|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:armament
|
none
|
|
gptkbp:aspectRatio
|
7.6
|
|
gptkbp:climbRate
|
5 m/s
|
|
gptkbp:cockpit
|
tandem_seating
|
|
gptkbp:constructionMaterial
|
metal
|
|
gptkbp:controls
|
elevator, ailerons, rudder
|
|
gptkbp:countryOfOrigin
|
gptkb:Argentina
|
|
gptkbp:covers
|
split flaps
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
low-wing monoplane
FMA_team
|
|
gptkbp:enginePower
|
200 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1960
1980s
|
|
gptkbp:fuelCapacity
|
200 L
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
2.80 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
FMA IA-1000
|
|
gptkbp:introduced
|
1960
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.20 m
|
|
gptkbp:manufacturer
|
gptkb:Fábrica_Militar_de_Aviones
|
|
gptkbp:market
|
training market
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:nickname
|
IA-1000
|
|
gptkbp:notableFeature
|
1961
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:operationalHistory
|
used for pilot training.
|
|
gptkbp:primaryUser
|
gptkb:Argentine_Air_Force
|
|
gptkbp:productionYears
|
1960-1970
|
|
gptkbp:propulsion
|
two-bladed
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
trainer aircraft
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:setting
|
single-engine
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:succeededBy
|
4.5°/s
|
|
gptkbp:successor
|
gptkb:FMA_IA-63_Pampa
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:type
|
civilian aircraft
|
|
gptkbp:variant
|
gptkb:FMA_IA-1000B
|
|
gptkbp:wingArea
|
12.5 m²
|
|
gptkbp:wingspan
|
9.50 m
|