gptkbp:instance_of
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gptkb:helicopter
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gptkbp:armament
|
machine guns
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gptkbp:cargo_capacity
|
5,000 lb
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gptkbp:configuration
|
twin-engine
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gptkbp:control_system
|
fly-by-wire
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gptkbp:country_of_origin
|
gptkb:United_States
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gptkbp:crew
|
2
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gptkbp:customer_support
|
extensive support network
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gptkbp:design
|
modular design
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gptkbp:diameter
|
gptkb:Fenestron
14.63 m
two-bladed
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gptkbp:engine
|
PT6 T-3 B
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gptkbp:engine_type
|
turboshaft
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gptkbp:first_flight
|
gptkb:1980
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gptkbp:fuel_capacity
|
1,200 lb
|
gptkbp:global_presence
|
used worldwide
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gptkbp:height
|
4.57 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bell 412 S
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gptkbp:introduced
|
gptkb:1981
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gptkbp:landing_gear
|
skid type
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gptkbp:length
|
16.61 m
|
gptkbp:maintenance
|
easy access to components
|
gptkbp:manufacturer
|
gptkb:Bell_Helicopter
|
gptkbp:market
|
commercial and military
|
gptkbp:market_segment
|
civil and military aviation
|
gptkbp:max_speed
|
130 knots
|
gptkbp:max_takeoff_weight
|
10,500 lb
|
gptkbp:military_technology
|
gptkb:emergency_services
transport and reconnaissance
|
gptkbp:modifications
|
gptkb:search_and_rescue
|
gptkbp:notable_features
|
advanced avionics
|
gptkbp:number_of_engines
|
2
|
gptkbp:operational_cost
|
moderate
|
gptkbp:operational_range
|
1,000 km
|
gptkbp:passenger_capacity
|
gptkb:13
|
gptkbp:performance
|
high maneuverability
|
gptkbp:power_source
|
twin-turbine engine
|
gptkbp:primary_user
|
gptkb:military
|
gptkbp:production_years
|
gptkb:1981
present
|
gptkbp:range
|
600 nautical miles
|
gptkbp:related_model
|
gptkb:Bell_407
|
gptkbp:role
|
gptkb:helicopter
|
gptkbp:safety_features
|
crashworthy design
|
gptkbp:service_ceiling
|
20,000 ft
|
gptkbp:service_history
|
used in various conflicts
|
gptkbp:successor
|
gptkb:Bell_429
|
gptkbp:training
|
pilot training available
|
gptkbp:type
|
multi-role helicopter
|
gptkbp:upgrades
|
modern avionics systems
|
gptkbp:variant
|
gptkb:Bell_412_EP
gptkb:Bell_412
|
gptkbp:weight
|
5,400 lb
|
gptkbp:bfsParent
|
gptkb:Bell_412
|
gptkbp:bfsLayer
|
5
|