BELL® 206® BIII® JetRanger® 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) |
3,350 LBS |
1,519KGS |
| Empty Weight (standard config) |
1,710 LBS |
775 KGS |
| Useful Load (with IIGW kit) |
1,635 LBS |
741 KGS |
| Useful Load with Full Fuel |
1,135 LBS |
514 KGS |
| Maximum External Load (cargo hook) |
1,500 LBS |
680 KGS |
| Size |
|
|
| Cabin Length (aft seat and leg room) |
3’3″ ft |
99 m |
| Cabin Width |
3’11” ft |
1.19 m |
| Cabin Height |
4’3″ ft |
1.30 m |
| External Length |
32’5″ ft |
9.89 m |
| External Length (including blades) |
39’4″ ft |
11.96 m |
| External Width (at horiz. fin) |
6’4″ |
1.96 m |
| External Height (low skids, to mast) |
9’7″ |
2.91 m |
| Rotor Diameter |
33’4″ |
10.16 m |
| Performance |
|
|
| Service ceiling |
20,000 ft |
6,096 m |
| Hover ceiling, IGE |
19,500 ft |
5,943 m |
| Hover ceiling, OGE |
14,800 ft |
4,511 m |
| Capacities |
|
| Required crew |
1 |
| Passengers |
4 |
| Rotor blades |
|
| Main rotor |
2 |
| Tail rotor |
2 |
| Speed |
|
|
| Vne (maximum air speed) |
130 kts |
149 mph |
| Long range cruise speed |
113 kts |
130mph |
| Range |
|
| Maximum Fuel Range (LRC Speed) |
389 nautical mi |
| Endurance (Loiter Speed, 57 ktas) |
4.7 hrs |
| Fuel |
|
| Fuel Capacity (standard) |
344 litres / 91 US Gallon |
| Fuel Consumption (average) |
95 litres p/hour |
| Auxiliary Tank |
N/A |
| Engine |
|
|
| Single Engine |
|
|
| Manufacturer |
Allison |
|
| Model |
250-C20 B / J |
|
| Engine Power |
420 shp |
313 kw |
| Maximum Continuous |
370 shp |
276 kw |
| Transmission |
|
|
| Take off |
317 shp |
236 kw |
| Maximum continuous |
270 shp |
201 kw |
