Bell 412
Overview
The Bell 412EP is a helicopter aircraft manufactured by Bell, with the profile centered on its utility helicopter role. It first flew in 1979-08 and entered service in 1981-01. The current production-status field is listed as In Production. The listed configuration provides for a crew of 2 and passenger capacity of 13. Power is provided by 2 Pratt & Whitney Canada PT6T-3D (Twin-Pac) engines. Listed performance includes maximum speed 161 kt. Its ICAO type designator is B412. 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 1979
Crew
2
Passengers
13
Range
357 nm
Cruise Speed
122 kt
Max Speed
161 kt
Specifications
| ICAO Type Code | B412 |
|---|---|
| First Flight | Aug 1979 |
| Introduction Date | Jan 1981 |
| Crew | 2 |
| Passenger Capacity | 13 |
| Length | 56 ft |
| Wingspan / Rotor Diameter | 46 ft rotor diameter |
| Height | 15 ft |
| Empty Weight | 6790 lb |
| Max Takeoff Weight | 11900 lb |
| Cruise Speed | 122 kt |
| Max Speed | 161 kt |
| Range | 357 nm |
| Service Ceiling | 20000 ft |
| Engine Manufacturer | Pratt & Whitney Canada |
| Engine Model | PT6T-3D (Twin-Pac) |
| Engine Count | 2 |
Data verification status: Verified
Source: ICAO Aircraft Type Designators