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IH Cub Cadet was a premium line of small tractors, established in 1960 as part of International Harvester. The IH Cub Cadet was a new line of heavy-duty small tractors using components from the previous Cub series tractors. [1] Cub Cadet loader. During the 1960s, IH Cub Cadet was marketed to the owners of rural homes with large lawns and ...
In 1981 the Cub Cadet product line was acquired from International Harvester, and the White Outdoor Products Company was acquired from the old White Motor Company. In 1985 the company's Martin, Tennessee plant began operation, and Arnold Corporation was acquired. In 1986 Aircap Industries in Tupelo, Mississippi was acquired.
The Cub was initially designated the Farmall X, and was to use a two-cylinder engine. [1] Development started in July, 1943, changing to a four-cylinder engine. A prototype was built by December 1944. In September 1945, it became the Farmall Cub. [2] The two major variations of the Cub were the "Standard Cub" and the "Lo-Boy Cub" (or "Cub Lo-Boy").
In another June 2016 flight review of the CC19-180, Paul Bertorelli of AVweb said, "The XCub has aluminum rather than steel or the Cub’s traditional bungee gear. This was a revelation for me because aluminum does a nice job of absorbing surplus touchdown energy; it’s far less energetic than steel or those blasted bungees in returning ...
The Leyland Tiger, also known as the B43, [1] was a mid-engined bus and coach chassis manufactured by Leyland between 1981 and 1992. [2] This name had previously been used for a front-engined bus built between 1927 and 1968.
PA-18-125 Super Cub Variant to replace the PA-18-95 with flaps and horn-balanced elevators and a 125 hp Lycoming O-290-D piston engine and either wood or metal controllable-pitch propeller. [5] PA-18-135 Super Cub Variant with a 135 hp Lycoming O-290-D piston engine and fitted with two wing tanks as standard. [5] PA-18-150 PA-18-150 Super Cub
Data from Jane's All the World's Aircraft 1948 General characteristics Crew: one, pilot Capacity: two passengers Length: 22 ft 10 in (6.96 m) Wingspan: 35 ft 5 + 1 ⁄ 2 in (10.81 m) Height: 6 ft 10 in (2.08 m) Wing area: 179.3 sq ft (16.66 m 2) Empty weight: 950 lb (431 kg) Gross weight: 1,750 lb (794 kg) Max takeoff weight: 1,753 lb (795 kg) Fuel capacity: 38 US gal (32 imp gal; 140 L ...
Ryan PT-22 Recruit instrument panel PT-22 Military version of the Model ST.3KR powered by a 160 hp R-540-1, 1,023 built. PT-22A Model ST-3S twin-float seaplanes ordered by the Netherlands Navy powered by 160 hp Menasco D4B, ordered cancelled and completed for the United States Army Air Corps with 160 hp R-540-1 engines, 25 built.