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However, its development was postponed by the recession of the early 1980s.
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The DC-9-90 was designed to meet the needs of the newly deregulated American airline industry. Seating up to 117 passengers, the DC-9-90 was to be equipped with the DC-9's wing with 2 ft (0.61 m) tip extensions, rather than the more heavily modified increased area of the MD-80.
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The aircraft was proposed with a 17,000 lbf (76 kN) thrust version of the JT8D-200 series engine, although the CFM International CFM56-3 was also considered. Dubbed the DC-9-90, it was revealed in February 1983 and was to be some 25 ft 4 in (7.72 m) shorter than the DC-9-81, giving it an overall length of 122 ft 6 in (37.34 m). During the early 1980s, as production of the DC-9 family moved away from the smaller Series 30 towards the larger Super 80 (later redesignated MD-80) variants, McDonnell Douglas proposed a smaller version of the DC-9 to fill the gap left by the DC-9-30. The MD-95 traces its history back to 1983 when McDonnell Douglas outlined a study named the DC-9-90. A total of 116 MD-90 airliners were delivered. The MD-90 was longer and featured a glass cockpit (electronic instrumentation) and more powerful, quieter, fuel-efficient IAE V2525-D5 engines, with the option of upgrading to an IAE V2528 engine. It was launched in 1989 and first flew in 1993. The MD-90 was developed from the MD-80 series. It was a lengthened DC-9-50 with a higher maximum take-off weight (MTOW) and higher fuel capacity, as well as next-generation Pratt and Whitney JT8D-200 series engines and an improved wing design. The McDonnell Douglas MD-80 series, the second generation of the DC-9, began airline service in 1980. When production ended in 1982, a total of 976 DC-9s had been produced. The DC-9's maiden flight was in 1965 and entered airline service later that year. The DC-9 was an all-new design, using two rear fuselage-mounted Pratt & Whitney JT8D turbofan engines a small, efficient wing and a T-tail. Background ĭouglas Aircraft launched the DC-9, a short- range companion to its larger four-engine DC-8, in 1963. The 717 retains the five-abreast seating from the DC-9.
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As of July 2018, 148 Boeing 717 aircraft were still in service. Production of the Boeing 717 ceased in May 2006 after 156 were built. With McDonnell Douglas and Boeing merging in 1997 prior to production, the airliner entered service in 1999 as the Boeing 717. The first order for the airliner was placed with McDonnell Douglas in October 1995 by ValuJet Airlines (later AirTran Airways). It is powered by two Rolls-Royce BR715 turbofan engines mounted at the rear of the fuselage.
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Capable of seating up to 134 passengers, the 717 has a design range of 2,060 nautical miles (3,820 km). The airliner was designed and originally marketed by McDonnell Douglas as the MD-95, a derivative of the DC-9 family. The Boeing 717 is an American twin-engine, single-aisle jet airliner, developed for the 100-seat market. For the earlier jetliner temporarily coded as the Boeing 717, see Boeing 720.Ī Boeing 717 of Delta Air Lines, its largest operator For the 1950s military transport, see Boeing Model 717. This article is about the airliner derived from the McDonnell Douglas DC-9.