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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Letov_Š-328_A
gptkb:Zlin_Aircraft
gptkb:Zlin_Aircraft_Company
|
|
gptkbp:aircraft_operated
|
gptkb:Zlin_Z-43
gptkb:Zlin_Z-50
high-wing
|
|
gptkbp:capacity
|
2
|
|
gptkbp:cockpit
|
two-seat tandem
|
|
gptkbp:controls
|
conventional control surfaces
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
gptkb:Zlin_Aircraft_Company
|
|
gptkbp:engine
|
gptkb:Avia_M137
|
|
gptkbp:first_flight
|
gptkb:1968
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
120 liters
|
|
gptkbp:height
|
2.40 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Zlin Z-42
|
|
gptkbp:is_used_by
|
various flying schools
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.20 m
|
|
gptkbp:manufacturer
|
gptkb:Zlin_Aircraft
|
|
gptkbp:marketed_as
|
gptkb:Zlin_Z-42_trainer
|
|
gptkbp:material
|
gptkb:NACA_2412
monocoque construction
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
400 m
1,200 kg
|
|
gptkbp:notable_features
|
durable construction
easy handling
low operating costs
good visibility
good climb rate
stable flight characteristics
low stall speed
|
|
gptkbp:number_built
|
over 200
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:power_output
|
140 hp
|
|
gptkbp:production_years
|
1968-1980
|
|
gptkbp:propulsion
|
two-bladed
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:service_ceiling
|
4,000 m
|
|
gptkbp:speed
|
65 km/h
|
|
gptkbp:tail_type
|
T-tail configuration
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:variant
|
Z-42 C
Z-42 L
Z-42 M
|
|
gptkbp:wing_area
|
14.5 m²
|
|
gptkbp:wingspan
|
10.80 m
|