Cessna 441 Conquest II
Corporate Aircraft
The Cessna 441 Conquest II is a twin-engined max. eleven-seat light turboprop corporate aircraft with retractable landing gear produced by the US-American manufacturer Cessna Aircraft Company.
The Cessna 441 is a turboprop-powered pressurized development of the
Cessna 404 Titan.
| Crew | 1 / 2 |
| Passengers | max. 9 |
| Propulsion | 2 Turboprop Engines |
| Engine Model | Garrett TPE331-8 |
| Engine Power (each) | 474 kW | 636 shp |
| Speed | 454 km/h | 245 kts
282 mph |
| Mmo (max. Mach) | Mach 0.55 |
| Service Ceiling | 10.668 m | 35.000 ft |
| Range | 4.245 km | 2.292 NM
2.638 mi. |
| Empty Weight | 2.588 kg | 5.706 lbs |
| max. Takeoff Weight | 4.468 kg | 9.850 lbs |
| Wing Span | 15,04 m | 49 ft 4 in |
| Wing Area | 23,6 m² | 254 ft² |
| Length | 11,89 m | 39 ft 0 in |
| Height | 4,01 m | 13 ft 2 in |
| First Flight | 08/1976 |
| Production Status | out of production |
| Total Production | 362 |
| Developed from | Cessna 404 Titan |
| ICAO Code | C441 |
| FAA TCDS | A28CE |
| Data for (Version) | Cessna 441 Conquest II |
