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gptkbp:instance_of
|
gptkb:helicopter
|
|
gptkbp:air_traffic_control
|
cyclic and collective controls
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
basic avionics suite
|
|
gptkbp:certification
|
EASA certified
NATO certified
|
|
gptkbp:cockpit
|
two-seat cockpit
|
|
gptkbp:country_of_origin
|
gptkb:Romania
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:design
|
gptkb:IAR_S._A.
|
|
gptkbp:diameter
|
11.0 m
fenestron tail rotor
|
|
gptkbp:engine
|
gptkb:Turbomeca_Astazou
|
|
gptkbp:first_flight
|
gptkb:1975
|
|
gptkbp:fuel_capacity
|
400 liters
|
|
gptkbp:fuselage_material
|
metal and composite materials
|
|
gptkbp:height
|
3.5 m
|
|
gptkbp:historical_significance
|
first Romanian helicopter design.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
IAR 316 B1
|
|
gptkbp:landing_gear
|
skid landing gear
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:maintenance
|
relatively easy to maintain
|
|
gptkbp:manufacturer
|
gptkb:IAR_S._A.
|
|
gptkbp:market
|
primarily Eastern Europe
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:navigation_system
|
gptkb:radio_station
|
|
gptkbp:number_built
|
over 100
|
|
gptkbp:operational_history
|
used in various missions
|
|
gptkbp:passenger_capacity
|
gptkb:5
|
|
gptkbp:performance
|
good maneuverability
|
|
gptkbp:produces
|
1975-1990
|
|
gptkbp:production_location
|
gptkb:Romania
|
|
gptkbp:propulsion
|
gptkb:turbofan_engine
|
|
gptkbp:range
|
600 km
|
|
gptkbp:related_aircraft
|
gptkb:SA_316_Alouette_III
gptkb:IAR_330
SA 319 Alouette II
|
|
gptkbp:retirement_year
|
2000s
|
|
gptkbp:role
|
gptkb:transportation
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:IAR_330
|
|
gptkbp:type
|
gptkb:helicopter
|
|
gptkbp:used_by
|
gptkb:Romanian_Police
gptkb:Romanian_Air_Force
civil operators
|
|
gptkbp:variant
|
IAR 316 B1-1
IAR 316 B1-2
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:weight_limit
|
2,500 kg
|
|
gptkbp:bfsParent
|
gptkb:IAR_316_B
|
|
gptkbp:bfsLayer
|
7
|