Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:Flight
|
| gptkbp:bypass_ratio |
5.5:1
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:diameter |
1,000 mm
|
| gptkbp:engine |
gptkb:CF34
|
| gptkbp:first_flight |
gptkb:1994
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF34-8 L12
|
| gptkbp:length |
1,800 mm
|
| gptkbp:maintenance |
4,000 hours
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:max_speed |
10,000 RPM
|
| gptkbp:noise_level |
Stage 4 compliant
|
| gptkbp:notable_users |
gptkb:Bombardier_CRJ-900
|
| gptkbp:propulsion |
18,500 lbf
|
| gptkbp:related_aircraft |
gptkb:Embraer_E-Jet_series
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:CF34-8_L
|
| gptkbp:bfsLayer |
7
|