Cessna 401 & 402
401 & 402
Corporate / Commuter / Cargo Aircraft
| Passengers | 6-10 |
| | ||
| Propulsion | 2 Piston Engines |
| Engine Model | Continental
TSIO-520-VB |
| Engine Power (each) | 242 kW | 325 hp |
| | ||
| Speed | 435 km/h | 235 kts |
| | ||
| Empty Weight | 1.846 kg | 4.069 lbs |
| max. Takeoff Weight | 3.107 kg | 6.850 lbs |
| | ||
| Wing Span | 13,45 m | 44,1 ft |
| Length | 11,09 m | 36,4 ft |
| Height | 3,49 m | 11,5 ft |
| | ||
| First Flight | 26. Aug. 1965 |
| Production Status | out of production |
| Total Production | 1936 |
| | ||
| FAA TCDS | A7CE |
| | ||
| Data for (Version) | Cessna 402C |
| Remarks | Total Production: 1936 (401=401, 402=1535). Lighter development of Cessna 411. |
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