1976 · Twin-engine intermediate turbine helicopter
Specifications
| Engine | 2 x Lycoming LTS101-650C-3 630 shp |
|---|---|
| Capacity | 1 + 9 |
| Length (m) | 15.1 |
| Height (m) | 3.56 |
| Blades | 2 |
| Rotor diam. (m) | 12.2 |
| Weight (kgs) | Empty: 2066 Max: 3500 |
| Speed (km/h) | Max: 240 |
| Range (km) | 600 |
| Ceiling (m) | 3900 |
| Rate/Climb (m/min) | 481 |
Derivatives & Versions
| 222B | 1982 | Uses the more powerful Honeywell (formerly Lycoming) LTS-101-750Cs and a larger main rotor |
| 222UT | 1983 | The Utility Twin is based on 222B but equipped with skids. |
| → 230 | 1991 | The Bell 230 is a development of the model 222 with its Lycoming engines replaced by two Allison 250 turboshafts, plus other refinements including optional skid or wheel undercarriage. |