Bell 214B
Overview
The Bell 214B is a helicopter aircraft manufactured by Bell, with the profile centered on its utility helicopter role. It first flew in 1970 and entered service in 1972. Production is recorded as ending in 1981. The listed crew requirement is 2. Power is provided by 1 Lycoming T5508D engine. Listed performance includes cruise speed 112 mph kt. Its ICAO type designator is B214. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
First Flight
1970
Crew
2
Cruise Speed
112 mph
Specifications
| ICAO Type Code | B214 |
|---|---|
| First Flight | 1970 |
| Introduction Date | 1972 |
| Crew | 2 |
| Cruise Speed | 112 mph |
| Engine Manufacturer | Lycoming |
| Engine Model | T5508D |
| Engine Count | 1 |
Data verification status: Verified
Source: ICAO Aircraft Type Designators