Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
Boeing 737 aircraft
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
1.5 m
1.1 m |
| gptkbp:emissions_standard |
CAEP/6
|
| gptkbp:engine |
gptkb:CFM56_family
|
| gptkbp:engine_configuration |
dual spool
|
| gptkbp:first_flight |
gptkb:1982
|
| gptkbp:fuel_economy |
0.5 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
CFM56-2 C5
|
| gptkbp:length |
3.3 m
|
| gptkbp:maintenance |
4,000 hours
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:noise_level |
Stage 3 compliant
|
| gptkbp:number_of_engines |
2 per aircraft
|
| gptkbp:number_of_stages |
gptkb:10
|
| gptkbp:operational_use |
commercial aviation
|
| gptkbp:propulsion |
22,000 lbf
|
| gptkbp:service_ceiling |
41,000 ft
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:CFM56-2_C
|
| gptkbp:bfsLayer |
6
|