Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:avionicsUpgrade |
Digital Automatic Flight Control System (DAFCS)
|
| gptkbp:basedOn |
gptkb:Boeing_CH-47_Chinook
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:crew |
3
|
| gptkbp:designation |
HC6
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
2012
|
| gptkbp:height |
5.7 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Boeing Chinook HC6
|
| gptkbp:introduced |
2013
|
| gptkbp:length |
30.1 m
|
| gptkbp:manufacturer |
gptkb:Boeing
|
| gptkbp:maximumSpeed |
302 km/h
|
| gptkbp:maxTakeoffWeight |
24,500 kg
|
| gptkbp:numberBuilt |
14
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:operator |
gptkb:Royal_Air_Force
|
| gptkbp:primaryUser |
gptkb:United_Kingdom
|
| gptkbp:range |
741 km
|
| gptkbp:role |
heavy-lift transport helicopter
|
| gptkbp:rotorConfiguration |
tandem rotors
|
| gptkbp:usedFor |
gptkb:aircraft
disaster relief cargo transport medical evacuation |
| gptkbp:bfsParent |
gptkb:No._18_Squadron_RAF
|
| gptkbp:bfsLayer |
8
|