Pratt & Whitney Canada PT6A-65B
GPTKB entity
Statements (50)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turboprop engine
|
| gptkbp:aircraft |
gptkb:Cessna_208_Caravan
gptkb:Pilatus_PC-12 gptkb:Beechcraft_King_Air_200 Dornier 228 |
| gptkbp:application |
aircraft
|
| gptkbp:compressionRatio |
8:1
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
16.5 in
|
| gptkbp:engine |
300 lb
civil aviation rear-mounted 16.5 in 45.5 in turboprop engine design |
| gptkbp:engineConfiguration |
free turbine
|
| gptkbp:engineType |
gptkb:PT6A-65
advanced technology turboprop high reliability environmentally friendly high power output low noise levels ease of maintenance low operating costs robust design versatile applications starter-generator good fuel efficiency proven performance |
| gptkbp:exhaustSystem |
straight exhaust
|
| gptkbp:fuel_capacity |
0.5 lb/hp/hr
200 lb/hr |
| gptkbp:fuelType |
Jet A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6A-65B
|
| gptkbp:introduced |
1980
|
| gptkbp:length |
45.5 in
|
| gptkbp:maintenance |
1,500 hours
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:operationalRange |
1,000 nautical miles
|
| gptkbp:powerOutput |
1,100 shp
|
| gptkbp:propulsion |
3.67
1,100 lb 3.67 hp/lb |
| gptkbp:related_engine |
PT6 family
|
| gptkbp:reliability |
high
|
| gptkbp:service_ceiling |
25,000 ft
|
| gptkbp:setting |
twin-shaft
|
| gptkbp:weight |
approximately 300 lb
|