gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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7
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gptkbp:bfsParent
|
gptkb:Mikulin
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:item
retired
single-engine
straight wing
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gptkbp:allows
|
+6/-3 g
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gptkbp:climb_rate
|
5 m/s
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gptkbp:cockpit
|
open cockpit
side-by-side seating
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gptkbp:crew
|
2
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gptkbp:design
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gptkb:Yakovlev_design_bureau
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gptkbp:engine
|
Vedeneyev M-14 P
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gptkbp:features
|
simple construction
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gptkbp:first_flight
|
gptkb:1955
gptkb:battle
1955-07-01
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gptkbp:flaps
|
manual flaps
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gptkbp:fuel_capacity
|
200 L
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gptkbp:height
|
2.5 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Yakovlev Yak-56
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gptkbp:instrumentation
|
basic flight instruments
|
gptkbp:landing_gear
|
tricycle gear
retractable landing gear
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gptkbp:length
|
8.5 m
|
gptkbp:manufacturer
|
gptkb:Yakovlev
|
gptkbp:material
|
gptkb:item
|
gptkbp:max_speed
|
250 km/h
|
gptkbp:max_takeoff_weight
|
300 m
1,200 kg
250 m
|
gptkbp:notable_users
|
gptkb:Aeroflot
|
gptkbp:number_built
|
approximately 200
|
gptkbp:operational_history
|
used for pilot training
|
gptkbp:power_output
|
1 × Vedeneyev M-14 P engine
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gptkbp:primary_user
|
gptkb:Monarch
|
gptkbp:production_location
|
gptkb:Monarch
|
gptkbp:production_years
|
1955-1960
|
gptkbp:propulsion
|
2-bladed propeller
|
gptkbp:range
|
800 km
|
gptkbp:retirement_year
|
1970s
|
gptkbp:role
|
gptkb:aircraft
aerobatic training
civilian training aircraft
|
gptkbp:roll_rate
|
360°/s
|
gptkbp:seating_capacity
|
400 kg
|
gptkbp:services
|
gptkb:Soviet_Air_Force
gptkb:1956
|
gptkbp:setting
|
low-wing monoplane
|
gptkbp:speed
|
70 km/h
|
gptkbp:successor
|
gptkb:Yak-52
|
gptkbp:surface
|
elevator, ailerons, rudder
|
gptkbp:tail_type
|
conventional tail
|
gptkbp:training
|
basic flight training
|
gptkbp:variant
|
Yak-56 A
|
gptkbp:weight
|
800 kg
|
gptkbp:wing_area
|
15 m²
|
gptkbp:wingspan
|
10.5 m
|