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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
9
|
|
gptkbp:bfsParent
|
gptkb:Aero_L-60
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:controls
|
conventional control surfaces
|
|
gptkbp:crew
|
1-2
|
|
gptkbp:design
|
gptkb:Aero_Vodochody
low-wing monoplane
|
|
gptkbp:engine
|
200 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:financial_performance
|
good stability characteristics
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
300 L
|
|
gptkbp:height
|
2.8 m
|
|
gptkbp:historical_significance
|
used in various roles during its service life.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Aero L-60 M
|
|
gptkbp:introduced
|
gptkb:1960
|
|
gptkbp:is_used_by
|
gptkb:Czech_Air_Force
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Aero_Vodochody
|
|
gptkbp:marketed_as
|
gptkb:Aero_L-60_M
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
400 m
1,800 kg
|
|
gptkbp:number_built
|
over 200
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:primary_user
|
gptkb:Czech_Air_Force
|
|
gptkbp:production_years
|
1960-1970
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
gptkb:aircraft
utility aircraft
|
|
gptkbp:seating_capacity
|
gptkb:6
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:successor
|
gptkb:none
|
|
gptkbp:variant
|
gptkb:Aero_L-60
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:wing_area
|
20 m²
|
|
gptkbp:wingspan
|
12.5 m
|