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gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
light aircraft
straight wing
|
|
gptkbp:cockpit
|
two-seat tandem
|
|
gptkbp:covers
|
split flaps
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
low-wing monoplane
FMA_design_team
|
|
gptkbp:engine
|
gptkb:Continental_O-200
|
|
gptkbp:firstFlight
|
1960
1980s
1960-12-01
|
|
gptkbp:fuelCapacity
|
120 liters
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
2.80 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
FMA IA-2600
|
|
gptkbp:introduced
|
1960
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.20 m
|
|
gptkbp:manufacturer
|
gptkb:Fábrica_Militar_de_Aviones
|
|
gptkbp:maximumDepth
|
450 kg
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:notableFeature
|
easy handling
low operating costs
good visibility
robust construction
simple maintenance
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:powerOutput
|
100 hp
|
|
gptkbp:primaryUser
|
gptkb:Argentine_Air_Force
|
|
gptkbp:productionYears
|
1960-1965
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:relatedAircraft
|
gptkb:Piper_PA-28
gptkb:Cessna_150
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
military training
trainer aircraft
civilian training
|
|
gptkbp:services
|
1961
4,000 m
|
|
gptkbp:setting
|
single-engine
|
|
gptkbp:speed
|
65 km/h
|
|
gptkbp:successor
|
gptkb:FMA_IA-63_Pampa
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:variant
|
gptkb:FMA_IA-2600B
FMA IA-2600C
|
|
gptkbp:weight
|
750 kg
|
|
gptkbp:wingspan
|
10.50 m
|