Cessna 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.
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.
Propulsion | 2 Turboprop Engines |
Engine Model | Pratt & Whitney Canada PT6A-112 |
Engine Power (each) | 373 kW | 500 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 ft 2 in |
Wing Area | 20,9 m² | 225 ft² |
Length | 10,93 m | 35 ft 10 in |
Height | 3,84 m | 12 ft 7 in |
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 |