Bell Helicopter Bell 407
Photo ©: Karsten Palt
Bell 407
Light Utility Helicopter
The Bell 407 is a single-engine seven-seat light utility helicopter produced by the US-American manufacturer Bell Helicopter Textron, produced in Mirabel, Quebec (Canada).
| Crew | 1 | |
| Passengers | 6 | |
| Propulsion | 1 Turboshaft Engine | |
| Engine Model | Allison / Rolls-Royce 250-C47 | |
| Engine Power | 503 kW | 675 shp |
| Speed | 259 km/h | 140 kts 161 mph |
| Service Ceiling | 6.096 m | 20.000 ft |
| Range | 550 km | 297 NM 342 mi. |
| Empty Weight | 1.178 kg | 2.597 lbs |
| max. Takeoff Weight | 2.381 kg | 5.249 lbs |
| Rotor Blades (main/tail) | 4/2 | 4/2 |
| Main Rotor Diameter | 10,66 m | 35,0 ft |
| Tail Rotor Diameter | 1,56 m | 5,1 ft |
| Rotor Disc Area | 89,2 m² | 960 ft² |
| Length (Fuselage) | 10,57 m | 34,7 ft |
| Length | 12,68 m | 41,6 ft |
| Height | 3,10 m | 10,2 ft |
| First Flight | 21.04.1994 | |
| Production Status | in production | |
| Developed from | Bell 206 | |
| ICAO Code | B407 | |
| FAA TCDS | H2SW | |
| Data for (Version) | Bell 407 | |
Remarks
The Bell 407 is a development of the Bell 206L-4 Long Ranger with four-blade main-rotor.
| Weblinks | Extras |
| Bell Helicopter Textron |
print view| [Photo-ID: 681] © Karsten Palt 2007-09-15 | |
 | Bell 407 Pabst Air Reg.: D-HJSP c/n: 53500 |
| Airport-Days 2007 [Hamburg-Fuhlsbüttel (EDDH / HAM)] | |