Honeywell TFE731-2-2 B

GPTKB entity

Statements (51)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application gptkb:business_jet
gptkbp:average_temperature -40 to 50 ° C
gptkbp:certification Stage 3
gptkbp:compressor_type axial-flow
gptkbp:control_system gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:cooling_system air-cooled
gptkbp:diameter 2.5 ft
gptkbp:engine gptkb:TFE731
Brayton cycle
gptkbp:engine_configuration twin-spool
gptkbp:first_flight gptkb:1972
gptkbp:fuel_economy 0.8 lb/hp/hr
gptkbp:fuel_type gptkb:Jet_A
https://www.w3.org/2000/01/rdf-schema#label Honeywell TFE731-2-2 B
gptkbp:ignition_system gptkb:spark_plug
gptkbp:length 4.5 ft
gptkbp:maintenance 3,500 hours
gptkbp:manufacturer gptkb:Honeywell
gptkbp:noise_level Stage 3
gptkbp:number_of_stages gptkb:10
gptkbp:power_output 3,500 hp
gptkbp:propulsion 3,500 lbf
gptkbp:related_aircraft gptkb:Cessna_Citation_III
gptkb:Cessna_Citation_Longitude
gptkb:Cessna_Citation_Encore
gptkb:Cessna_Citation_Encore+
gptkb:Cessna_Citation_Ultra
gptkb:Cessna_Citation_VI
gptkb:Cessna_Citation_VII
gptkb:Gulfstream_G150
gptkb:Cessna_Citation_CJ4
gptkb:Cessna_Citation_M2
gptkb:Hawker_800
gptkb:Cessna_Citation_Latitude
gptkb:Cessna_Citation_CJ1
gptkb:Cessna_Citation_X+
gptkb:Cessna_Citation_CJ3
gptkb:Bombardier_Learjet_60
gptkb:Cessna_Citation_X
gptkb:Dassault_Falcon_50
gptkb:Gulfstream_G280
gptkb:Gulfstream_G100
gptkb:Cessna_Citation_CJ2
gptkb:Cessna_Citation_Sovereign
gptkb:Gulfstream_G200
gptkbp:turbine_type single-shaft
gptkbp:water_requirement 1,000 lb/hr
gptkbp:weight 1,200 lb
gptkbp:bfsParent gptkb:L-159_Alca
gptkbp:bfsLayer 6