Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:average_temperature |
1,500 ° F
|
| gptkbp:bypass_ratio |
5.1:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:compressor_type |
gptkb:5
|
| gptkbp:control_system |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:diameter |
68 in
3.0 ft |
| gptkbp:engine |
gptkb:CFM56
|
| gptkbp:first_flight |
gptkb:1982
|
| gptkbp:fuel_economy |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CFM56-2 N6
|
| gptkbp:length |
11.5 ft
|
| gptkbp:maintenance |
4,000 hours
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:noise_level |
Stage 3 compliant
|
| gptkbp:propulsion |
22,000 lbf
|
| gptkbp:related_aircraft |
gptkb:Airbus
gptkb:Boeing_737 |
| gptkbp:turbine_type |
2
|
| gptkbp:weight |
3,000 lb
|
| gptkbp:bfsParent |
gptkb:CFM56-2_N
|
| gptkbp:bfsLayer |
7
|