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gptkbp:instance_of
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gptkb:engine
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gptkbp:accessories
|
integrated oil system
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gptkbp:application
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gptkb:aircraft
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gptkbp:average_temperature
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up to 1,000 ° C
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gptkbp:certification
|
FAA certified
EASA certified
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gptkbp:competitors
|
competes with Pratt & Whitney Canada P T6
competes with Rolls-Royce M250
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gptkbp:controls
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digital control system
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gptkbp:cooling_system
|
air-cooled
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gptkbp:drivetrain
|
reduction gearbox
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gptkbp:emissions_standard
|
meets ICAO standards
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gptkbp:engine_type
|
free turbine
axial compressor
|
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gptkbp:features
|
modular design
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gptkbp:first_introduced
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gptkb:1977
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gptkbp:fuel_capacity
|
0.5 kg/shp/h
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gptkbp:fuel_type
|
Jet A or Jet A-1
annular combustion chamber
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|
https://www.w3.org/2000/01/rdf-schema#label
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Arriel engine
|
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gptkbp:launch_site
|
electronic starter
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gptkbp:maintenance
|
line maintenance
3,500 hours
|
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gptkbp:manufacturer
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gptkb:Safran_Helicopter_Engines
|
|
gptkbp:market
|
widely available
|
|
gptkbp:market_segment
|
light helicopters
|
|
gptkbp:noise_level
|
low noise emissions
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gptkbp:notable_feature
|
gptkb:dual-channel_FADEC
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gptkbp:notable_users
|
gptkb:helicopter
military forces worldwide
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gptkbp:operational_range
|
-40 to 50 ° C
|
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gptkbp:power_output
|
up to 1,000 shp
|
|
gptkbp:propulsion
|
0.15 kg/shp
|
|
gptkbp:related_model
|
multiple variants
|
|
gptkbp:reliability
|
high reliability
|
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gptkbp:service_ceiling
|
up to 20,000 feet
|
|
gptkbp:services
|
global support network
|
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gptkbp:training
|
pilot training available
|
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gptkbp:type
|
turbo-shaft
|
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gptkbp:used_in
|
Agusta Westland A W109
Eurocopter A S350
Eurocopter E C130
|
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gptkbp:variant
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gptkb:Arriel_1_B
gptkb:Arriel_2_B
gptkb:Arriel_2_M
gptkb:Arriel_2_S
gptkb:Arriel_2_C
gptkb:Arriel_2_D
gptkb:Arriel_2_E
gptkb:Arriel_2_K
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gptkbp:weight
|
approximately 150 kg
|
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gptkbp:bfsParent
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gptkb:Safran_Helicopter_Engines
|
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gptkbp:bfsLayer
|
5
|