Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:Boeing_737_Next_Generation
|
| gptkbp:bypass_ratio |
5.5:1
|
| gptkbp:cancellation_reason |
hush kit available
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:control_system |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
61 inches
|
| gptkbp:emissions_standard |
ICAO Chapter 4
|
| gptkbp:first_flight |
gptkb:1997
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CFM56-7
|
| gptkbp:maintenance |
4,000 hours
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:operational_range |
over 30 years
|
| gptkbp:produces |
over 8,000 engines
|
| gptkbp:propulsion |
18,500 to 27,300 lbf
|
| gptkbp:successor |
gptkb:CFM_LEAP
|
| gptkbp:turbine_type |
two-stage high-pressure turbine
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:weight |
3,000 lb
|
| gptkbp:bfsParent |
gptkb:CFM56_Engine
gptkb:CFM56 gptkb:CFM56_engine |
| gptkbp:bfsLayer |
5
|