| gptkbp:instanceOf | gptkb:piston_engine 
 | 
                        
                            
                                | gptkbp:application | business jets 
 | 
                        
                            
                                | gptkbp:bypassRatio | high bypass 
 | 
                        
                            
                                | gptkbp:certification | 1972 
 | 
                        
                            
                                | gptkbp:countryOfOrigin | gptkb:United_States 
 | 
                        
                            
                                | gptkbp:developedBy | gptkb:Garrett_AiResearch 
 | 
                        
                            
                                | gptkbp:diameter | approximately 23 inches 
 | 
                        
                            
                                | gptkbp:family | Honeywell TFE family 
 | 
                        
                            
                                | gptkbp:firstRun | 1970 
 | 
                        
                            
                                | gptkbp:flightHours | over 100 million 
 | 
                        
                            
                                | gptkbp:fuelType | gptkb:Jet-A 
 | 
                        
                            
                                | gptkbp:hasConcept | axial-centrifugal 
 | 
                        
                            
                                | gptkbp:length | approximately 60 inches 
 | 
                        
                            
                                | gptkbp:manufacturer | gptkb:Honeywell_Aerospace 
 | 
                        
                            
                                | gptkbp:market | business aviation 
 | 
                        
                            
                                | gptkbp:notableFeature | modular design quiet operation
 low emissions
 
 | 
                        
                            
                                | gptkbp:numberBuilt | over 11,000 
 | 
                        
                            
                                | gptkbp:numberOfStages | two two axial, one centrifugal
 
 | 
                        
                            
                                | gptkbp:successor | HTF7000 
 | 
                        
                            
                                | gptkbp:thrust | 3,500 to 5,000 lbf 
 | 
                        
                            
                                | gptkbp:type | turbofan 
 | 
                        
                            
                                | gptkbp:usedInAircraft | gptkb:Dassault_Falcon_20 gptkb:Dassault_Falcon_10
 gptkb:Dassault_Falcon_50
 gptkb:Learjet_31
 gptkb:Learjet_35
 gptkb:Learjet_36
 gptkb:Learjet_55
 gptkb:Learjet_60
 gptkb:IAI_Astra
 gptkb:Cessna_Citation_III
 gptkb:Cessna_Citation_VI
 gptkb:Cessna_Citation_VII
 gptkb:IAI_Westwind
 
 | 
                        
                            
                                | gptkbp:weight | approximately 900 lbs 
 | 
                        
                            
                                | gptkbp:bfsParent | gptkb:Garrett_TFE731 
 | 
                        
                            
                                | gptkbp:bfsLayer | 7 
 | 
                        
                            
                                | https://www.w3.org/2000/01/rdf-schema#label | TFE731 
 |