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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
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gptkbp:bfsParent
|
gptkb:Mikulin
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:historical_event
gptkb:Yakovlev_Yak-40
high performance
lightweight
commercial aviation
domestic flights
twin-engine
high-wing
conventional design
Yakovlev family
commercial specifications
|
|
gptkbp:airlines
|
gptkb:Aeroflot
|
|
gptkbp:avionics
|
analog instruments
|
|
gptkbp:capacity
|
up to 200 passengers
|
|
gptkbp:crew
|
gptkb:3
2 pilots
|
|
gptkbp:date
|
1970s
|
|
gptkbp:design
|
gptkb:patent
gptkb:Yakovlev_Design_Bureau
regional transport
|
|
gptkbp:emergency_services
|
overwing exits
|
|
gptkbp:engine
|
Kuznetsov NK-8
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_flight
|
gptkb:1976
1990s
two-pilot cockpit
|
|
gptkbp:fuel_capacity
|
30,000 L
|
|
gptkbp:height
|
12.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Yakovlev Yak-86
|
|
gptkbp:introduced
|
gptkb:1976
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
46.5 m
|
|
gptkbp:manufacturer
|
gptkb:Yakovlev
|
|
gptkbp:max_speed
|
950 km/h
|
|
gptkbp:max_takeoff_weight
|
100,000 kg
|
|
gptkbp:notable_features
|
wide fuselage
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_history
|
gptkb:Monarch
|
|
gptkbp:production_location
|
gptkb:Monarch
|
|
gptkbp:production_years
|
1976-1982
|
|
gptkbp:range
|
5,000 km
long-range
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
10,000 kg
single-class layout
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:services
|
gptkb:1976
|
|
gptkbp:speed
|
850 km/h
|
|
gptkbp:successor
|
gptkb:Yakovlev_Yak-42
|
|
gptkbp:type
|
narrow-body aircraft
|
|
gptkbp:variant
|
Yakovlev Yak-86 D
|
|
gptkbp:wingspan
|
44.0 m
|