Photo ©: Karsten Palt
414
Corporate Aircraft
The Cessna 414 is a twin engined light corporate aircraft with pressurized cabin for a maximum of 7 passengers built by US-American manufacturer Cessna Aircraft Company.
| Crew | 1-2 | |
| Passengers | 5-7 | |
| Propulsion | 2 Piston Engines | |
| Engine Model | Continental TSIO-520-N | |
| Engine Power (each) | 231 kW | 310 hp |
| max. Cruise Speed | 376 km/h | 203 kts 234 mph |
| max. Speed (vne) | 439 km/h | 237 kts 273 mph |
| Service Ceiling | 9.144 m | 30.000 ft |
| Rate of climb | 463 m/min | 1520 ft/min |
| Range | 2.459 km | 1.328 NM 1.528 mi. |
| Empty Weight | 1.973 kg | 4.350 lbs |
| max. Takeoff Weight | 3.062 kg | 6.750 lbs |
| max. Landing Weight | 3.062 kg | 6.750 lbs |
| Wing Span | 13,45 m | 44,1 ft |
| Wing Area | 21,0 m² | 226 ft² |
| Length | 11,09 m | 36,4 ft |
| Height | 3,49 m | 11,5 ft |
| First Flight | 1968 | |
| Production Status | out of production | |
| Production Range | 1968-1985 | |
| Total Production | 1070 | |
| Developed from | Cessna 421 | |
| ICAO Code | C414, C14T | |
| FAA TCDS | A7CE | |
| Data for (Version) | Cessna 414A Chancellor | |
| Variants | 414, 414A Chancellor, Turbo Star Pressurized 414 | |
Remarks
The Cessna 414 is a less powerfull and lighter development of the Cessna 421.