Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:capacity |
4 passengers
|
| gptkbp:crew |
1
|
| gptkbp:developedBy |
gptkb:Bell_YOH-4
gptkb:Bell_206B_JetRanger_II |
| gptkbp:emptyWeight |
1,691 lb (767 kg)
|
| gptkbp:engine |
gptkb:Allison_250-C18
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
1966
|
| gptkbp:height |
9 ft 4 in (2.84 m)
|
| gptkbp:introduced |
1967
|
| gptkbp:length |
39 ft 8 in (12.09 m)
|
| gptkbp:mainRotorDiameter |
33 ft 4 in (10.16 m)
|
| gptkbp:manufacturer |
gptkb:Bell_Helicopter
|
| gptkbp:maximumSpeed |
120 mph (193 km/h)
|
| gptkbp:maxTakeoffWeight |
3,200 lb (1,451 kg)
|
| gptkbp:range |
374 mi (602 km)
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:serviceCeiling |
13,500 ft (4,115 m)
|
| gptkbp:usedBy |
civilian operators
military operators |
| gptkbp:bfsParent |
gptkb:Bell_206_JetRanger
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bell 206A
|