gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
|
7
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gptkbp:bfsParent
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gptkb:Zlin_Aviation
gptkb:Zlin_Z-37
gptkb:Zlin_Z-42
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gptkbp:aircraft_operated
|
general aviation
1,200 kg
single-engine aircraft
utility aircraft
low wing
conventional controls
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gptkbp:certification
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gptkb:EASA
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gptkbp:climb_rate
|
5 m/s
|
gptkbp:cockpit
|
tandem seating
|
gptkbp:controls
|
yoke
|
gptkbp:crew
|
gptkb:musical
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gptkbp:date
|
gptkb:1968
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gptkbp:design
|
gptkb:aircraft
Zlin Aircraft design team
|
gptkbp:engine
|
gptkb:Lycoming_IO-360
180 hp
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gptkbp:engine_type
|
piston engine
|
gptkbp:features
|
low drag design
|
gptkbp:financial_performance
|
high stability
|
gptkbp:first_flight
|
gptkb:1968
|
gptkbp:flaps
|
split flaps
|
gptkbp:fuel_capacity
|
120 L
|
gptkbp:height
|
2.5 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Zlin Z-43
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
8.1 m
|
gptkbp:manufacturer
|
gptkb:Zlin_Aircraft
|
gptkbp:market_segment
|
private pilots
|
gptkbp:marketed_as
|
gptkb:Zlin_Z-43_Trainer
|
gptkbp:material
|
gptkb:item
|
gptkbp:max_speed
|
200 km/h
|
gptkbp:max_takeoff_weight
|
300 m
400 m
1,600 kg
|
gptkbp:notable_users
|
gptkb:Czech_Air_Force
|
gptkbp:number_built
|
over 200
|
gptkbp:operational_history
|
used in flight training
|
gptkbp:origin
|
gptkb:Monarch
|
gptkbp:performance
|
good performance
|
gptkbp:production_location
|
gptkb:Monarch
|
gptkbp:production_years
|
gptkb:1980
1968-1980
|
gptkbp:propulsion
|
constant speed propeller
propeller-driven
|
gptkbp:range
|
800 km
|
gptkbp:roll_rate
|
3°/s
|
gptkbp:safety_features
|
crashworthy design
|
gptkbp:seating_capacity
|
gptkb:3
400 kg
|
gptkbp:service_ceiling
|
3,000 m
|
gptkbp:speed
|
65 km/h
180 km/h
|
gptkbp:squadrons
|
various colors
|
gptkbp:supports
|
certified
|
gptkbp:tail_type
|
T-tail
|
gptkbp:training
|
basic flight training
|
gptkbp:type
|
gptkb:aircraft
|
gptkbp:variant
|
gptkb:Zlin_Z-42
|
gptkbp:wing_area
|
14.5 m²
|
gptkbp:wingspan
|
10.5 m
|