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Contents • • • • • • • • • • • • • • • • • • • • • • • • • • • Design and development [ ] Origins [ ] During the 1950s studied a short- to medium-range airliner to complement their higher capacity, long range. (DC stands for Douglas Commercial.) A medium-range four-engine Model 2067 was studied but it did not receive enough interest from airlines and it was abandoned. In 1960, Douglas signed a two-year contract with for technical cooperation.

Douglas would market and support the and produce a licensed version if airlines ordered large numbers. None were ordered and Douglas returned to its design studies after the cooperation deal expired.

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(NWA) DC-9 T-tail at In 1962, design studies were underway. Euc ieena for mac. The first version seated 63 passengers and had a gross weight of 69,000 lb (31,300 kg). This design was changed into what would be the initial DC-9 variant.

Douglas gave approval to produce the DC-9 on April 8, 1963. Unlike the competing but larger, which used as many components as possible, the DC-9 was an all-new design. The DC-9 has two rear-mounted engines, relatively small, efficient wings, and a. The DC-9's takeoff weight was limited to 80,000 lb (36,300 kg) for a two-person flight crew by regulations at the time.

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DC-9 aircraft have five seats across for economy seating. The airplane seats 80 to 135 passengers depending on version and seating arrangement. The DC-9 was designed for short to medium routes, often to smaller airports with shorter runways and less ground infrastructure than the major airports being served by larger designs like the Boeing 707 and Douglas DC-8. Accessibility and short field characteristics were called for.

Turnarounds were simplified by built-in airstairs, including one in the tail, which shortened boarding and deplaning times. The tail-mounted engine design facilitated a clean wing without engine pods, which had numerous advantages. For example, could be longer, unimpeded by pods on the leading edge and engine blast concerns on the trailing edge. This simplified design improved airflow at low speeds and enabled lower takeoff and approach speeds, thus lowering field length requirements and keeping wing structure light. The second advantage of the tail-mounted engines was the reduction in from ingested debris from runways and aprons. However, with this position, the engines could ingest ice streaming off the wing roots.

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Third, the absence of engines in underslung pods allowed a reduction in fuselage ground clearance, making the aircraft more accessible to baggage handlers and passengers. The problem of, revealed by the loss of the prototype in 1963, was overcome through various changes, including the introduction of, small surfaces beneath the wing's leading edge used to control airflow and increase low speed lift.

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Production [ ]. A DC-9 in 2006 The first DC-9, a production model, flew on February 25, 1965. The second DC-9 flew a few weeks later, with a test fleet of five aircraft flying by July. This allowed the initial Series 10 to gain on November 23, 1965, and to enter service with on December 8. The DC-9 was always intended to be available in multiple versions to suit customer requirements, The first stretched version, the Series 30, with a longer fuselage and extended wing tips, flew on August 1, 1966, entering service with in 1967. The initial Series 10 would be followed by the improved,, and variants.

This entry was posted on 23.09.2016.