Statements (50)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:capacity |
5
|
| gptkbp:crew |
1
|
| gptkbp:engine |
gptkb:Rolls-Royce_250-C20R
|
| gptkbp:firstFlight |
1992
|
| gptkbp:fuelCapacity |
120 gallons
|
| gptkbp:height |
3.6 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bell 206L-4
|
| gptkbp:introduced |
1992
|
| gptkbp:length |
13.4 m
|
| gptkbp:manufacturer |
gptkb:Bell_Helicopter
|
| gptkbp:maximumDepth |
1,000 lbs
|
| gptkbp:maxSpeed |
130 knots
|
| gptkbp:maxTakeoffWeight |
2,268 kg
|
| gptkbp:notableFeature |
high speed
reliability advanced avionics versatility high reliability good stability low noise levels ease of maintenance high resale value low operating costs good visibility good climb rate comfortable cabin good fuel efficiency easy to fly widely used in various industries excellent maneuverability good handling characteristics proven design good payload capacity available in multiple configurations good for training purposes strong performance in hot conditions wide range of configurations |
| gptkbp:numberBuilt |
over 1,000
|
| gptkbp:primaryUser |
tourism
law enforcement medical services corporate transport |
| gptkbp:range |
400 nautical miles
|
| gptkbp:role |
utility helicopter
|
| gptkbp:services |
15,000 ft
|
| gptkbp:successor |
gptkb:Bell_407
|
| gptkbp:variant |
gptkb:Bell_206
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:wingspan |
nan
|