gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Letov_Š-328
|
gptkbp:aircraft_operated
|
gptkb:Letov_Š-45
high-wing
Letov Š-28
|
gptkbp:aspect_ratio
|
6.0
|
gptkbp:climb_rate
|
3 m/s
|
gptkbp:cockpit
|
enclosed
|
gptkbp:crew
|
gptkb:musical
|
gptkbp:design
|
gptkb:Miloš_Štěpánek
|
gptkbp:engine
|
gptkb:Avia_M-137
200 hp
|
gptkbp:engine_type
|
piston engine
|
gptkbp:features
|
all-metal construction
|
gptkbp:first_flight
|
1947
|
gptkbp:fuel_capacity
|
500 L
40 L/h
|
gptkbp:height
|
2.5 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Letov Š-47
|
gptkbp:introduced
|
1948
|
gptkbp:is_used_by
|
gptkb:Czechoslovak_Air_Force
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
8.5 m
|
gptkbp:manufacturer
|
Letov
|
gptkbp:max_speed
|
250 km/h
|
gptkbp:max_takeoff_weight
|
300 m
400 m
2500 kg
|
gptkbp:number_built
|
50
|
gptkbp:origin
|
gptkb:Monarch
|
gptkbp:production_years
|
1947-1950
|
gptkbp:propulsion
|
two-bladed propeller
|
gptkbp:range
|
800 km
|
gptkbp:retired
|
1960s
|
gptkbp:role
|
gptkb:aircraft
utility aircraft
|
gptkbp:seating_capacity
|
gptkb:4
500 kg
1000 kg
|
gptkbp:service_ceiling
|
5000 m
|
gptkbp:service_history
|
used in various roles including training and transport.
|
gptkbp:speed
|
70 km/h
|
gptkbp:successor
|
Letov Š-56
|
gptkbp:surface
|
elevator and ailerons
|
gptkbp:tail_type
|
conventional tail
|
gptkbp:type
|
gptkb:aircraft
|
gptkbp:variant
|
Letov Š-47 A
Letov Š-47 B
|
gptkbp:wing_area
|
20 m²
|
gptkbp:wingspan
|
12.0 m
|