Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypass_ratio |
5.1:1
|
| gptkbp:compression_ratio |
30:1
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
1.68 m
1.53 m |
| gptkbp:engine |
CF M56-5 B
CF M56-5 A |
| gptkbp:engine_type |
turbofan
axial compressor high-pressure turbine |
| gptkbp:first_flight |
gptkb:1988
|
| gptkbp:fuel_capacity |
high efficiency
|
| gptkbp:fuel_type |
gptkb:Jet_A
annular combustor |
| https://www.w3.org/2000/01/rdf-schema#label |
CFM56-5 E
|
| gptkbp:length |
3.3 m
|
| gptkbp:maintenance |
5,000 hours
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:noise_level |
Stage 3 compliant
|
| gptkbp:produced_by |
over 8,000 units
|
| gptkbp:propulsion |
22,000 to 34,000 lbf
|
| gptkbp:services |
gptkb:1994
|
| gptkbp:weight |
3,000 kg
|