FMA IA-3200

GPTKB entity

Properties (50)
Predicate Object
gptkbp:instanceOf aircraft
gptkbp:aircraft light aircraft
low-wing
gptkbp:armament none
gptkbp:avionics basic flight instruments
gptkbp:climbRate 5 m/s
gptkbp:cockpit tandem_seating
gptkbp:constructionMaterial metal
gptkbp:controls elevator, ailerons, rudder
gptkbp:crew 2
gptkbp:design gptkb:Argentina
high visibility cockpit
FMA_IA-3200_design_team
gptkbp:developer FMA_IA-3200_development_program
gptkbp:emergencyServices parachute system
gptkbp:enginePower 180 hp
gptkbp:engineType piston engine
gptkbp:firstFlight 1980
gptkbp:fuelCapacity 200 L
gptkbp:hasArea gptkb:Juan_Carlos
gptkbp:headlights conventional tail
gptkbp:height 2.5 m
https://www.w3.org/2000/01/rdf-schema#label FMA IA-3200
gptkbp:influences gptkb:Cessna_152
gptkbp:introduced 1980
gptkbp:landingGear tricycle gear
gptkbp:length 8.2 m
gptkbp:manufacturer gptkb:Fábrica_Militar_de_Aviones
gptkbp:market gptkb:South_America
gptkbp:maxSpeed 250 km/h
gptkbp:maxTakeoffWeight 1,500 kg
gptkbp:nickname IA-3200
gptkbp:numberBuilt 50
gptkbp:operationalHistory used in flight training
gptkbp:predecessor none
gptkbp:primaryUser gptkb:Argentine_Air_Force
gptkbp:productionCompany 1980-1990
gptkbp:propulsion two-bladed propeller
gptkbp:range 1,000 km
gptkbp:relatedAircraft FMA IA-58 Pucará
gptkbp:retired 1990
gptkbp:role trainer aircraft
gptkbp:services 4,500 m
gptkbp:speed 70 km/h
gptkbp:succeededBy 10°/s
gptkbp:successor none
gptkbp:type civilian_trainer
gptkbp:variant gptkb:FMA_IA-3200B
FMA IA-3200A
gptkbp:wingspan 10.5 m