| Name | Bell 214 |
| Image |  |
| Role | Transport |
| Status | |
| Ceiling (m) | 5,950 |
| Crew | |
| Date First flight | 1970 |
| Date Introduction | 1972 |
| Date production ended | 1981 |
| Date production started | 1972 |
| Date retired | |
| Empty weight (kg) | 3,445 |
| Engine | turbomoteur [Turbomoteur] Avco-Lycoming [Lycoming_Engines] T5508D[1] |
| Height (m) | |
| Length (m) | |
| Maximum speed (m/s) | |
| Maximum weight at takeoff (kg) | 7,257 |
| Number built | 1 |
| Power (W) | |
| Range (m) | 500,000 |
| Rotor diameter (m) | |
| Country | |
| Constructor | Bell Aircraft, Bell Helicopter |
| entities - helicopter2 Relations |