gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:SIAI-Marchetti_SF.260
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:item
general aviation
flight training
single-engine
recreational flying
aerobatic training
|
gptkbp:allows
|
+6/-3 g
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gptkbp:cockpit
|
two-seat tandem
|
gptkbp:controls
|
yoke
|
gptkbp:crew
|
gptkb:musical
|
gptkbp:design
|
low-wing monoplane
|
gptkbp:engine
|
gptkb:Lycoming_IO-540
|
gptkbp:engine_type
|
piston engine
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gptkbp:first_flight
|
gptkb:1964
|
gptkbp:flaps
|
split flaps
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gptkbp:height
|
2.40 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
SF.260 D
|
gptkbp:is_used_by
|
gptkb:aircraft
gptkb:military_unit
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
7.62 m
|
gptkbp:manufacturer
|
gptkb:SIAI_Marchetti
|
gptkbp:material
|
gptkb:item
|
gptkbp:max_speed
|
250 km/h
|
gptkbp:max_takeoff_weight
|
300 m
400 m
1,200 kg
|
gptkbp:notable_users
|
gptkb:aircraft
gptkb:Royal_Netherlands_Air_Force
gptkb:Italian_Air_Force
|
gptkbp:number_built
|
over 1,000
|
gptkbp:power_output
|
260 hp
|
gptkbp:production_years
|
1964-1989
|
gptkbp:propulsion
|
constant-speed propeller
|
gptkbp:range
|
1,200 km
|
gptkbp:role
|
gptkb:aircraft
|
gptkbp:roll_rate
|
3.5°/s
|
gptkbp:seating_capacity
|
2
|
gptkbp:service_ceiling
|
4,500 m
|
gptkbp:speed
|
70 km/h
|
gptkbp:tail_type
|
T-tail
|
gptkbp:variant
|
gptkb:SF.260_TP
SF.260 C
SF.260 E
|
gptkbp:wing_area
|
14.5 m²
|
gptkbp:wingspan
|
9.00 m
|