|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
high-wing
|
|
gptkbp:armament
|
none
|
|
gptkbp:aspectRatio
|
7.0
|
|
gptkbp:cockpit
|
tandem_seating
|
|
gptkbp:controls
|
elevator
rudder
aileron
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Fábrica_Militar_de_Aviones
low-wing monoplane
|
|
gptkbp:engine
|
Lycoming O-360
|
|
gptkbp:enginePower
|
180 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1960
|
|
gptkbp:fuelCapacity
|
200 L
30 L/h
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
FMA IA-1600
|
|
gptkbp:introduced
|
1960
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.1 m
|
|
gptkbp:manufacturer
|
gptkb:Fábrica_Militar_de_Aviones
|
|
gptkbp:maximumDepth
|
400 kg
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:notableFeature
|
easy handling
low operating costs
good visibility
retractable landing gear
stable flight characteristics
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:numberOfSeasons
|
2
|
|
gptkbp:primaryUser
|
gptkb:Argentine_Air_Force
|
|
gptkbp:productionStartYear
|
1960
|
|
gptkbp:productionYears
|
1965
|
|
gptkbp:propulsion
|
two-bladed
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
trainer aircraft
civil training aircraft
|
|
gptkbp:serviceHistory
|
used for pilot training
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:successor
|
gptkb:FMA_IA-63_Pampa
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:variant
|
IA-1600A
IA-1600B
|
|
gptkbp:wingArea
|
15 m²
|
|
gptkbp:wingspan
|
10.5 m
|