Cessna 425 Corsair & Conquest I

Corporate Aircraft

Cessna 425 Corsair/Conquest I © Roger Oldfield
Photo ©: Roger Oldfield (Photos at airliners.net)
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.
Crew1 / 2
Propulsion2 Turboprop Engines
Engine ModelPratt & Whitney Canada PT6A-112
Engine Power (each)373 kW500 shp
Speed426 km/h230 kts
  265 mph
Mmo (max. Mach)Mach 0.52
Service Ceiling10.180 m33.400 ft
Range2.919 km1.576 NM
1.814 mi.
Empty Weight2.209 kg4.870 lbs
max. Takeoff Weight3.901 kg8.600 lbs
Wing Span13,45 m44 ft 2 in
Wing Area20,9 m225 ft
Length10,93 m35 ft 10 in
Height3,84 m12 ft 7 in
First Flight12. Sep. 1978
Production Statusout of production
Total Production236
Developed fromCessna 421 Golden Eagle
ICAO CodeC425
Data for (Version)Cessna 425 Conquest I