Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:basedOn |
gptkb:Bell_206
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:crew |
1
|
| gptkbp:cruiseSpeed |
222 km/h
|
| gptkbp:emptyWeight |
1,180 kg
|
| gptkbp:engine |
gptkb:Allison_250-C30P
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
1992
|
| gptkbp:fuelType |
492 L
|
| gptkbp:height |
3.14 m
|
| gptkbp:introduced |
1992
|
| gptkbp:length |
13.00 m
|
| gptkbp:mainRotorDiameter |
10.16 m
|
| gptkbp:manufacturer |
gptkb:Bell_Helicopter
|
| gptkbp:maximumSpeed |
241 km/h
|
| gptkbp:maxTakeoffWeight |
1,973 kg
|
| gptkbp:range |
611 km
|
| gptkbp:role |
gptkb:helicopter
light helicopter |
| gptkbp:seatingCapacity |
6
|
| gptkbp:serviceCeiling |
6,096 m
|
| gptkbp:status |
in service
|
| gptkbp:variant |
gptkb:Bell_206L_LongRanger
|
| gptkbp:bfsParent |
gptkb:Bangladesh_Naval_Aviation
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bell 206L-4
|