Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
helicopters
light fixed-wing aircraft |
| gptkbp:civilianDesignation |
gptkb:Allison_250
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:firstFlight |
1959
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison T63
|
| gptkbp:introduced |
1960s
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:militaryDesignation |
gptkb:T63
|
| gptkbp:powerOutput |
317 to 715 shaft horsepower
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Rolls-Royce_M250
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Bell_UH-1_Iroquois
gptkb:Bell_206_JetRanger |
| gptkbp:bfsParent |
gptkb:Allison_T63-A-5_turboshaft
|
| gptkbp:bfsLayer |
7
|