Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
5.7:1
|
| gptkbp:certification |
gptkb:EASA
gptkb:FAA |
| gptkbp:compressionRatio |
30:1
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_States |
| gptkbp:family |
gptkb:CFM56
|
| gptkbp:firstFlight |
1994
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CFM56-5B
|
| gptkbp:length |
98.4 in
|
| gptkbp:mainRotorDiameter |
68.3 in
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:notableFeature |
improved fuel efficiency
low emissions high reliability |
| gptkbp:primaryUser |
gptkb:Airbus
|
| gptkbp:successor |
gptkb:LEAP-1A
|
| gptkbp:thrust |
22,000 to 33,000 lbf
|
| gptkbp:usedOn |
gptkb:Airbus_A320_family
|
| gptkbp:weight |
4,300 lb
|
| gptkbp:bfsParent |
gptkb:A321-200
gptkb:Airbus_A318 gptkb:CFM56_engine_family |
| gptkbp:bfsLayer |
6
|