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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:air_traffic_control
|
conventional controls
|
|
gptkbp:aircraft_configuration
|
single-engine
|
|
gptkbp:aircraft_operated
|
gptkb:light_aircraft
|
|
gptkbp:aircraft_type
|
civilian aircraft
|
|
gptkbp:ceiling
|
4,000 m
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
low-wing monoplane
|
|
gptkbp:engine
|
gptkb:Vedeneyev_M14_P
|
|
gptkbp:first_flight
|
1946
2000s
|
|
gptkbp:fuselage_material
|
monocoque
|
|
gptkbp:has_limitations
|
+6/-3 g
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Yakovlev Yak-18
|
|
gptkbp:introduced
|
1947
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
gptkb:Yakovlev
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:notable_features
|
durable construction
easy maintenance
good handling characteristics
versatile training capabilities
affordable operating costs
|
|
gptkbp:number_built
|
over 1,000
|
|
gptkbp:power_output
|
360 hp
|
|
gptkbp:primary_user
|
gptkb:Soviet_Union
|
|
gptkbp:production_years
|
1946-1970s
|
|
gptkbp:propeller
|
two-bladed
|
|
gptkbp:range
|
800 km
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:roll_rate
|
4.5°/s
|
|
gptkbp:service
|
1950s
|
|
gptkbp:stall_speed
|
70 km/h
|
|
gptkbp:successor
|
gptkb:Yakovlev_Yak-52
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:used_by
|
gptkb:Soviet_Air_Force
gptkb:Aeroflot
various flying clubs
|
|
gptkbp:variant
|
gptkb:Yak-18_A
gptkb:Yak-18_P
gptkb:Yak-18_T
|
|
gptkbp:wing_configuration
|
straight wing
|
|
gptkbp:wingspan
|
10.5 m
|
|
gptkbp:bfsParent
|
gptkb:Shvetsov_ASh-82
gptkb:Soviet_Naval_Aviation
gptkb:Laotian_Air_Force
|
|
gptkbp:bfsLayer
|
6
|