|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
light aircraft
single-engine
|
|
gptkbp:armament
|
none
|
|
gptkbp:aspectRatio
|
7.0
|
|
gptkbp:cockpit
|
glass 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_design_team
|
|
gptkbp:engine
|
Lycoming IO-540
|
|
gptkbp:enginePower
|
260 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstAwarded
|
2000
|
|
gptkbp:firstFlight
|
1990
|
|
gptkbp:fuelCapacity
|
200 L
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
FMA IA-1100
|
|
gptkbp:introduced
|
1990
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
gptkb:Fábrica_Militar_de_Aviones
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:nickname
|
IA-1100
|
|
gptkbp:notableFeature
|
1991
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:participatesIn
|
pilot training
|
|
gptkbp:primaryUser
|
gptkb:Argentine_Air_Force
|
|
gptkbp:productionYears
|
1990-2000
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:relatedAircraft
|
FMA IA-58 Pucará
|
|
gptkbp:retired
|
2000
|
|
gptkbp:role
|
trainer aircraft
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
none
|
|
gptkbp:supportRole
|
basic flight training
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:type
|
civil and military training aircraft
|
|
gptkbp:variant
|
IA-1100B
|
|
gptkbp:weight
|
800 kg
|
|
gptkbp:wingArea
|
15 m²
|
|
gptkbp:wingspan
|
10.5 m
|