Pratt & Whitney Canada T400-CP-400
GPTKB entity
Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:basedOn |
gptkb:Pratt_&_Whitney_Canada_PT6T
|
| gptkbp:configuration |
twin power section
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:firstFlight |
1969
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada T400-CP-400
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:powerOutput |
1,800 shp
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
gptkb:United_States_Marine_Corps gptkb:United_States_Navy |
| gptkbp:usedIn |
gptkb:Bell_UH-1N_Twin_Huey
|
| gptkbp:bfsParent |
gptkb:UH-1N_Huey
gptkb:Bell_AH-1J_SeaCobra |
| gptkbp:bfsLayer |
6
|