gptkbp:instanceOf
|
aircraft
|
gptkbp:aircraft
|
4.5 m
fixed-wing aircraft
utility aircraft
15.5 m
3,500 kg
transport aircraft
straight wing
|
gptkbp:armament
|
machine guns
|
gptkbp:cockpit
|
pressurized
|
gptkbp:constructionMaterial
|
aluminum
|
gptkbp:crew
|
2
military pilots
|
gptkbp:design
|
gptkb:France
high-wing configuration
Jean_Cantinieau
|
gptkbp:engine
|
2
|
gptkbp:engineConfiguration
|
gptkb:Pratt_&_Whitney
twin-engine
|
gptkbp:enginePower
|
1,000 hp
|
gptkbp:engineType
|
turboprop
|
gptkbp:firstFlight
|
1960
1990
|
gptkbp:fuelCapacity
|
1,500 L
|
gptkbp:height
|
4.5 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
SA 341
|
gptkbp:landingGear
|
tricycle gear
|
gptkbp:length
|
15.5 m
|
gptkbp:manufacturer
|
Société_Aéronautique_de_France
|
gptkbp:maximumDepth
|
2,000 kg
|
gptkbp:maxRange
|
1,800 km
|
gptkbp:maxSpeed
|
400 km/h
|
gptkbp:maxTakeoffWeight
|
4,500 kg
5,000 kg
|
gptkbp:notableFeature
|
1961
|
gptkbp:notableUsers
|
gptkb:French_Navy
|
gptkbp:numberBuilt
|
200
|
gptkbp:operationalRange
|
1,200 km
|
gptkbp:operationalStatus
|
retired
|
gptkbp:passengerCapacity
|
20
rear ramp
|
gptkbp:primaryUser
|
gptkb:French_military
|
gptkbp:productionYears
|
1960-1970
|
gptkbp:propulsion
|
2
|
gptkbp:range
|
1,500 km
|
gptkbp:retirementYear
|
1980
|
gptkbp:role
|
military transport aircraft
cargo_aircraft
|
gptkbp:services
|
1961
6,000 m
|
gptkbp:successor
|
SA_342
|
gptkbp:takeoffDistance
|
600 m
800 m
|
gptkbp:usedBy
|
gptkb:French_Air_Force
|
gptkbp:variant
|
SA_341G
|
gptkbp:wingArea
|
30 m²
|
gptkbp:wingspan
|
15.0 m
|