Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypass_ratio |
5.5:1
|
| gptkbp:compressor_type |
gptkb:6
|
| gptkbp:control_system |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:diameter |
68 inches
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
PW6000 series
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:noise_level |
Stage 4 compliant
|
| gptkbp:original_run |
gptkb:1999
|
| gptkbp:propulsion |
18,500 to 24,000 lbf
|
| gptkbp:successor |
PW6100
|
| gptkbp:turbine_type |
2
|
| gptkbp:type |
high bypass turbofan
|
| gptkbp:used_in |
gptkb:Airbus
|
| gptkbp:weight |
approximately 3,000 lb
|
| gptkbp:bfsParent |
gptkb:PW6000_family
|
| gptkbp:bfsLayer |
8
|