Pratt & Whitney Canada PW308C
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Dassault_Falcon_2000EX
|
| gptkbp:bypassRatio |
4.2:1
|
| gptkbp:certification |
gptkb:Transport_Canada
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
33.5 in
|
| gptkbp:family |
gptkb:PW300
|
| gptkbp:firstFlight |
1996
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW308C
|
| gptkbp:length |
75.6 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:thrust |
7,000 lbf
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:usedOn |
gptkb:Dassault_Falcon_2000DX
gptkb:Dassault_Falcon_2000LX |
| gptkbp:weight |
1,625 lb
|
| gptkbp:bfsParent |
gptkb:Dassault_Falcon_2000
gptkb:Dassault_Falcon_2000DX gptkb:Dassault_Falcon_2000EX gptkb:Dassault_Falcon_2000LXS gptkb:Dassault_Falcon_2000S |
| gptkbp:bfsLayer |
7
|