Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:basedOn |
gptkb:Bell_214
|
| gptkbp:capacity |
14 passengers
|
| gptkbp:countryOfOrigin |
gptkb:Italy
|
| gptkbp:crew |
2
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
1970s
|
| https://www.w3.org/2000/01/rdf-schema#label |
Agusta-Bell 214
|
| gptkbp:length |
17.4 m
|
| gptkbp:mainRotorDiameter |
14.63 m
|
| gptkbp:manufacturer |
gptkb:Bell_Helicopter
gptkb:Agusta |
| gptkbp:maxTakeoffWeight |
6,804 kg
|
| gptkbp:powerplant |
Lycoming LTC4B-8 turboshaft
|
| gptkbp:primaryUser |
gptkb:Iranian_military
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:status |
in service
|
| gptkbp:bfsParent |
gptkb:Imperial_Iranian_Air_Force
|
| gptkbp:bfsLayer |
7
|