|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:configuration
|
free turbine
|
|
gptkbp:control_system
|
electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
22 in
|
|
gptkbp:emissions_standard
|
EPA Tier 4
|
|
gptkbp:engine
|
modular design
Brayton cycle
regional aircraft
developed from TPE331-1
|
|
gptkbp:engine_configuration
|
pylon-mounted
twin-shaft
detailed specifications available.
|
|
gptkbp:engine_power
|
high reliability
|
|
gptkbp:engine_type
|
gptkb:TPE331-10
turboprop
|
|
gptkbp:first_flight
|
gptkb:1965
|
|
gptkbp:fuel_capacity
|
dry sump
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
hydromechanical
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TPE331-12
|
|
gptkbp:ignition_system
|
dual spark
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:launch_platform
|
electric starter
|
|
gptkbp:length
|
42 in
|
|
gptkbp:maintenance
|
2000 hours
|
|
gptkbp:manufacturer
|
gptkb:Honeywell
|
|
gptkbp:max_speed
|
40,000 rpm
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:power_output
|
1000 shp
|
|
gptkbp:propeller
|
constant speed
|
|
gptkbp:propulsion
|
3.33
1000 lbf
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:torque
|
splash lubrication
|
|
gptkbp:turbine_type
|
single stage
|
|
gptkbp:weight
|
300 lb
|
|
gptkbp:bfsParent
|
gptkb:Honeywell_TPE331
gptkb:TPE331_family
|
|
gptkbp:bfsLayer
|
6
|