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gptkbp:instanceOf
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aircraft
|
|
gptkbp:aircraft
|
1,200 miles
light aircraft
low-wing monoplane
|
|
gptkbp:avionics
|
modern avionics systems
|
|
gptkbp:climbRate
|
1,200 ft/min
|
|
gptkbp:cockpit
|
tandem_seating
|
|
gptkbp:crew
|
1-2
|
|
gptkbp:design
|
light twin aircraft
|
|
gptkbp:designatedAs
|
private and business use
|
|
gptkbp:engine
|
2
|
|
gptkbp:enginePower
|
200 hp per engine
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1967
|
|
gptkbp:fuelCapacity
|
100 gallons
|
|
gptkbp:fuelType
|
aviation gasoline
|
|
gptkbp:golfingEvents
|
25,000 ft
|
|
gptkbp:hasFieldOfUse
|
twin-engine aircraft
|
|
gptkbp:height
|
11 ft 5 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Cessna 421 Golden Eagle II
|
|
gptkbp:introduced
|
1967
|
|
gptkbp:landingGear
|
retractable gear
|
|
gptkbp:length
|
35 ft 10 in
|
|
gptkbp:manufacturer
|
gptkb:Cessna_Aircraft_Company
|
|
gptkbp:marketedAs
|
Golden Eagle II
|
|
gptkbp:marketSegment
|
general aviation
|
|
gptkbp:maximum_speed
|
200 knots
|
|
gptkbp:maximumDepth
|
2,000 lb
|
|
gptkbp:maxTakeoffWeight
|
5,200 lb
|
|
gptkbp:notableFeature
|
high performance
pressurized cabin
twin-engine configuration
|
|
gptkbp:notableUsers
|
charter services
flight schools
private owners
|
|
gptkbp:numberOfEpisodes
|
2
|
|
gptkbp:passengerCapacity
|
6
|
|
gptkbp:productionYears
|
1967-1985
|
|
gptkbp:products
|
A24CE
|
|
gptkbp:propulsion
|
constant speed propellers
|
|
gptkbp:range
|
1,200 nautical miles
|
|
gptkbp:retired
|
1985
|
|
gptkbp:services
|
25,000 ft
|
|
gptkbp:speed
|
70 knots
|
|
gptkbp:successor
|
gptkb:Cessna_425
|
|
gptkbp:takeoffDistance
|
1,600 ft
1,800 ft
65 knots
|
|
gptkbp:variant
|
gptkb:Cessna_421C
gptkb:Cessna_421B
gptkb:Cessna_421_Golden_Eagle
|
|
gptkbp:weight
|
3,200 lb
|
|
gptkbp:wingArea
|
250 sq ft
|
|
gptkbp:wingspan
|
38 ft 4 in
|