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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:air_traffic_control
|
manual controls
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gptkbp:aircraft_configuration
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single-engine
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gptkbp:aircraft_operated
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gptkb:light_aircraft
|
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gptkbp:armament
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gptkb:none
|
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gptkbp:climb_rate
|
5 m/s
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|
gptkbp:cockpit
|
tandem seating
|
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gptkbp:cockpit_instruments
|
analog instruments
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gptkbp:country_of_origin
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gptkb:Czechoslovakia
|
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gptkbp:crew
|
2
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gptkbp:design
|
low-wing monoplane
Aero Vodochody design team
|
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gptkbp:engine_power
|
200 hp
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gptkbp:engine_type
|
piston engine
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gptkbp:first_flight
|
gptkb:1956
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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
|
Aero 30
|
|
gptkbp:landing_distance
|
400 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
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gptkbp:length
|
8.2 m
|
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gptkbp:manufacturer
|
gptkb:Aero_Vodochody
|
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gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
1,600 kg
|
|
gptkbp:number_built
|
approximately 200
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gptkbp:number_of_engines
|
gptkb:1
|
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gptkbp:offers_certificate
|
gptkb:Czech_Republic
|
|
gptkbp:operational_history
|
used in military training
|
|
gptkbp:primary_user
|
gptkb:Czechoslovak_Air_Force
|
|
gptkbp:production_years
|
1956-1960
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:range
|
800 km
|
|
gptkbp:related_aircraft
|
Aero 45
Aero 60
|
|
gptkbp:retirement_year
|
gptkb:1970
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:stall_speed
|
70 km/h
|
|
gptkbp:successor
|
Aero 45
|
|
gptkbp:takeoff_distance
|
300 m
|
|
gptkbp:training
|
basic flight training
|
|
gptkbp:variant
|
Aero 30 A
Aero 30 B
Aero 30 C
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:wing_area
|
15 m²
|
|
gptkbp:wingspan
|
10.5 m
|
|
gptkbp:bfsParent
|
gptkb:Aero_320
|
|
gptkbp:bfsLayer
|
7
|