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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
low-wing monoplane
two-seat
800 kg empty weight
good performance for aerobatics
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gptkbp:armament
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gptkb:none
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gptkbp:certification
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Type Certificate No. 1-1-1
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gptkbp:cockpit
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tandem seating
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gptkbp:crew
|
2
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gptkbp:design
|
civilian trainer
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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:first_flight
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gptkb:1976
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gptkbp:flaps
|
split flaps
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gptkbp:floors
|
push-pull rods
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gptkbp:fuel_capacity
|
200 L
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gptkbp:height
|
2.60 m
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gptkbp:historical_significance
|
used in many air forces for training purposes
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|
https://www.w3.org/2000/01/rdf-schema#label
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Yak-52 U
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gptkbp:introduced
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gptkb:1976
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gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
|
8.20 m
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gptkbp:manufacturer
|
gptkb:Yakovlev
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gptkbp:max_speed
|
250 km/h
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gptkbp:max_takeoff_weight
|
1,200 kg
+6g to -3g
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gptkbp:notable_features
|
all-metal construction
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gptkbp:number_built
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over 1,000
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gptkbp:origin
|
gptkb:Monarch
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gptkbp:power_output
|
360 hp
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gptkbp:primary_user
|
gptkb:Soviet_Air_Force
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gptkbp:production_years
|
1976-1998
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gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:retired
|
still in service in some countries
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
4.5 seconds per 360 degrees
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:speed
|
80 km/h
docile stall characteristics
|
|
gptkbp:status
|
some still in operation
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:training
|
basic and advanced training
aerobatic training
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|
gptkbp:variant
|
gptkb:Yak-52
|
|
gptkbp:wing_area
|
15.5 m²
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|
gptkbp:wingspan
|
9.80 m
|