C425 Aircraft - Cessna 425 Corsair VH-PTH² (c/n 425-0044 - ex N555BE) at Bankstown, New South Wales in February 1982 (David S. Eyre)
In 1980, the Cessna line was introduced with the Cessna 425 Corsair. Based on the Model 421 Golden Eagle airframe, powered by Corsair Pratt & Whitney PT6A turboprop engines. Construction of the prototype began on January 30, 1978, and the aircraft first flew on September 12, 1978. The cockpit seats two (side-by-side with dual controls), and the cabin seats four passengers. Room. As an option, the front passenger seats can be installed rearward, and the seventh and eighth seats can be installed facing forward, for a total of ten. A luggage compartment was provided in the bow, with an external door with a load capacity of 272 kg (600 lb) and a load capacity of 227 kg (500 lb) at the rear.
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Later, in 1982, the name Corsair was changed to Conquest I. During that time, 132 Corsairs were delivered, and starting with aircraft number 119, new avionics were introduced, as well as additional parts for the cockpit, furniture and interior. . Results are available. In 1983, the Conquest II (Model 441) appeared with 474 kW (635 hp) Garrett TPE 331-8-403S turboprops, while the Conquest I had 336 kW Pratt & Whitney of Canada PT6A-112 turboprops (450 hp).
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A small number of 425s were registered in this region, including: VH-ULX (c/n 425-0124 - formerly N6882M), registered from December 1988 to August 2000; VH-PTH (c/n 425-0044) registered when exported to USA from December 1981 to July 1983; VH-HBM (c/n 425-0151), registered from May 1982 to June 1989, when it was also exported to the United States; VH-JEC (c/n 425-183), first registered in June 1985, became VH-EGS in June 1986; and VH-EGR (c/n 425-0195), registered 30 August 1988, served in Royal Flying Doctor service before being exported to the US in March 1999. The Cessna 425 was known as the Corsair and later as the Conquest I. , American turboprop twin-engine light multipurpose monoplane. It was produced from 1980 to 1986, designed as an easy-to-fly and easy-to-configure Cessna turboprop aircraft.
The Cessna 425 was introduced in 1980 to compete with the Beechcraft King Air. It was a development of the Cessna 421 powered by two 450 hp Pratt and Whitney PD6 engines. The plane is designed to be very easy to fly, and critics noted its spacious cabin with large windows for better visibility and comfortable seats.
In September 1978, the first prototype made its first flight, and in mid-1980 it was certified by the Federal Aviation Administration. Originally called the Corsair, it was renamed the Conquest I in 1983 due to customer requests for more cabin space and an increase in maximum takeoff weight. The horizontal stabilizer used a significant dihedral angle to reduce the effect of water on the leg, and the retractable landing gear was reinforced to handle the increased landing and tilt weight.
The Cessna 425 Conquest I is a light-pressure aircraft designed as a cantilever low-wing aircraft with a conventional tail and aluminum main body. It has an external length of 10.92 meters, a height of 3.84 meters and a fuselage diameter of 1.55 meters. Wingspan 13.4 meters, wing area 20.90 square meters, wheelbase 3.2 meters. The aircraft is equipped with various seating configurations, usually for six to seven passengers. The cabin is 3.2 meters long, 1.3 meters high and 1.4 meters wide.
Propellers, Nosewheel Undercarriage And Windshield Of A Cessna 425 Corsair/conquest 1 Parked Stock Photo
Most Conquests were originally equipped with the Cessna 1000 Series avionics system, which included dual communications radios, dual navigation, dual transponders, dual automatic direction finder (ADF), dual distance measuring instrument (DME) and autopilot. The aircraft is equipped with Collins avionics including VHF 20A dual link, VIR-30A dual navigation system, ADF 60, DME 40, flight instrument system, horizontal situation indicator, Sperry 1000 autopilot and WXR-300 weather radar systems.
Conquest I is powered by two 450 horsepower PT6A-112 engines, each driving Hartzell 9910438-1 or McCauley 9910535-1 three-blade constant speed propellers. The aircraft has a maximum speed of 265 knots and a range of 1,646 nautical miles.
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