Comparison of Bell 212 and Bell 214 [S]ave
| Attribute |  Bell 214 × |  Bell 212 × |
|---|---|---|
| General | ||
| Manufacturer | Bell Helicopter | Bell Helicopter |
| Model | Bell 214 | Bell 212 |
| Country | United States | United States |
| Manufactured from (year) | 1970 | 1968 |
| Manufactured to (year) | 1981 | 1998 |
| Type | Mid Size Helicopters | Mid Size Helicopters |
| Icao | B214 | B212 |
| Performance | ||
| Engine | 1x Lycoming LTC4B-8D | 1x Pratt & Whitney Canada PT6T-3 |
| Power, hp (hp) | 2,930 | 1,800 |
| Max cruise speed (km/h) | 259 | 222 |
| Travel range (km) | 407 | 463 |
| Service ceiling (m) | 4,999 | 5,304 |
| Rate of climb (m/sec) | 7.62 | 8.86 |
| Weights | ||
| Max take off weight (kg) | 6,800 | 5,080 |
| Max payload (kg) | 3,000 | 2,130 |
| Fuel tank capacity (l) | 1,893 | 1,120 |
| Dimensions | ||
| Seats | 2 | 15 |
| Cabin height (m) | 1.3 | 1.2 |
| Cabin width (m) | 2.4 | 2.4 |
| Cabin length (m) | 2.3 | 2.7 |
| Exterior length (m) | 14.65 | 17.4 |
| Tail height (m) | 3.9 | 3.8 |
| Fuselage diameter (m) | 2.5 | 2.6 |
| Wing span (m) | 15.25 | 14.6 |
| Wing tips | No Winglets | No Winglets |
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