|
gptkbp:instance_of
|
gptkb:helicopter
|
|
gptkbp:aircraft_type
|
gptkb:helicopter
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:cargo_capacity
|
1,000 kg
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
two-seat tandem
|
|
gptkbp:combat_role
|
gptkb:emergency_services
reconnaissance
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:decommissioned
|
1990s
|
|
gptkbp:design
|
gptkb:Henri_Ziegler
|
|
gptkbp:diameter
|
12.0 m
|
|
gptkbp:engine_power
|
500 shp
|
|
gptkbp:engine_type
|
turboshaft
|
|
gptkbp:first_flight
|
gptkb:1956
|
|
gptkbp:fuel_capacity
|
400 liters
|
|
gptkbp:height
|
3.2 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SA 315 D
|
|
gptkbp:landing_gear
|
skids
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Sud_Aviation
|
|
gptkbp:max_speed
|
220 km/h
|
|
gptkbp:max_takeoff_weight
|
2,500 kg
|
|
gptkbp:military_technology
|
SA 315 B
SA 315 M
|
|
gptkbp:notable_case
|
used in the 1970s conflicts
|
|
gptkbp:notable_features
|
fenestron tail rotor
|
|
gptkbp:notable_operators
|
gptkb:South_African_Air_Force
|
|
gptkbp:number_built
|
over 1,000
|
|
gptkbp:operational_range
|
300 km
|
|
gptkbp:origin
|
gptkb:France
|
|
gptkbp:passenger_capacity
|
gptkb:4
|
|
gptkbp:payload_capacity
|
1,200 kg
|
|
gptkbp:power_source
|
gptkb:Artouste_IIIB
|
|
gptkbp:production_location
|
gptkb:France
|
|
gptkbp:production_years
|
1956-1985
|
|
gptkbp:range
|
600 km
|
|
gptkbp:replaced_by
|
gptkb:Eurocopter_AS350
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:service_history
|
used in various conflicts
|
|
gptkbp:successor
|
gptkb:SA_341_Gazelle
|
|
gptkbp:used_by
|
gptkb:French_Army
|
|
gptkbp:used_in
|
search and rescue missions
|
|
gptkbp:variant
|
gptkb:SA_316_Alouette_III
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:wingspan
|
not applicable
|
|
gptkbp:bfsParent
|
gptkb:Aérospatiale_SA_315_Lama
|
|
gptkbp:bfsLayer
|
8
|