Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
regional aircraft
|
| gptkbp:bypass_ratio |
8:1
|
| gptkbp:cancellation_reason |
yes
|
| gptkbp:compressor_type |
gptkb:6
|
| gptkbp:configuration |
twin-spool
|
| gptkbp:control_system |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:diameter |
1,600 mm
1,500 mm |
| gptkbp:emissions_standard |
CAEP/6
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
PW1200 G-16
|
| gptkbp:length |
3,200 mm
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:original_run |
gptkb:2013
|
| gptkbp:propulsion |
16,000 lbf
|
| gptkbp:turbine_type |
2
|
| gptkbp:type |
geared turbofan
|
| gptkbp:used_in |
gptkb:Bombardier_CSeries
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_PW1200_G
|
| gptkbp:bfsLayer |
6
|