gptkbp:instanceOf
|
aircraft
|
gptkbp:aircraft
|
twin-engine
civil aircraft
cantilever wing
2800 kg
|
gptkbp:capacity
|
10 passengers
|
gptkbp:cockpit
|
enclosed cockpit
|
gptkbp:constructionMaterial
|
metal construction
|
gptkbp:crew
|
2
|
gptkbp:design
|
gptkb:Henri_Farman
high-wing monoplane
|
gptkbp:enginePower
|
450 hp
|
gptkbp:engineType
|
piston engine
|
gptkbp:firstFlight
|
1931
|
gptkbp:fuelCapacity
|
500 L
|
gptkbp:headlights
|
conventional tail
|
gptkbp:historicalSignificance
|
early airliner development
|
https://www.w3.org/2000/01/rdf-schema#label
|
Farman F.82A
|
gptkbp:introduced
|
1931
|
gptkbp:landingGear
|
fixed landing gear
|
gptkbp:length
|
14.0 m
|
gptkbp:manufacturer
|
gptkb:Farman_Aviation_Works
|
gptkbp:maxSpeed
|
200 km/h
|
gptkbp:maxTakeoffWeight
|
3000 kg
|
gptkbp:numberBuilt
|
50
|
gptkbp:operationalArea
|
commercial aviation
|
gptkbp:primaryUser
|
gptkb:Air_France
|
gptkbp:productionYears
|
1931-1935
|
gptkbp:propulsion
|
2
|
gptkbp:range
|
800 km
|
gptkbp:retired
|
1940s
|
gptkbp:role
|
transport aircraft
|
gptkbp:services
|
4000 m
|
gptkbp:usedBy
|
gptkb:French_Air_Force
|
gptkbp:variant
|
gptkb:Farman_F.82B
|
gptkbp:wingspan
|
20.0 m
|