Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:aircraftType |
gptkb:aircraft
|
| gptkbp:alsoKnownAs |
gptkb:Tobago
|
| gptkbp:capacity |
3 passengers
|
| gptkbp:configuration |
low-wing
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:crew |
1
|
| gptkbp:cruiseSpeed |
235 km/h
|
| gptkbp:emptyWeight |
760 kg
|
| gptkbp:engineType |
piston
|
| gptkbp:firstFlight |
1977
|
| gptkbp:height |
2.97 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Socata TB-10
|
| gptkbp:introduced |
1979
|
| gptkbp:landingGear |
fixed tricycle
|
| gptkbp:length |
7.56 m
|
| gptkbp:manufacturer |
gptkb:SOCATA
|
| gptkbp:maximumSpeed |
260 km/h
|
| gptkbp:maxTakeoffWeight |
1,150 kg
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:powerOutput |
180 hp
|
| gptkbp:powerplant |
Lycoming O-360-A1AD
|
| gptkbp:produced |
1979-2002
|
| gptkbp:range |
1,250 km
|
| gptkbp:serviceCeiling |
4,115 m
|
| gptkbp:successor |
gptkb:Socata_TB-20
|
| gptkbp:usedBy |
gptkb:French_Air_Force
civil aviation |
| gptkbp:wingspan |
9.97 m
|
| gptkbp:bfsParent |
gptkb:Royal_Cameroonian_Air_Force
|
| gptkbp:bfsLayer |
5
|