Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:aircraftType |
gptkb:aircraft
|
| gptkbp:cruiseSpeed |
240 knots
|
| gptkbp:engine |
gptkb:Continental_GTSIO-520-L
|
| gptkbp:engineType |
twin piston
|
| gptkbp:firstFlight |
1975
|
| https://www.w3.org/2000/01/rdf-schema#label |
Cessna 421C Golden Eagle
|
| gptkbp:introduced |
1976
|
| gptkbp:landingGear |
retractable tricycle
|
| gptkbp:manufacturer |
gptkb:Cessna
|
| gptkbp:maxTakeoffWeight |
7,450 lb
|
| gptkbp:notableFeature |
improved landing gear design
wet wing fuel system |
| gptkbp:numberOfAxles |
cantilever low-wing
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:pressurizedCabin |
yes
|
| gptkbp:productionEndYear |
1985
|
| gptkbp:range |
1,770 nautical miles
|
| gptkbp:seatingCapacity |
6 to 8
|
| gptkbp:serviceCeiling |
30,000 ft
|
| gptkbp:successor |
gptkb:Cessna_425_Corsair
|
| gptkbp:usedFor |
air taxi
business aviation private transport |
| gptkbp:variant |
gptkb:Cessna_421
|
| gptkbp:bfsParent |
gptkb:Continental_TSIO-520-VB
gptkb:No._42_Squadron_RNZAF |
| gptkbp:bfsLayer |
7
|