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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
|
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gptkbp:bfsParent
|
gptkb:Yakovlev_Yak-14
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Antonov_An-2
utility transport
cantilever wing
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:cockpit
|
pressurized cockpit
|
|
gptkbp:communication
|
gptkb:radio_station
|
|
gptkbp:crew
|
2
|
|
gptkbp:decommissioned
|
gptkb:1980s
|
|
gptkbp:design
|
gptkb:Yakovlev_Design_Bureau
low-wing monoplane
|
|
gptkbp:emergency_services
|
overwing exits
|
|
gptkbp:engine
|
2
2 x 1200 hp
|
|
gptkbp:engine_type
|
twin-engine
|
|
gptkbp:first_flight
|
gptkb:1952
|
|
gptkbp:fuel_capacity
|
3000 L
|
|
gptkbp:height
|
7.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Yak-14 B
|
|
gptkbp:influenced_by
|
Yak-12
|
|
gptkbp:interior_features
|
passenger seating and cargo area
|
|
gptkbp:introduced
|
gptkb:1954
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
22.5 m
|
|
gptkbp:manufacturer
|
gptkb:Yakovlev
|
|
gptkbp:material
|
metal fuselage
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
500 m
600 m
12000 kg
|
|
gptkbp:navigation_system
|
radio navigation
|
|
gptkbp:notable_features
|
large cargo door
|
|
gptkbp:operational_area
|
military and civilian missions
|
|
gptkbp:operational_history
|
used in various roles
|
|
gptkbp:operational_range
|
2000 km
|
|
gptkbp:primary_user
|
gptkb:Soviet_Air_Force
|
|
gptkbp:produced_by
|
50
|
|
gptkbp:production_years
|
1952-1954
|
|
gptkbp:propulsion
|
variable-pitch propellers
|
|
gptkbp:range
|
2000 km
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
gptkb:television_series
4000 kg
|
|
gptkbp:service_ceiling
|
8000 m
|
|
gptkbp:speed
|
100 km/h
|
|
gptkbp:successor
|
gptkb:Yak-40
|
|
gptkbp:surface
|
elevators and ailerons
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:used_in
|
gptkb:aircraft
|
|
gptkbp:variant
|
Yak-14
|
|
gptkbp:weight
|
7000 kg
|
|
gptkbp:wing_area
|
80 m²
|
|
gptkbp:wingspan
|
25.0 m
|