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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Letov_Š-328
|
|
gptkbp:aircraft_operated
|
gptkb:Letov_Š-34
60 kg/m²
Letov Š-231
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:aspect_ratio
|
7.0
|
|
gptkbp:climb_rate
|
4 m/s
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
Letov design bureau
Vladimír Štros
|
|
gptkbp:engine
|
Avia R-14
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1935
1945-12-31
1935-06-01
|
|
gptkbp:fuel_capacity
|
150 L
|
|
gptkbp:height
|
2.5 m
|
|
gptkbp:historical_significance
|
used in training pilots during WWII
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Letov Š-50
|
|
gptkbp:is_used_by
|
gptkb:Czechoslovak_Air_Force
|
|
gptkbp:landing_gear
|
tailwheel
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
Letov
|
|
gptkbp:material
|
gptkb:NACA_2412
8.2 m
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
1,400 kg
|
|
gptkbp:number_built
|
50
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:power_consumption
|
6 kg/hp
|
|
gptkbp:powers
|
200 hp
|
|
gptkbp:primary_user
|
gptkb:Czechoslovak_Air_Force
|
|
gptkbp:production_location
|
gptkb:Monarch
|
|
gptkbp:production_years
|
1935-1938
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retirement_year
|
1945
|
|
gptkbp:role
|
gptkb:aircraft
civil trainer
|
|
gptkbp:service_ceiling
|
3,500 m
|
|
gptkbp:services
|
1936
|
|
gptkbp:setting
|
two-seat
|
|
gptkbp:speed
|
160 km/h
70 km/h
|
|
gptkbp:successor
|
gptkb:Letov_Š-328
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:variant
|
Letov Š-50 A
Letov Š-50 B
|
|
gptkbp:wing_area
|
20 m²
|
|
gptkbp:wingspan
|
10.5 m
|