Bell 230
Overview
The Bell 230 is a helicopter aircraft manufactured by Bell, with the profile centered on its civil helicopter role. It first flew in 1991-08-12 and entered service in 1991. Production is recorded as ending in 1995. The listed configuration provides for a crew of 2 and passenger capacity of 8. Power is provided by 2 Allison (Rolls-Royce) 250-C30G2 engines. Maximum takeoff weight is listed as 8400. Listed performance includes cruise speed 141 kt. Its ICAO type designator is B230. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
First Flight
Aug 12, 1991
Crew
2
Passengers
8
Range
380 nm
Cruise Speed
141 kt
Max Speed
150 kt
Specifications
| ICAO Type Code | B230 |
|---|---|
| First Flight | Aug 12, 1991 |
| Introduction Date | 1991 |
| Crew | 2 |
| Passenger Capacity | 8 |
| Length | 50 ft 9 in |
| Wingspan / Rotor Diameter | 42 ft rotor diameter |
| Height | 11 ft 8 in |
| Empty Weight | 5097 lb |
| Max Takeoff Weight | 8400 lb |
| Cruise Speed | 141 kt |
| Max Speed | 150 kt |
| Range | 380 nm |
| Service Ceiling | 15000 ft |
| Engine Manufacturer | Allison (Rolls-Royce) |
| Engine Model | 250-C30G2 |
| Engine Count | 2 |
Data verification status: Verified
Source: ICAO Aircraft Type Designators