Bell 222
Overview
The Bell 222 is a helicopter aircraft manufactured by Bell, with the profile centered on its civil helicopter role. It first flew in 1976-08-13 and entered service in 1979. Production is recorded as ending in 1991. The listed configuration provides for a crew of 2 and passenger capacity of 8. Power is provided by 2 Lycoming (Textron/Avco) LTS101-750C engines. Recorded dimensions include length 42 ft 2 in, wingspan 42 ft 0 in, height 11 ft 6 in. Maximum takeoff weight is listed as 8250. Listed performance includes cruise speed 130 kt, range 390 nautical miles, service ceiling 10300 ft. Its ICAO type designator is B222. 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 | B222 |
|---|---|
| First Flight | Aug 13, 1976 |
| Introduction Date | 1979 |
| Crew | 2 |
| Passenger Capacity | 8 |
| Length | 42 ft 2 in |
| Wingspan / Rotor Diameter | 42 ft 0 in |
| Height | 11 ft 6 in |
| Empty Weight | 4577 lb |
| Max Takeoff Weight | 8250 lb |
| Cruise Speed | 130 kt |
| Range | 390 nm |
| Service Ceiling | 10300 ft |
| Engine Manufacturer | Lycoming (Textron/Avco) |
| Engine Model | LTS101-750C |
| Engine Count | 2 |
Data verification status: Verified
Source: ICAO Aircraft Type Designators