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Cessna’s Conquest II is one of the more easier transitions from multiengine to turbine power aircraft for an instrument-rated pilot. The airplane was born from the 400-series line of twin Cessnas, known for their easygoing flight maneuvers, comfortable cabins, and generous baggage areas.
The Cessna 425 Conquest I is a light, pressurized aircraft configured as a cantilever low-wing monoplane with a conventional tail and an aluminum monocoque airframe. It has an exterior length of 10.92 meters, a height of 3.84 meters, and a fuselage diameter of 1.55 meters.
The Cessna 441 Conquest II is the first turboprop powered aircraft designed by Cessna and was meant to fill the gap between their jets and piston-engined aircraft. It was developed in November 1974, with the first aircraft delivered in September 1977. It is a pressurized, 8–9 passenger turbine development of the Cessna 404 Titan.
The Cessna Conquest I is a light, pressurized, twin-turboprop business aircraft configured as a cantilever low-wing monoplane with a conventional tail. The horizontal stabilizer employs a large dihedral angle in order to minimize its exposure to prop wash.
1 Φεβ 2019 · Conquest IIs were delivered with the 800-shaft-horsepower (flat rated to 635 shaft horsepower) -8 version of the TPE-331, which delivered 290 KTAS in the high teens. A -10-equipped 441 can exceed 310 KTAS at Flight Level 290.
Conquest I, CE-425; TO (Sea Level, ISA Temp) 2,490: TO (5000′, @25C) 3,505: Hot/High WAT: N/A: NBAA IFR Ranges V2 @ SL ISA, MTOW 1,275 N/A VREF: N/A: Landing Distance with 4 Passengers: N/A: Climb Conquest I, CE-425; Time to Climb/Alt: N/A: Engine Out Rate fpm: 357: FAR 25 Engine-Out Grad (ft/nm) 193: Ceilings (ft) Conquest I, CE-425 ...
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.
