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gptkbp:instanceOf
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aircraft
|
|
gptkbp:aircraft
|
fixed-wing aircraft
light aircraft
high-wing
|
|
gptkbp:armament
|
none
|
|
gptkbp:built
|
1965
|
|
gptkbp:cockpit
|
tandem_seating
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
gptkb:Fábrica_Militar_de_Aviones
all-metal construction
|
|
gptkbp:engine
|
Lycoming IO-540
|
|
gptkbp:enginePower
|
260 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:financial_aid
|
good stability characteristics
|
|
gptkbp:firstFlight
|
1970
successful
|
|
gptkbp:fuelCapacity
|
600 L
30 L/h
|
|
gptkbp:height
|
2.8 m
|
|
gptkbp:historicalSignificance
|
first indigenous aircraft design in Argentina.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
FMA IA-4000
|
|
gptkbp:introduced
|
1970
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Fábrica_Militar_de_Aviones
|
|
gptkbp:market
|
civil and military aviation
|
|
gptkbp:marketedAs
|
multi-role aircraft
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
2,500 kg
|
|
gptkbp:missions
|
conventional control surfaces
|
|
gptkbp:nickname
|
IA-4000
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:operationalHistory
|
used in various roles
|
|
gptkbp:passengerCapacity
|
6
|
|
gptkbp:performance
|
good short-field performance
|
|
gptkbp:primaryUser
|
gptkb:Argentine_Air_Force
|
|
gptkbp:productionCompany
|
1970-1990
|
|
gptkbp:productionLocation
|
gptkb:Argentina
|
|
gptkbp:propulsion
|
constant-speed propeller
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:relatedAircraft
|
gptkb:Cessna_206
Beechcraft Baron
Piper PA-31
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
utility aircraft
trainer aircraft
|
|
gptkbp:services
|
3,000 m
|
|
gptkbp:successor
|
IA-58 Pucará
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:team
|
FMA_engineers
|
|
gptkbp:variant
|
IA-4000B
IA-4000C
|
|
gptkbp:weight
|
1,500 kg
1,000 kg
|
|
gptkbp:wingspan
|
11.5 m
|