Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:helicopter
|
| gptkbp:armament |
machine guns
|
| gptkbp:climb_rate |
5 m/s
|
| gptkbp:combat_role |
transport and reconnaissance
|
| gptkbp:configuration |
single rotor
|
| gptkbp:crew |
gptkb:1
|
| gptkbp:design_features |
fenestron tail rotor
|
| gptkbp:diameter |
12.0 m
|
| gptkbp:engine_type |
turboshaft
|
| gptkbp:first_flight |
gptkb:1956
|
| gptkbp:height |
3.3 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
SA 315 C
|
| gptkbp:length |
12.5 m
|
| gptkbp:manufacturer |
gptkb:Sud_Aviation
|
| gptkbp:max_speed |
120 knots
|
| gptkbp:max_takeoff_weight |
2,500 kg
|
| gptkbp:notable_users |
gptkb:French_Army
|
| gptkbp:number_built |
over 1,000
|
| gptkbp:passenger_capacity |
gptkb:4
|
| gptkbp:production_years |
1956-1974
|
| gptkbp:range |
400 nautical miles
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:service_ceiling |
4,500 m
|
| gptkbp:successor |
gptkb:SA_341_Gazelle
|
| gptkbp:used_by |
gptkb:military
|
| gptkbp:variant |
SA 316 B
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:Aérospatiale_SA_315_Lama
|
| gptkbp:bfsLayer |
8
|