| Specifications |
| Country of Origin |
|
| Builder |
|
| Role |
|
| Similar Aircraft |
|
| Dimensions (External) |
| Overall Length Rotors Turning |
22.80 m |
| Fuselage Length |
19.53 m |
| Width (excluding rotor) |
4.52 m |
| Overall Height |
6.62 m |
| Folded Length |
15.75 m |
| Folded Width |
5.20 m |
| Folded Height |
5.20 m |
| Main Rotor Diameter |
18.60 m |
| Tail Rotor Diameter |
4.00 m |
|
|
| Dimensions (Internal) |
| Cabin Length |
7.09 m |
| Cabin Width |
2.49 m |
| Cabin Height |
1.83 m |
|
|
| Accommodation |
|
| Cockpit |
Pilot and Co-Pilot or Observer |
| Cabin |
2 mission system operators |
| Cabin Volume |
29.0 cu m |
| Cabin Floor Area |
17.0 sq m |
| Rotor System |
|
| Main Rotor Type |
Fully articulated |
| Main Rotor Blades |
5 composite blades |
| Tail Rotor Type |
Teetering |
| Tail Rotor Blades |
4 composite blades |
|
|
| Weights |
| Maximum All Up Mass |
14600 kg |
| Cargo Hook Capacity |
4535 kg |
| Standard Fuel (4 tanks) |
3408 kg |
| Armament |
|
| Crew |
|
| Cost |
|
| User Countries |
|
