|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:armament
|
none
|
|
gptkbp:aspectRatio
|
6.67
|
|
gptkbp:barrelLength
|
2°/s
|
|
gptkbp:climbRate
|
5 m/s
|
|
gptkbp:cockpit
|
tandem_cockpit
|
|
gptkbp:controls
|
dual control
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Argentina
low-wing monoplane
FMA_IA-3600_design_team
|
|
gptkbp:enginePower
|
180 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1960
|
|
gptkbp:flag
|
4°/s
|
|
gptkbp:fuelCapacity
|
200 liters
|
|
gptkbp:height
|
2.80 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
FMA IA-3600
|
|
gptkbp:introduced
|
1960
|
|
gptkbp:landingGear
|
tricycle landing gear
|
|
gptkbp:length
|
8.20 m
|
|
gptkbp:manufacturer
|
gptkb:Fábrica_Militar_de_Aviones
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,600 kg
|
|
gptkbp:notableFeature
|
good visibility from cockpit.
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:primaryUser
|
gptkb:Argentine_Air_Force
|
|
gptkbp:productionYears
|
1960-1980
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:retired
|
1980
|
|
gptkbp:role
|
light aircraft
trainer aircraft
|
|
gptkbp:serviceHistory
|
used for training and aerobatics.
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:succeededBy
|
3°/s
|
|
gptkbp:successor
|
gptkb:FMA_IA-63_Pampa
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:variant
|
gptkb:FMA_IA-3600B
FMA IA-3600A
|
|
gptkbp:wingArea
|
15 m²
|
|
gptkbp:wingspan
|
10.00 m
|