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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
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helicopters
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gptkbp:average_temperature
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up to 1,200 ° C
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gptkbp:certification
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certified by Transport Canada
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gptkbp:combustor_type
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annular combustion chamber
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gptkbp:compressor_type
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axial
axial compressor
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gptkbp:configuration
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free turbine
two-shaft
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gptkbp:control_system
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gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
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gptkbp:cooling_system
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air-cooled
air cooling
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gptkbp:design
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modular design
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gptkbp:design_features
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high reliability
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gptkbp:diameter
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0.4 m
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gptkbp:elevation
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up to 20,000 feet
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gptkbp:emissions_standard
|
meets ICAO standards
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gptkbp:engine
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PW206
PW207 D
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gptkbp:engine_configuration
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horizontal configuration
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gptkbp:engine_shutdown_time
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less than 30 seconds
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gptkbp:engine_start_time
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less than 30 seconds
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gptkbp:engine_type
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PW207 E1
PW207 E10
PW207 E2
PW207 E3
PW207 E4
PW207 E5
PW207 E6
PW207 E7
PW207 E8
PW207 E9
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gptkbp:first_flight
|
gptkb:1996
gptkb:2001
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|
gptkbp:fuel_capacity
|
approximately 1.5 meters
approximately 0.5 meters
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gptkbp:fuel_economy
|
high fuel efficiency
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gptkbp:fuel_type
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gptkb:Jet_A-1
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gptkbp:gearbox
|
reduction gearbox
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PW207 E
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gptkbp:is_tested_for
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extensively tested
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gptkbp:launch_window
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starter-generator
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gptkbp:length
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1.2 m
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|
gptkbp:maintenance
|
3,500 hours
|
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gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
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gptkbp:max_speed
|
up to 140 knots
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gptkbp:noise_level
|
low noise emissions
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gptkbp:power_output
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1,800 shp at takeoff
700 shp at 95% RPM
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gptkbp:propulsion
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1,800 shp
700 shp
4.5 shp/lb
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gptkbp:service_entry
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gptkb:2001
|
|
gptkbp:turbine_type
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free power turbine
two-stage gas generator turbine
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gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Agusta_Westland_AW109
gptkb:Agusta_Westland_AW139
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|
gptkbp:weight
|
150 kg
approximately 400 lb
approximately 180 kg
|