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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:horse_race
gptkb:aircraft
gptkb:battle
biplane configuration
fabric-covered wood
fabric-covered wooden wings
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:climb_rate
|
3.5 m/s
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:crew
|
2
1 pilot
|
|
gptkbp:date
|
gptkb:1935
|
|
gptkbp:design
|
gptkb:Václav_Klement
biplane design
|
|
gptkbp:engine
|
Avia R-14
|
|
gptkbp:engine_type
|
inline engine
|
|
gptkbp:first_flight
|
gptkb:1935
|
|
gptkbp:fuel_capacity
|
150 L
|
|
gptkbp:height
|
2.5 m
|
|
gptkbp:historical_event
|
pilot training
|
|
gptkbp:historical_significance
|
used for pilot training during WWII
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Letov Š-18
|
|
gptkbp:is_used_by
|
gptkb:Czechoslovak_Air_Force
|
|
gptkbp:landing_gear
|
tailwheel
tailwheel landing gear
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
Letov
|
|
gptkbp:material
|
wooden structure
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:nationality
|
Czechoslovakian
|
|
gptkbp:number_built
|
50
|
|
gptkbp:powers
|
300 hp
|
|
gptkbp:produced_by
|
1935-1940
|
|
gptkbp:production_location
|
gptkb:Monarch
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retirement_year
|
1945
|
|
gptkbp:role
|
gptkb:aircraft
civilian training aircraft
|
|
gptkbp:seating_capacity
|
1 student pilot
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:services
|
1936
1936-1945
|
|
gptkbp:setting
|
gptkb:aircraft
two-seat tandem
|
|
gptkbp:speed
|
60 km/h
|
|
gptkbp:successor
|
Letov Š-28
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:variant
|
Letov Š-18 A
Letov Š-18 B
|
|
gptkbp:wing_area
|
20 m²
|
|
gptkbp:wingspan
|
10.5 m
|