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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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5
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gptkbp:bfsParent
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gptkb:SIAI-Marchetti_SF.260
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gptkbp:armament
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gptkb:none
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gptkbp:aspect_ratio
|
7.5
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gptkbp:avionics
|
basic avionics package
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gptkbp:climb_rate
|
1,200 ft/min
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gptkbp:cockpit
|
open cockpit
analog instruments
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|
gptkbp:color
|
various civilian schemes
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gptkbp:crew
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gptkb:musical
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gptkbp:design
|
low-wing monoplane
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gptkbp:engine
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260 hp
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gptkbp:engine_type
|
piston engine
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gptkbp:first_flight
|
gptkb:1964
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gptkbp:flaps
|
split flaps
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gptkbp:fuel_capacity
|
120 liters
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gptkbp:height
|
2.4 m
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gptkbp:historical_significance
|
used for military training
used for aerobatic displays
popular in flight schools
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|
https://www.w3.org/2000/01/rdf-schema#label
|
SF.260 W
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gptkbp:landing_gear
|
tricycle gear
|
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gptkbp:length
|
8.2 m
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gptkbp:manufacturer
|
gptkb:SIAI_Marchetti
|
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gptkbp:max_speed
|
200 knots
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|
gptkbp:max_takeoff_weight
|
300 m
400 m
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gptkbp:notable_users
|
gptkb:aircraft
gptkb:Philippine_Air_Force
gptkb:Brazilian_Air_Force
gptkb:Italian_Air_Force
gptkb:military_base
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gptkbp:number_built
|
over 1,000
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gptkbp:origin
|
gptkb:Italy
|
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gptkbp:production_years
|
1964-1989
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
4°/s
|
|
gptkbp:seating_capacity
|
2
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:speed
|
60 knots
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:trim_levels
|
elevator trim
|
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gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:variant
|
gptkb:SF.260_D
gptkb:SF.260_TP
gptkb:SF.260_W
SF.260 C
SF.260 E
|
|
gptkbp:weight
|
1,200 kg
700 kg
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wingspan
|
10.8 m
|