|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
1,400 kg
light aircraft
100 kg/m²
|
|
gptkbp:armament
|
none
|
|
gptkbp:climbRate
|
5 m/s
|
|
gptkbp:cockpit
|
tandem_seating
|
|
gptkbp:constructionMaterial
|
NACA 2412
|
|
gptkbp:covers
|
split flaps
|
|
gptkbp:crew
|
2
military pilot training
|
|
gptkbp:design
|
low-wing monoplane
trainer and utility aircraft
Fábrica_Militar_de_Aviones_team
|
|
gptkbp:engine
|
Lycoming O-360
|
|
gptkbp:enginePower
|
180 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1970
1990s
|
|
gptkbp:fuelCapacity
|
200 L
30 L/h
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
2.80 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
FMA IA-3400
|
|
gptkbp:introduced
|
1970
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.20 m
|
|
gptkbp:manufacturer
|
gptkb:Fábrica_Militar_de_Aviones
|
|
gptkbp:maximumDepth
|
500 kg
4,500 m
|
|
gptkbp:maxRange
|
1,200 km
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,500 kg
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:powerOutput
|
8.33 kg/hp
|
|
gptkbp:primaryUser
|
gptkb:Argentine_Air_Force
|
|
gptkbp:productionYears
|
1970-1980
|
|
gptkbp:propulsion
|
two-bladed
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
trainer aircraft
|
|
gptkbp:services
|
1970
4,500 m
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:succeededBy
|
3°/s
|
|
gptkbp:successor
|
none
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:type
|
civil and military trainer
|
|
gptkbp:variant
|
gptkb:FMA_IA-3400B
|
|
gptkbp:weight
|
1,000 kg
|
|
gptkbp:wingArea
|
15 m²
|
|
gptkbp:wingspan
|
10.50 m
|