Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:combustor_type |
annular combustor
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
36 in
|
| gptkbp:engine |
gptkb:F414-GE-400
|
| gptkbp:engine_configuration |
twin-spool
|
| gptkbp:first_flight |
gptkb:1995
|
| gptkbp:fuel_type |
gptkb:JP-5
|
| https://www.w3.org/2000/01/rdf-schema#label |
F414-GE-400 C
|
| gptkbp:length |
160 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notable_features |
reduced maintenance costs
|
| gptkbp:propulsion |
22,000 lbf
26,000 lbf with afterburner |
| gptkbp:related_aircraft |
gptkb:F/_A-18_Super_Hornet
|
| gptkbp:service_entry |
gptkb:1999
|
| gptkbp:successor |
gptkb:F404_engine
|
| gptkbp:turbine_type |
high-pressure turbine
|
| gptkbp:type |
afterburning turbofan engine
|
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
|
| gptkbp:weight |
3,500 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_F414_engine
|
| gptkbp:bfsLayer |
8
|