Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:basedOn |
gptkb:Bell_412
|
| gptkbp:capacity |
10
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:crew |
2
|
| gptkbp:engineType |
twin-turboshaft
|
| gptkbp:firstFlight |
1997
|
| gptkbp:height |
4.6 m
|
| gptkbp:introduced |
1997
|
| gptkbp:length |
17.1 m
|
| gptkbp:manufacturer |
gptkb:Bell_Helicopter
|
| gptkbp:maximumSpeed |
140 knots
|
| gptkbp:maxTakeoffWeight |
5,398 kg
|
| gptkbp:numberBuilt |
14
|
| gptkbp:operator |
gptkb:Royal_Air_Force
|
| gptkbp:powerplant |
2 × Pratt & Whitney Canada PT6T-3D turboshaft engines
|
| gptkbp:primaryUser |
gptkb:Defence_Helicopter_Flying_School
|
| gptkbp:range |
420 nautical miles
|
| gptkbp:replacedBy |
Airbus H135 Juno HT1
|
| gptkbp:retired |
2018
|
| gptkbp:usedFor |
training
|
| gptkbp:bfsParent |
gptkb:Juno_HT1_helicopter
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bell Griffin HT1
|