|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
-40 to 50 ° C
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:configuration
|
free turbine
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
22 in
|
|
gptkbp:emissions_standard
|
EPA Tier 4
|
|
gptkbp:engine
|
gptkb:transport_aircraft
gptkb:aircraft
gptkb:military_aircraft
gptkb:trainer_aircraft
gptkb:business_jet
gptkb:drones
helicopters
utility aircraft
cargo planes
civil aircraft
light transport aircraft
firefighting aircraft
aerial survey aircraft
regional airliners
executive jets
search and rescue aircraft
special mission aircraft
|
|
gptkbp:engine_configuration
|
twin-engine
pylon mounted
|
|
gptkbp:engine_power
|
5000 hours
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
gptkb:TPE331-10
|
|
gptkbp:first_flight
|
gptkb:1965
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
dual fuel system
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TPE331-14
|
|
gptkbp:ignition_system
|
dual spark
|
|
gptkbp:is_tested_for
|
bench tested
|
|
gptkbp:launch_platform
|
electric starter
|
|
gptkbp:length
|
48 in
|
|
gptkbp:maintenance
|
1000 hours
|
|
gptkbp:manufacturer
|
gptkb:Honeywell
|
|
gptkbp:max_continuous_power
|
950 shp
|
|
gptkbp:max_intermittent_power
|
1200 shp
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:power_output
|
1000 shp
|
|
gptkbp:propeller
|
variable pitch
|
|
gptkbp:propulsion
|
2.5:1
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:turbine_type
|
single stage
|
|
gptkbp:warranty
|
5 years
|
|
gptkbp:weight
|
400 lb
|
|
gptkbp:bfsParent
|
gptkb:Honeywell_TPE331
gptkb:TPE331_family
|
|
gptkbp:bfsLayer
|
6
|