Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:aircraftType |
gptkb:aircraft
single-engine |
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:crew |
1
|
| gptkbp:cruiseSpeed |
155 knots
|
| gptkbp:emptyWeight |
980 kg
|
| gptkbp:engine |
gptkb:Lycoming_IO-540
|
| gptkbp:enginePower |
250 hp
|
| gptkbp:engineType |
piston
|
| gptkbp:firstFlight |
1981
|
| gptkbp:fuelType |
318 liters
|
| gptkbp:height |
2.97 m
|
| gptkbp:introduced |
1981
|
| gptkbp:landingGear |
retractable tricycle
|
| gptkbp:length |
7.62 m
|
| gptkbp:manufacturer |
gptkb:SOCATA
|
| gptkbp:maximumSpeed |
165 knots
|
| gptkbp:maxTakeoffWeight |
1400 kg
|
| gptkbp:numberBuilt |
over 2,150 (all TB-20 variants)
|
| gptkbp:primaryUse |
training
general aviation touring |
| gptkbp:range |
1100 nautical miles
|
| gptkbp:relatedTo |
gptkb:SOCATA_TB-10_Tobago
SOCATA TB-21 Trinidad |
| gptkbp:seatingCapacity |
4
|
| gptkbp:serviceCeiling |
20,000 ft
|
| gptkbp:wingspan |
10.01 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
SOCATA TB-20 Trinidad XL
|