Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:capacity |
14 passengers
|
| gptkbp:crew |
2
|
| gptkbp:emptyWeight |
3,175 kg
|
| gptkbp:enginePower |
2,930 shp
|
| gptkbp:engineType |
Lycoming LTC4B-8 turboshaft
|
| gptkbp:firstFlight |
1970
|
| gptkbp:height |
4.6 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bell 214A
|
| gptkbp:introduced |
1972
|
| gptkbp:length |
17.4 m
|
| gptkbp:mainRotorDiameter |
15.24 m
|
| gptkbp:manufacturer |
gptkb:Bell_Helicopter
|
| gptkbp:maximumSpeed |
296 km/h
|
| gptkbp:maxTakeoffWeight |
6,804 kg
|
| gptkbp:primaryUser |
gptkb:Iranian_Army
|
| gptkbp:range |
560 km
|
| gptkbp:relatedTo |
gptkb:Bell_205
gptkb:Bell_214B |
| gptkbp:serviceCeiling |
4,570 m
|
| gptkbp:bfsParent |
gptkb:Bell_214
|
| gptkbp:bfsLayer |
6
|