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gptkbp:instanceOf
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aircraft
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|
gptkbp:aircraft
|
general aviation
1,500 kg
fixed-wing aircraft
single-engine
used in military training
good performance for training purposes
|
|
gptkbp:armament
|
none
|
|
gptkbp:aspectRatio
|
7.0
|
|
gptkbp:avionics
|
basic instrumentation
|
|
gptkbp:cockpit
|
tandem_seating
|
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gptkbp:controls
|
elevator, ailerons, rudder
|
|
gptkbp:countryOfOrigin
|
gptkb:Argentina
|
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gptkbp:crew
|
2
used for flight training
|
|
gptkbp:design
|
low-wing monoplane
high visibility cockpit
FMA_design_team
|
|
gptkbp:engine
|
twin piston engine
|
|
gptkbp:engineConfiguration
|
piston engine configuration
|
|
gptkbp:enginePower
|
200 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1990
|
|
gptkbp:fuelCapacity
|
200 L
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
FMA IA-2600B
|
|
gptkbp:introduced
|
1990
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|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
gptkb:Fábrica_Militar_de_Aviones
|
|
gptkbp:maximumDepth
|
500 kg
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,600 kg
|
|
gptkbp:navigationEquipment
|
VHF radio
|
|
gptkbp:numberBuilt
|
20
|
|
gptkbp:operationalHistory
|
limited service
|
|
gptkbp:primaryUser
|
gptkb:Argentine_Air_Force
|
|
gptkbp:productionYears
|
1990-2000
|
|
gptkbp:products
|
not certified
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:relatedAircraft
|
IA-58 Pucará
|
|
gptkbp:retired
|
2000
|
|
gptkbp:role
|
light aircraft
trainer aircraft
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:successor
|
none
|
|
gptkbp:supportRole
|
primary flight training
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:variant
|
IA-2600A
|
|
gptkbp:wingArea
|
15 m²
|
|
gptkbp:wingspan
|
10.5 m
|