|
gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Zlin_Z-42
|
|
gptkbp:aircraft_operated
|
general aviation
single-engine
|
|
gptkbp:aspect_ratio
|
7.2
|
|
gptkbp:certification
|
gptkb:Monarch
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
two-seat tandem
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:design
|
Zlin Aircraft design team
|
|
gptkbp:engine
|
gptkb:Avia_M137
|
|
gptkbp:first_flight
|
gptkb:1968
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
200 liters
|
|
gptkbp:height
|
2.4 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Zlin Z-42 trainer
|
|
gptkbp:introduced
|
gptkb:1970
|
|
gptkbp:is_used_by
|
gptkb:Czech_Air_Force
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
gptkb:Zlin_Aircraft
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:notable_features
|
good visibility
|
|
gptkbp:number_built
|
over 200
|
|
gptkbp:operational_history
|
used in training and aerobatics.
|
|
gptkbp:powers
|
180 hp
|
|
gptkbp:primary_user
|
flight schools
|
|
gptkbp:production_years
|
1968-1980
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
3.5°/s
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:successor
|
gptkb:Zlin_Z-43
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:trademark
|
gptkb:Zlin
|
|
gptkbp:type
|
low-wing monoplane
|
|
gptkbp:variant
|
gptkb:Zlin_Z-42_M
|
|
gptkbp:wing_area
|
14.5 m²
|
|
gptkbp:wingspan
|
10.5 m
|