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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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9
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gptkbp:bfsParent
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gptkb:Aero_L-60
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gptkbp:aircraft_operated
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gptkb:aircraft
general aviation
high-wing configuration
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gptkbp:cockpit
|
two-seat cockpit
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gptkbp:combat_role
|
transport and reconnaissance
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gptkbp:crew
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2
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gptkbp:design
|
low-wing monoplane
Václav Krištof
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gptkbp:engine
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gptkb:musical
250 hp
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gptkbp:engine_type
|
piston engine
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|
gptkbp:financial_performance
|
good stability and handling
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gptkbp:first_flight
|
gptkb:1956
1956-05-01
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gptkbp:flaps
|
manual flaps
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|
gptkbp:fuel_capacity
|
400 liters
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gptkbp:height
|
2.8 m
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gptkbp:historical_significance
|
important in Czechoslovak aviation history
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Aero L-60 T
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|
gptkbp:introduced
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gptkb:1956
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|
gptkbp:is_used_by
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gptkb:Czech_Air_Force
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Aero_Vodochody
|
|
gptkbp:market
|
domestic and international markets
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
400 m
2,500 kg
|
|
gptkbp:notable_features
|
versatile utility capabilities
|
|
gptkbp:number_built
|
over 200
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|
gptkbp:primary_user
|
civil aviation, military
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|
gptkbp:production_location
|
gptkb:Monarch
|
|
gptkbp:production_years
|
1956-1960
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|
gptkbp:propulsion
|
two-bladed propeller
propeller-driven
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:retired
|
1970s
|
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gptkbp:role
|
utility aircraft
|
|
gptkbp:seating_capacity
|
gptkb:6
1,000 kg
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:successor
|
gptkb:Aero_L-39_Albatros
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:variant
|
L-60, L-60 T, L-60 T-1
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
12.5 m
|