Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:helicopter
|
| gptkbp:country_of_origin |
gptkb:France
|
| gptkbp:crew |
2
|
| gptkbp:engine |
Turbomeca Arriel 1
|
| gptkbp:engine_type |
turboshaft
|
| gptkbp:first_flight |
gptkb:1974
gptkb:1975 |
| gptkbp:height |
3.60 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
AS365 N
|
| gptkbp:introduced |
gptkb:1974
|
| gptkbp:length |
13.10 m
13.80 m |
| gptkbp:manufacturer |
gptkb:Airbus
|
| gptkbp:max_speed |
155 knots
150 knots 287 km/h |
| gptkbp:max_takeoff_weight |
3,600 kg
|
| gptkbp:notable_features |
dual-engine design
|
| gptkbp:passenger_capacity |
gptkb:5
|
| gptkbp:primary_user |
various military and civilian operators
|
| gptkbp:production_years |
gptkb:1974
present |
| gptkbp:range |
600 km
850 km |
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:service_ceiling |
5,500 m
|
| gptkbp:successor |
gptkb:AS365_N3
|
| gptkbp:variant |
gptkb:AS365_N2
|
| gptkbp:bfsParent |
gptkb:Eurocopter_AS365_Dauphin
|
| gptkbp:bfsLayer |
6
|