| Primary Function |
|
Utility helicopter |
|
|
|
| Manufacturer |
|
Bell Helicopter Textron |
|
|
|
| Power plant |
|
Pratt and Whitney T400-CP-400 |
|
|
|
| Power |
|
Burst: 1290 shaft horsepower (transmission limited)
Continuous: 1134 shaft horsepower (transmission limited) |
|
|
|
| Length |
|
57.3 feet (17.46 meters) |
|
|
|
| Height |
|
14.9 feet (4.54 meters) |
|
|
|
| Rotor Diameter |
|
48 feet (14.62 meters) |
|
|
|
| Speed |
|
121 knots (139.15 miles per hour) at sea level |
|
|
|
| Ceiling |
|
14,200 feet (4331 meters)
(limited to 10,000 feet (3050 meters) by oxygen requirements) |
|
|
|
| Maximum takeoff weight |
|
10,500 pounds (4,767 kilograms) |
|
|
|
| Range |
|
172 nautical miles (197.8 miles) |
|
|
|
