|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:armament
|
none
|
|
gptkbp:aspectRatio
|
7:1
|
|
gptkbp:cockpit
|
basic flight instruments
tandem_seating
|
|
gptkbp:covers
|
split flaps
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
FMA IA-170
FMA_design_team
|
|
gptkbp:engine
|
Lycoming O-360
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1970
1990-12-01
1970-12-01
|
|
gptkbp:floors
|
conventional elevator
|
|
gptkbp:fuelCapacity
|
200 L
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
FMA IA-1700
|
|
gptkbp:introduced
|
1970
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Fábrica_Militar_de_Aviones
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,500 kg
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:operationalHistory
|
used in training missions.
|
|
gptkbp:operationalStatus
|
single aileron
|
|
gptkbp:payloadCapacity
|
500 kg
|
|
gptkbp:primaryUser
|
gptkb:Argentine_Air_Force
|
|
gptkbp:productionYears
|
1970-1990
|
|
gptkbp:propulsion
|
two-bladed
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:retired
|
1990
|
|
gptkbp:role
|
light aircraft
trainer aircraft
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:setting
|
low-wing
|
|
gptkbp:speed
|
70 km/h
good stall characteristics
|
|
gptkbp:steering
|
conventional rudder
|
|
gptkbp:successor
|
none
|
|
gptkbp:supportRole
|
pilot training
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:type
|
civilian aircraft
|
|
gptkbp:variant
|
FMA IA-1700B
|
|
gptkbp:wingArea
|
15 m²
|
|
gptkbp:wingspan
|
10.5 m
|