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Cessna 425 Corsair & Conquest I

Cessna 425 Corsair/Conquest I © Roger Oldfield
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.

Crew1 / 2
Passengers4-6
 
Propulsion2 Turboprop Engines
Engine ModelPratt & Whitney Canada PT6A-112
Engine Power (each)336 kW450 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 m44,1 ft
Wing Area20,9 m225 ft
Length10,93 m35,9 ft
Height3,84 m12,6 ft
 
First Flight12. Sep. 1978
Production Statusout of production
Total Production236
Developed fromCessna 421 Golden Eagle
 
ICAO CodeC425
FAA TCDSA7CE
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.


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Cessna Aircraft Company

 

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