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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
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gptkb:civil_aviation
|
|
gptkbp:capacity
|
10 passengers
|
|
gptkbp:ceiling
|
6,000 m
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|
gptkbp:climb_rate
|
5 m/s
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gptkbp:cockpit
|
two-seat cockpit
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gptkbp:control_surfaces
|
gptkb:elevator
rudder
aileron
|
|
gptkbp:crew
|
2
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gptkbp:design
|
gptkb:Alberto_Savoia
|
|
gptkbp:design_date
|
1940s
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gptkbp:engine_power
|
300 hp
|
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gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
1947
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|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
800 L
|
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gptkbp:fuselage_material
|
gptkb:metal
gptkb:NACA_2412
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gptkbp:height
|
4.5 m
|
|
gptkbp:historical_significance
|
post-war transport aircraft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Savoia-Marchetti S.248
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gptkbp:influenced_by
|
gptkb:Savoia-Marchetti_S.55
|
|
gptkbp:landing_distance
|
700 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
15.5 m
|
|
gptkbp:manufacturer
|
gptkb:Savoia-Marchetti
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
3,500 kg
|
|
gptkbp:number_built
|
gptkb:100
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:primary_user
|
gptkb:Alitalia
|
|
gptkbp:production_years
|
1947-1955
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirement
|
1960s
|
|
gptkbp:role
|
gptkb:transport_aircraft
|
|
gptkbp:service_ceiling
|
5,000 m
|
|
gptkbp:service_entry
|
1948
|
|
gptkbp:slats
|
leading-edge slats
|
|
gptkbp:stall_speed
|
80 km/h
|
|
gptkbp:successor
|
gptkb:Savoia-Marchetti_S.211
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:takeoff_distance
|
600 m
|
|
gptkbp:used_by
|
gptkb:Italian_Air_Force
|
|
gptkbp:variant
|
S.248 A
S.248 B
|
|
gptkbp:weight
|
2,200 kg
|
|
gptkbp:wing_configuration
|
gptkb:metal
high-wing
|
|
gptkbp:wingspan
|
20.0 m
|
|
gptkbp:bfsParent
|
gptkb:Savoia-Marchetti
|
|
gptkbp:bfsLayer
|
5
|