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gptkbp:instance_of
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gptkb:helicopter
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|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modern glass cockpit
|
|
gptkbp:cargo_capacity
|
1,000 kg
|
|
gptkbp:certification
|
FAA and EASA
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|
gptkbp:crew
|
2
|
|
gptkbp:design
|
twin-engine design
MBB and Kawasaki
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|
gptkbp:diameter
|
gptkb:Fenestron
11.0 m
|
|
gptkbp:emergency_services
|
yes
|
|
gptkbp:engine_type
|
twin-turbine
|
|
gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:fuel_capacity
|
600 liters
|
|
gptkbp:fuselage_material
|
aluminum alloy
|
|
gptkbp:height
|
3.8 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
BK117 A-1
|
|
gptkbp:landing_gear
|
skid
|
|
gptkbp:length
|
13.3 m
|
|
gptkbp:maintenance
|
easy access to components
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:market
|
global
|
|
gptkbp:market_segment
|
commercial and private
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
3,200 kg
|
|
gptkbp:military_technology
|
yes
limited
|
|
gptkbp:modifications
|
various configurations available
|
|
gptkbp:notable_case
|
none reported
|
|
gptkbp:notable_features
|
dual-use for civilian and military purposes
|
|
gptkbp:operational_range
|
300 km
|
|
gptkbp:operational_use
|
gptkb:search_and_rescue
|
|
gptkbp:passenger_capacity
|
gptkb:10
|
|
gptkbp:performance
|
highly versatile
|
|
gptkbp:power_source
|
2 x Turbomeca Arriel 1 B
|
|
gptkbp:primary_user
|
air ambulance services
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:production_location
|
Germany and Japan
|
|
gptkbp:production_years
|
1980-2000
|
|
gptkbp:range
|
600 km
|
|
gptkbp:related_model
|
gptkb:BK117_C-1
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:safety_record
|
generally good
|
|
gptkbp:service_ceiling
|
5,000 m
|
|
gptkbp:successor
|
gptkb:BK117_D-2
|
|
gptkbp:training
|
available for pilots
|
|
gptkbp:variant
|
BK117
|
|
gptkbp:weight
|
2,800 kg
|
|
gptkbp:wingspan
|
not applicable
|
|
gptkbp:year_established
|
gptkb:1982
|
|
gptkbp:bfsParent
|
gptkb:Kawasaki_BK117
|
|
gptkbp:bfsLayer
|
7
|