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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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5
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gptkbp:bfsParent
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gptkb:Zlin_Z-142
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gptkbp:aircraft_operated
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general aviation
varies by country
800 kg
single-engine
civil aircraft
conventional layout
varied by model and configuration
64 kg/m²
stable and forgiving handling
Z-142, Z-143
developed in Czechoslovakia.
flight training, aerobatics
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gptkbp:cockpit
|
dual control
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|
gptkbp:crew
|
1 pilot
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|
gptkbp:design
|
Zlin Aircraft design team
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gptkbp:engine
|
180 hp
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gptkbp:engine_type
|
piston engine
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|
gptkbp:first_flight
|
gptkb:1970
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|
gptkbp:flaps
|
split flaps
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|
gptkbp:fuel_capacity
|
120 liters
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|
gptkbp:height
|
2.40 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Zlin Z-142 Trainer
|
|
gptkbp:introduced
|
gptkb:1970
|
|
gptkbp:involved_units
|
over 200
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|
gptkbp:is_used_by
|
various flying schools
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.20 m
|
|
gptkbp:manufacturer
|
gptkb:Zlin_Aircraft
|
|
gptkbp:market
|
Europe, Asia
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:notable_features
|
good visibility
|
|
gptkbp:operational_history
|
used in military and civilian training
|
|
gptkbp:production_years
|
1970-1990
|
|
gptkbp:propulsion
|
variable-pitch propeller
0.225 hp/kg
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
1 student
|
|
gptkbp:service_ceiling
|
4,000 m
|
|
gptkbp:setting
|
low-wing monoplane
|
|
gptkbp:speed
|
160 km/h
65 km/h
|
|
gptkbp:successor
|
gptkb:Zlin_Z-143
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
basic flight training
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:wing_area
|
12.5 m²
|
|
gptkbp:wingspan
|
9.80 m
|