In 1983, the manufacturing company renamed the Model 441 as the Conquest II. On August 19, 1977, it was awarded the Federal Aviation Administration type certification. The aircraft can seat eight to ten passengers and one or two pilots.īy 1975, the prototype was further developed and evolved into a turboprop-powered aircraft, designated as the Model 441. The cabin length is 3.9 meters, the cabin height is 1.3 meters, and the cabin width is 1.4 meters. The fuselage diameter is 1.6 meters, the wingspan is 15 meters, and the wing area is 23.56 square meters. It has an exterior length of 11.9 meters, an exterior height of 2.2 meters, a tail height of 4 meters, and a fuselage diameter of 1.6 meters. The Model 435 has the same dimensions as the 441 Conquest II. The powerplant is also equipped with three-bladed propellers. Each engine produces a maximum thrust of over 300 horsepower. It is a six-cylinder, horizontally opposed engine with an overhead valve train, TCM fuel injection, and an air-cooling system. A prototype the same with the 441, the Model 435 was intended to be powered with GTSIO-520 engines by Teledyne Continental Motors. The initial design from 1972 for the Cessna 441 Conquest II was designated as the Model 435. Conquest II Production and Development Model 435
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