Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypass_ratio |
5.1:1
|
| gptkbp:compressor_type |
axial
|
| gptkbp:configuration |
twin-spool
|
| 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:first_flight |
gptkb:1982
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CFM56-2 C3
|
| gptkbp:length |
3.4 m
|
| gptkbp:maintenance |
4,000 hours
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:noise_level |
Stage 3
|
| gptkbp:notable_users |
gptkb:Airbus
gptkb:Boeing_737 |
| gptkbp:propulsion |
22,000 lbf
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:CFM56-2_C
|
| gptkbp:bfsLayer |
6
|