Bell 212
Overview
The Bell 212 is a helicopter aircraft manufactured by Bell, with the profile centered on its utility helicopter role. It first flew in 1968 and entered service in 1968. Production is recorded as ending in 1998. The listed configuration provides for a crew of 2 and passenger capacity of 14. Power is provided by 1 Pratt & Whitney Canada PT6T-3 (TwinPac) engine. Recorded dimensions include wingspan 48 ft 0 in, height 12 ft 6.83 in. Maximum takeoff weight is listed as 11200. Listed performance includes cruise speed 100 kt, range 237 nautical miles, service ceiling 17400 ft. Its ICAO type designator is B212. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
Specifications
| ICAO Type Code | B212 |
|---|---|
| First Flight | 1968 |
| Introduction Date | 1968 |
| Crew | 2 |
| Passenger Capacity | 14 |
| Wingspan / Rotor Diameter | 48 ft 0 in |
| Height | 12 ft 6.83 in |
| Empty Weight | 6529 lb |
| Max Takeoff Weight | 11200 lb |
| Cruise Speed | 100 kt |
| Range | 237 nm |
| Service Ceiling | 17400 ft |
| Engine Manufacturer | Pratt & Whitney Canada |
| Engine Model | PT6T-3 (TwinPac) |
| Engine Count | 1 |
Data verification status: Verified
Source: ICAO Aircraft Type Designators