- |
2 |
| Blade speed at 100% RPM |
T/Min |
517 |
| Blade chord |
inch |
7,68 |
| Blade twist |
degree |
Linear twist |
| Articulation |
- |
Free to teeter |
| Blade profile |
Naca |
Asymmetrical (composite) |
| Tail rotor diameter |
inch |
43,30 (composite) |
| Blade number |
- |
2 |
| Blade speed at 100 % RPM |
T/Min |
3.340 |
| Blade twist |
degree |
0 |
| Articulation |
|
Free to teeter |
| Engine |
- |
Turbine 150 hp |
| Turbine constant power at |
HP |
150 (112 Kw) |
| Empty weigth |
lb |
727 |
| Pilot + passenger + baggages |
lb |
483 |
| Maximum gross weigth |
lb |
1543 |
| Maximum rate of climb |
Ft/min |
1.100 |
| Absolute ceilling |
Ft |
18.500 |
| Service ceilling |
Ft |
11.000 |
| Hover ceilling out of effect ; ISA |
Ft |
9.200 |
| Hover ceilling in ground effect ; ISA |
Ft |
6.200 |
| Cruise speed |
Kt |
89 |
| Vne |
Kt |
102 |
| Autorotation speed |
Kt |
60 |
| Consumption |
U.S gallons |
16 |
| Fuel type |
- |
Jet-A, kerosene or diesel |
| Fuel tanks capacity |
U.S gallons |
50 |
| Endurance |
Hours |
+ / - 4 |
| Range |
Nm |
+ / - 213 |
|
