BELL® 407® Data
This data is generalised for informational purposes, gathered by in-house tests. If you wish to know further details or specifics, then please contact us.
| Weight |
|
|
| Maximum Gross Weight (with IIGW kit) |
5,250 lbs |
2,381 kgs |
| Empty Weight (standard config) |
2,676 lbs |
1,214 kgs |
| Useful Load (with IIGW kit) |
2,582 lbs |
1,171 kgs |
| Useful Load with Full Fuel |
1,832 lbs |
830 kgs |
| Maximum External Load (cargo hook) |
2,646 lbs |
1,200 kgs |
| Size |
|
|
| Cabin Width (aft passenger) |
3’11” ft |
1.2 m |
| Cabin Height (aft passenger) |
3’11” ft |
1.2 m |
| Cabin Length (aft passenger) |
5’0″ ft |
1.5 m |
| External Length |
34’9″ ft |
10.57 m |
| External Length (including blades) |
41’7″ ft |
12.68 m |
| External Width (at horiz. fin) |
7’4″ ft |
2.22 m |
| External Height (low skids – top vert. fin) |
10’3″ ft |
3.10 m |
| Rotor Diameter |
35’0″ ft |
10.66 m |
| Performance |
|
|
| Service Ceiling |
20,000 ft |
6,096 m |
| Hover Ceiling, IGE |
19,200 ft |
5,852 m |
| Hover Ceiling, OGE |
17,600 ft |
5,364 m |
| Rate Of Climb |
800 fpm |
243 mpm |
| Capacities |
|
| Required Crew |
1 |
| Passengers |
6 |
| Rotor Blades |
|
| Main Rotor |
4 |
| Tail Rotor |
2 |
| Speed |
|
|
| VNE (Maximum Air Speed) |
140 kts |
161 mph |
| Long Range Cruise Speed |
120 kts |
138 mph |
| Range |
|
| Maximum Fuel Range (LRC Speed) |
342 nautical mi |
| Endurance (Loiter Speed, 60 ktas) |
4.0 hrs |
| Fuel |
|
| Fuel Capacity (standard) |
483.8 litres / 127.8 US Gallon |
| Fuel Consumption (average) |
170 litres p/hour |
| Auxiliary Tank |
72 litres |
| Engine |
|
|
| 7 Place – Single Engine |
|
|
| Manufacturer |
Allison |
|
| Model |
250-C47P |
|
| Engine Power |
813 shp |
606 kw |
| Takeoff Power |
674 hp |
503 kw |
| Maximum Continuous |
701 shp |
523 kw |
| Transmission |
|
|
| Take Off |
674 shp |
503 kw |
| Maximum Continuous |
630 shp |
470 kw |
