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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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5
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gptkbp:bfsParent
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gptkb:Yak-52
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gptkbp:aircraft_operated
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gptkb:aircraft
250 km/h
1,000 kg
low-wing monoplane
conventional flight controls
8.20 m
trainer and aerobatic aircraft
2.60 m
77 kg/m²
single-engine, tandem seating
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gptkbp:certification
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Type Certificate issued in Russia
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gptkbp:cockpit
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tandem seating
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gptkbp:crew
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2
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gptkbp:date
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gptkb:1976
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gptkbp:design
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aerobatics and training
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gptkbp:engine
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gptkb:Vedeneyev_M14_P
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gptkbp:engine_type
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gptkb:engine
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gptkbp:exported_to
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multiple countries
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gptkbp:features
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robust construction
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gptkbp:financial_performance
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high stability and control
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gptkbp:first_flight
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gptkb:1976
capable of advanced aerobatics
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gptkbp:flaps
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split flaps
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gptkbp:floors
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all-moving tailplane
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gptkbp:fuel_capacity
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200 liters
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gptkbp:height
|
2.60 m
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https://www.w3.org/2000/01/rdf-schema#label
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Yak-52 M
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gptkbp:is_used_by
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various air forces
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gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
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8.20 m
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gptkbp:manufacturer
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gptkb:Yakovlev
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gptkbp:material
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gptkb:NACA_2412
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gptkbp:max_speed
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250 km/h
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gptkbp:max_takeoff_weight
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300 m
400 m
1,200 kg
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gptkbp:military_technology
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used by military flying schools
used in civilian flight schools
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gptkbp:notable_ships
|
large rudder for control
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gptkbp:notable_users
|
Aerobatic teams
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gptkbp:number_built
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over 1,000
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gptkbp:power_output
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360 hp
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gptkbp:production_years
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1976-1998
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gptkbp:propulsion
|
4-blade propeller
0.3 hp/kg
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gptkbp:range
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1,000 km
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gptkbp:role
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gptkb:aircraft
|
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gptkbp:roll_rate
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4.5 seconds per 360 degrees
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gptkbp:service_ceiling
|
3,000 m
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gptkbp:speed
|
80 km/h
gentle stall characteristics
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gptkbp:surface
|
full-span ailerons
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gptkbp:training
|
primary flight training
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gptkbp:variant
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gptkb:Yak-52
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gptkbp:wing_area
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15.5 m²
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gptkbp:wingspan
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9.80 m
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