gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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4
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gptkbp:bfsParent
|
gptkb:Czechoslovak_Air_Force
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gptkbp:aircraft_operated
|
conventional control surfaces
Aero 1000
Aero 300
Aero 500
Aero 600
Aero 700
Aero 800
Aero 900
Aero 120
Aero 140
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gptkbp:certification
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gptkb:Monarch
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gptkbp:climb_rate
|
5 m/s
|
gptkbp:cockpit
|
tandem seating
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gptkbp:crew
|
gptkb:musical
|
gptkbp:design
|
advanced trainer
Aero Vodochody design team
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gptkbp:engine_type
|
piston engine
|
gptkbp:first_flight
|
gptkb:1990
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gptkbp:first_released
|
gptkb:1991
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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 1900
|
gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
|
8.2 m
|
gptkbp:manufacturer
|
gptkb:Aero_Vodochody
|
gptkbp:material
|
low-wing monoplane
|
gptkbp:max_speed
|
200 km/h
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
gptkbp:number_built
|
50
|
gptkbp:operational_history
|
used in military training
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gptkbp:power_output
|
100 hp
|
gptkbp:primary_user
|
gptkb:Czech_Air_Force
|
gptkbp:production_years
|
1990-1995
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gptkbp:propulsion
|
two-bladed
|
gptkbp:range
|
1,000 km
|
gptkbp:retirement_year
|
gptkb:2005
|
gptkbp:role
|
gptkb:aircraft
|
gptkbp:roll_rate
|
3.5°/s
|
gptkbp:service_ceiling
|
3,000 m
|
gptkbp:speed
|
70 km/h
|
gptkbp:successor
|
gptkb:Aero_L-39_Albatros
|
gptkbp:variant
|
gptkb:Aero_1900_T
gptkb:Aero_1900_U
Aero 1900 S
|
gptkbp:wingspan
|
9.5 m
|