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T-50 in flight. In 1939, three years after Clyde Cessna retired, the Cessna T-50 made its first flight, becoming the company's first twin-engine airplane, and its first retractable undercarriage airplane. The prototype T-50 first flew on 26 March 1939, [1] and was issued Approved Type Certificate 722 on 24 March 1940. [2]
Cessna T-50 [b] 1939 5,422 Twin piston engine monoplane utility airplane Cessna 120: ... Cessna 650 Citation VI: 1991 39 Twin jet engine monoplane business airplane
Using the same basic design as the larger Cessna AT-17 Bobcat, the new CW-25 was designed to simulate the demands of multi-engined operations. The design featured a small layout, grouping two Lycoming R-680-9 radial engines forward and using a retractable tailwheel landing gear to achieve the performance necessary to meet the requirements of an ...
Viewed from below, showing wing sweep The 650 has a T-tail and two turbofans. In 1974, Cessna studied a long range model 700 stretch of its original Citation I powered by three JT15Ds called Citation III, with a 17,500 lb gross weight, an 8,000 lb empty weight and a 7,500 lb fuel capacity leaving 2,000 lb for the occupants, and targeting 1978 deliveries. [3]
First-generation American subcompacts, left to right: AMC Gremlin, Ford Pinto, Chevrolet Vega. American automakers had first countered imports such as the Volkswagen Beetle with compact cars including the Ford Falcon, Ford Maverick, Chevrolet Corvair and Plymouth Valiant, although these cars featured six-cylinder engines and comprised a larger vehicle class.
The Academy bars winners from profiting off the sales of their Oscar statues, in an effort "to preserve the integrity of the Oscar symbol," according to the organization's website.
They are powered by a 650 cc water-cooled 4-stroke twin engine. The manufacturer states the vehicles get up to 60 miles per gallon, [2] [3] although some dealers have suggested 40–60 miles per gallon is a more realistic figure. Both vehicles are manufactured by Jiangsu Sandi Motorcycle Co Ltd. [4] Wildfire WF650-T
An all new design, the Citation III had a 312 sq ft (29 m 2) swept wing for a 22,000 lb (10 t) MTOW and a 2,350 nmi (4,350 km) range, a T-tail and two 3,650–4,080 lbf (16.2–18.1 kN) TFE731 turbofans. Its fuselage cross section and cockpit were carried over and used in the later Citation X, Citation Excel and Citation Sovereign.
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