|
gptkbp:instance_of
|
gptkb:helicopter
|
|
gptkbp:avionics
|
digital
|
|
gptkbp:climb_rate
|
8.5 m/s
|
|
gptkbp:country_of_origin
|
gptkb:France
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:cruise_speed
|
120 knots
|
|
gptkbp:design
|
single-engine
|
|
gptkbp:diameter
|
gptkb:4
gptkb:5
10.69 m
|
|
gptkbp:elevation
|
5,000 m
|
|
gptkbp:engine_power
|
500 shp
|
|
gptkbp:engine_type
|
gptkb:Arriel_2_B1
turboshaft
|
|
gptkbp:first_flight
|
gptkb:1992
|
|
gptkbp:fuel_capacity
|
500 liters
|
|
gptkbp:height
|
3.3 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Airbus H125
|
|
gptkbp:landing_gear
|
skids
|
|
gptkbp:length
|
12.8 m
|
|
gptkbp:manufacturer
|
gptkb:Airbus
|
|
gptkbp:market_segment
|
gptkb:civil_aviation
|
|
gptkbp:max_speed
|
130 knots
|
|
gptkbp:max_takeoff_weight
|
2,250 kg
|
|
gptkbp:notable_users
|
gptkb:emergency_services
gptkb:military_forces
Tour operators
Police forces
Private owners
|
|
gptkbp:offers_certificate
|
gptkb:EASA
|
|
gptkbp:passenger_capacity
|
6 passengers
|
|
gptkbp:payload_capacity
|
1,050 kg
|
|
gptkbp:production_status
|
in production
|
|
gptkbp:production_years
|
gptkb:1992
|
|
gptkbp:range
|
600 km
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:safety_features
|
advanced avionics
dual hydraulic system
emergency flotation system
automatic flight control system
crash-resistant fuel system
|
|
gptkbp:service_ceiling
|
5,000 m
|
|
gptkbp:type
|
light helicopter
|
|
gptkbp:variant
|
H120
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:weight_limit
|
2,250 kg
|
|
gptkbp:year_established
|
gptkb:1992
|
|
gptkbp:bfsParent
|
gptkb:Royal_Air_Force_of_Oman
gptkb:Jordanian_Air_Force
gptkb:Bell_407
gptkb:Bell_505_Jet_Ranger_X
gptkb:Bell_407_GXi
|
|
gptkbp:bfsLayer
|
5
|