Cessna 425 Corsair & Conquest I
Photo ©: Roger Oldfield (Photos at airliners.net)
425 Corsair & Conquest I
Corporate Aircraft
The Cessna 425 Corsair & Conquest I is a twin-engined six- to eight-seat light turboprop corporate aircraft with retractable landing gear produced by the US-American manufacturer Cessna Aircraft Company.
| Crew | 1 / 2 | |
| Passengers | 4-6 | |
| Propulsion | 2 Turboprop Engines | |
| Engine Model | Pratt & Whitney Canada PT6A-112 | |
| Engine Power (each) | 336 kW | 450 shp |
| Speed | 426 km/h | 230 kts 265 mph |
| Mmo (max. Mach) | Mach 0.52 | |
| Service Ceiling | 10.180 m | 33.400 ft |
| Range | 2.919 km | 1.576 NM 1.814 mi. |
| Empty Weight | 2.209 kg | 4.870 lbs |
| max. Takeoff Weight | 3.901 kg | 8.600 lbs |
| Wing Span | 13,45 m | 44,1 ft |
| Wing Area | 20,9 m² | 225 ft² |
| Length | 10,93 m | 35,9 ft |
| Height | 3,84 m | 12,6 ft |
| First Flight | 12. Sep. 1978 | |
| Production Status | out of production | |
| Total Production | 236 | |
| Developed from | Cessna 421 Golden Eagle | |
| ICAO Code | C425 | |
| FAA TCDS | A7CE | |
| Data for (Version) | Cessna 425 Conquest I | |
Remarks
The Cessna 425 is a turboprop-powered development of the Cessna 421. The total production of 236 includes 132 Cessna 425 Corsair and 104 Conquest I which has a 400lb higher gross weight.
| Weblinks | Extras |
| Cessna Aircraft Company |
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