|
gptkbp:instance_of
|
gptkb:helicopter
|
|
gptkbp:capacity
|
gptkb:6
up to 6 passengers
|
|
gptkbp:configuration
|
single rotor
|
|
gptkbp:country_of_origin
|
gptkb:France
|
|
gptkbp:crew
|
gptkb:1
1 pilot
|
|
gptkbp:design
|
gptkb:Aerospatiale
|
|
gptkbp:diameter
|
11.0 m
2.69 m
|
|
gptkbp:engine
|
gptkb:Turmo_IV_A
Turbin Engine
|
|
gptkbp:first_flight
|
gptkb:1974
gptkb:1980
|
|
gptkbp:fuel_capacity
|
500 liters
500 L
|
|
gptkbp:height
|
3.6 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
AS350 BA
|
|
gptkbp:introduced
|
gptkb:1980
|
|
gptkbp:length
|
12.8 m
|
|
gptkbp:manufacturer
|
gptkb:Airbus
|
|
gptkbp:market
|
commercial aviation
|
|
gptkbp:max_speed
|
260 km/h
|
|
gptkbp:max_takeoff_weight
|
2,250 kg
|
|
gptkbp:notable_features
|
high maneuverability
Fenestron tail rotor
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:powers
|
1,000 hp
847 hp
|
|
gptkbp:primary_use
|
air transport
|
|
gptkbp:primary_user
|
Various military and civilian operators
|
|
gptkbp:production_years
|
1974-present
1980-2000
|
|
gptkbp:range
|
600 km
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:service_ceiling
|
5,500 m
|
|
gptkbp:successor
|
gptkb:AS350_B3
|
|
gptkbp:type
|
single-engine helicopter
|
|
gptkbp:used_by
|
various military and civilian operators
|
|
gptkbp:variant
|
gptkb:AS350_B3e_H
gptkb:AS350_B3e_S
gptkb:AS350_B3e_T
gptkb:AS350_B3e_T2
gptkb:AS350_B3e_T3
gptkb:AS350_B3e_T4
gptkb:AS350_B3e_T5
gptkb:AS350_B3e_T6
gptkb:AS350_B3e_T7
gptkb:AS350_B3e_T8
gptkb:AS350_BA_Ecureuil
gptkb:AS350_B2
gptkb:AS350_Ecureuil
gptkb:AS350_B
gptkb:AS350_B3e
gptkb:AS350_B3
AS350
AS350 B3e T10
AS350 B3e T11
AS350 B3e T12
AS350 B3e T13
AS350 B3e T14
AS350 B3e T15
AS350 B3e T16
AS350 B3e T17
AS350 B3e T18
AS350 B3e T19
AS350 B3e T20
AS350 B3e T9
|
|
gptkbp:weight
|
1,500 kg
1,800 kg
|
|
gptkbp:wingspan
|
gptkb:N/_A
not applicable
|
|
gptkbp:bfsParent
|
gptkb:Eurocopter_AS350
gptkb:AS350_Écureuil
|
|
gptkbp:bfsLayer
|
6
|