Pratt & Whitney Canada PT6A-34
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:certification |
gptkb:FAA
gptkb:Transport_Canada |
| gptkbp:compressionStages |
single axial, single centrifugal
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
approx. 19 in
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_Canada_PT6
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-34
|
| gptkbp:length |
approx. 62 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:powerOutput |
750 shp
|
| gptkbp:type |
turboprop
|
| gptkbp:usedInAircraft |
gptkb:Air_Tractor_AT-402
gptkb:Embraer_EMB_110_Bandeirante gptkb:Cessna_208_Caravan gptkb:PAC_Cresco gptkb:Beechcraft_King_Air_C90 |
| gptkbp:weight |
approx. 350 lb
|
| gptkbp:bfsParent |
gptkb:Viking_Air_DHC-6_Series_400
gptkb:De_Havilland_Canada_DHC-6_Twin_Otter |
| gptkbp:bfsLayer |
6
|