Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:aircraftType |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:cruiseSpeed |
135 knots
|
| gptkbp:engine |
gptkb:Lycoming_IO-360-A1B6
|
| gptkbp:enginePower |
200 hp
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:family |
Socata TB series
|
| gptkbp:firstFlight |
1991
|
| gptkbp:height |
2.92 m
|
| gptkbp:landingGear |
gptkb:cyclist
|
| gptkbp:length |
7.62 m
|
| gptkbp:manufacturer |
gptkb:SOCATA
|
| gptkbp:maxTakeoffWeight |
1157 kg
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:range |
650 nautical miles
|
| gptkbp:seatingCapacity |
4
|
| gptkbp:successor |
gptkb:Socata_TB-20_Trinidad
|
| gptkbp:wingConfiguration |
low wing
|
| gptkbp:wingspan |
9.97 m
|
| gptkbp:bfsParent |
gptkb:Royal_Cameroonian_Air_Force
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Socata TB-200 Tobago
|