|
gptkbp:instanceOf
|
gptkb:aircraft
|
|
gptkbp:aircraftType
|
general aviation
single-engine
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:crew
|
1
|
|
gptkbp:cruiseSpeed
|
170 knots
|
|
gptkbp:emptyWeight
|
2,300 lb
|
|
gptkbp:engine
|
gptkb:Continental_IO-520-L
|
|
gptkbp:enginePower
|
300 hp
|
|
gptkbp:engineType
|
piston
|
|
gptkbp:firstFlight
|
1957
|
|
gptkbp:height
|
9 ft 8 in
|
|
gptkbp:introduced
|
1960
|
|
gptkbp:landingGear
|
retractable
|
|
gptkbp:length
|
28 ft 2 in
|
|
gptkbp:manufacturer
|
gptkb:Cessna
|
|
gptkbp:maximumSpeed
|
200 knots
|
|
gptkbp:maxTakeoffWeight
|
4,000 lb
|
|
gptkbp:notableFeature
|
high performance
cantilever wing
pressurized variant available
|
|
gptkbp:numberBuilt
|
9240
|
|
gptkbp:pressurizedVariant
|
gptkb:Cessna_P210
|
|
gptkbp:primaryUse
|
air taxi
flight training
private aviation
|
|
gptkbp:productionEndYear
|
1986
|
|
gptkbp:range
|
900 nautical miles
|
|
gptkbp:seatingCapacity
|
5
|
|
gptkbp:serviceCeiling
|
17,300 ft
|
|
gptkbp:successor
|
gptkb:Cessna_TTx
|
|
gptkbp:variant
|
gptkb:Cessna_210L
gptkb:Cessna_210M
gptkb:Cessna_210N
gptkb:Cessna_P210
gptkb:Cessna_T210
Cessna 210A
Cessna 210B
Cessna 210C
Cessna 210D
Cessna 210E
Cessna 210F
Cessna 210G
Cessna 210H
Cessna 210J
Cessna 210K
|
|
gptkbp:wingspan
|
36 ft 11 in
|
|
gptkbp:bfsParent
|
gptkb:Cessna_210
gptkb:Cessna_U-210
|
|
gptkbp:bfsLayer
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Cessna 210 Centurion
|