|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional aircraft
|
|
gptkbp:armament
|
gptkb:4
|
|
gptkbp:combustion_system
|
annular combustion chamber
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:configuration
|
free turbine
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
approximately 2.5 ft
|
|
gptkbp:emissions_standard
|
compliant with regulations
|
|
gptkbp:engine
|
starter-generator
|
|
gptkbp:engine_power
|
up to 5,000 hours
|
|
gptkbp:first_flight
|
gptkb:1965
|
|
gptkbp:fuel_control
|
hydromechanical fuel control
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
Jet A or Jet A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Honeywell TPE331
|
|
gptkbp:length
|
approximately 4.5 ft
|
|
gptkbp:maintenance
|
3,600 hours
|
|
gptkbp:manufacturer
|
gptkb:Honeywell
|
|
gptkbp:market_segment
|
regional aviation
|
|
gptkbp:noise_level
|
low noise emissions
|
|
gptkbp:operational_cost
|
low operating costs
|
|
gptkbp:power_output
|
up to 1,000 shp
|
|
gptkbp:propulsion
|
3.3:1
|
|
gptkbp:related_aircraft
|
gptkb:Cessna_208_Caravan
gptkb:Piper_Aerostar
gptkb:De_Havilland_Canada_Dash_8
gptkb:Pilatus_PC-12
gptkb:Beechcraft_1900
gptkb:Embraer_EMB_120_Brasilia
gptkb:Lockheed_Martin_C-130_Hercules
gptkb:Fairchild_Swearingen_Metroliner
gptkb:Air_Tractor_AT-802
gptkb:Dornier_228
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:turbine_type
|
single-stage turbine
|
|
gptkbp:type
|
turbo-prop engine
|
|
gptkbp:variant
|
gptkb:TPE331-12
gptkb:TPE331-14
gptkb:TPE331-20
gptkb:TPE331-5
gptkb:TPE331-10
|
|
gptkbp:weight
|
approximately 300 lb
|
|
gptkbp:bfsParent
|
gptkb:Honeywell's_aerospace_division
|
|
gptkbp:bfsLayer
|
5
|