Bell 407
Overview
The Bell 407 is a helicopter aircraft manufactured by Bell, with the profile centered on its civil helicopter role. It first flew in 1995-06-29 and entered service in 1996. The current production-status field is listed as In Production. The listed configuration provides for a crew of 1 and passenger capacity of 6. Power is provided by 1 Rolls-Royce 250-C47B engine. Its ICAO type designator is B407. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
First Flight
Jun 29, 1995
Crew
1
Passengers
6
Range
324 nm
Cruise Speed
133 kt
Max Speed
140 kt
Specifications
| ICAO Type Code | B407 |
|---|---|
| First Flight | Jun 29, 1995 |
| Introduction Date | 1996 |
| Crew | 1 |
| Passenger Capacity | 6 |
| Length | 41 ft 10 in |
| Wingspan / Rotor Diameter | 35 ft rotor diameter |
| Height | 10 ft 11 in |
| Empty Weight | 2700 lb |
| Max Takeoff Weight | 5000 lb |
| Cruise Speed | 133 kt |
| Max Speed | 140 kt |
| Range | 324 nm |
| Service Ceiling | 20000 ft |
| Engine Manufacturer | Rolls-Royce |
| Engine Model | 250-C47B |
| Engine Count | 1 |
Data verification status: Partially Verified
Source: ICAO Aircraft Type Designators