Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:aircraftType |
general aviation
single-engine |
| gptkbp:category |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:crew |
1
|
| gptkbp:cruiseSpeed |
approximately 160 knots
|
| gptkbp:emptyWeight |
2,050 lb
|
| gptkbp:engine |
gptkb:Continental_IO-520-L
|
| gptkbp:engineType |
piston
|
| gptkbp:firstFlight |
1972
|
| gptkbp:fuelType |
90 US gallons
|
| https://www.w3.org/2000/01/rdf-schema#label |
Cessna 210L
|
| gptkbp:introduced |
1972
|
| gptkbp:landingGear |
retractable
|
| gptkbp:manufacturer |
gptkb:Cessna
|
| gptkbp:maxTakeoffWeight |
3,800 lb
|
| gptkbp:powerOutput |
300 hp
|
| gptkbp:predecessor |
Cessna 210K
|
| gptkbp:productionEndYear |
1976
|
| gptkbp:range |
approximately 900 nautical miles
|
| gptkbp:seatingCapacity |
6
|
| gptkbp:successor |
gptkb:Cessna_210M
|
| gptkbp:wingConfiguration |
high-wing
|
| gptkbp:bfsParent |
gptkb:Cessna_210
|
| gptkbp:bfsLayer |
6
|