Cessna 421 Golden Eagle
Corporate Aircraft
The Cessna 421 Golden Eagle is a twin-engined six- to ten-seat light corporate aircraft with retractable landing gear produced by the US-American manufacturer Cessna Aircraft Company.
The Cessna 421 is a development of the
Cessna 411 with pressurized cabin.
| Propulsion | 2 Piston Engines |
| Engine Model | Continental GTSIO-520-N |
| Engine Power (each) | 280 kW | 375 hp |
| max. Cruise Speed | 372 km/h | 201 kts
231 mph |
| max. Speed (vne) | 444 km/h | 240 kts
276 mph |
| Service Ceiling | 9.205 m | 30.200 ft |
| Range | 2.752 km | 1.486 NM
1.710 mi. |
| Empty Weight | 2.129 kg | 4.694 lbs |
| max. Takeoff Weight | 3.379 kg | 7.450 lbs |
| Wing Span | 12,53 m | 41 ft 1 in |
| Wing Area | 20,0 m² | 215 ft² |
| Length | 11,09 m | 36 ft 5 in |
| Height | 3,49 m | 11 ft 5 in |
| First Flight | 14.10.1965 |
| Production Status | out of production |
| Total Production | 1909 |
| ICAO Code | C21T C421 |
| FAA TCDS | A7CE |
| Data for (Version) | Cessna 421C Golden Eagle |
| Variants | 421, 421A, 421B, 421C |
