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gptkbp:instanceOf
|
gptkb:aircraft
|
|
gptkbp:aircraftType
|
gptkb:aircraft
|
|
gptkbp:category
|
single-engine aircraft
civil utility aircraft
|
|
gptkbp:countryOfOrigin
|
gptkb:France
|
|
gptkbp:crew
|
1
|
|
gptkbp:emptyWeight
|
900 kg
|
|
gptkbp:engine
|
gptkb:Lycoming_IO-540
|
|
gptkbp:engineType
|
piston
|
|
gptkbp:firstFlight
|
1977
|
|
gptkbp:fuelType
|
86 US gallons
|
|
gptkbp:height
|
2.97 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SOCATA TB-20 Trinidad
|
|
gptkbp:ICAOTypeDesignator
|
TB20
|
|
gptkbp:introduced
|
1980
|
|
gptkbp:landingGear
|
retractable tricycle
|
|
gptkbp:length
|
7.62 m
|
|
gptkbp:manufacturer
|
gptkb:SOCATA
|
|
gptkbp:maximumSpeed
|
165 knots
|
|
gptkbp:maxTakeoffWeight
|
1400 kg
|
|
gptkbp:powerplant
|
1 × Lycoming IO-540-C4D5D
|
|
gptkbp:primaryUse
|
general aviation
|
|
gptkbp:propulsion
|
constant-speed
|
|
gptkbp:range
|
1100 nautical miles
|
|
gptkbp:relatedTo
|
gptkb:SOCATA_TB-10_Tobago
gptkb:SOCATA_TB-9_Tampico
|
|
gptkbp:seatingCapacity
|
5
|
|
gptkbp:successor
|
SOCATA TB-21 Trinidad Turbo
|
|
gptkbp:wingConfiguration
|
low wing
|
|
gptkbp:wingspan
|
9.97 m
|
|
gptkbp:bfsParent
|
gptkb:Madagascar_Air_Force
|
|
gptkbp:bfsLayer
|
5
|