Smaller than the 
            DC-8, the trim DC-9 has a distinctive high-level horizontal 
            stabilizer atop the rudder, commonly called a "T" tail. Two engines 
            mounted on the aft fuselage power the aircraft at cruising speeds 
            exceeding 500 mph (800 km/h) and altitudes over 30,000 feet (9,144 
            m).
            Design, development 
            and production of the DC-9 was centred in Long Beach, Calif., at 
            what is now the Long Beach Division of Boeing Commercial Airplanes, 
            where 976 of the twin jets were built during an 18-year production 
            run. The first flight was Feb. 25, 1965; the final DC-9 was 
            delivered in October 1982.
            There are five basic 
            DC-9 versions, designated Series 10, Series 20, Series 30, Series 40 
            and Series 50. Several models in each series provide operators 
            maximum efficiency for diverse combinations of traffic density, 
            cargo volume and route distances to more than 2,000 miles (3,218 
            km). All models use variants of the reliable workhorse Pratt & 
            Whitney JT8D engine.
            
            Series 10: 
            The first in the twinjet family, the fuselage length of the Series 
            10 DC-9 is 104.4 feet (31.8 m), accommodating up to 90 passengers 
            with 600 cubic feet (16.9 m3) of cargo space below the 
            floor. Wingspan is 89.4 feet (27.2 m). Engines can be JT8D-5s or 
            JT8D-7s, with takeoff thrust ratings up to 14,000 pounds.
            
            Series 20: 
            The DC-9 Series 20, although numbered second in the sequence of 
            models, actually is the fourth member of the family. This 
            high-performance version was announced in December 1966, and the 
            first delivery was made in December 1968. The Series 20 is designed 
            for operation from very short runways. It combines the fuselage of 
            the DC-9 Series 10 with a high-lift wing developed for the Series 
            30. Power is provided by two JT8D-9s with 14,500 pounds thrust each, 
            or 15,000-pound JT8D-11s.
            
            Series 30: 
            Fuselage of the Series 30 DC-9, actually second developed, is nearly 
            15 feet longer than the Series 10, at 119.3 feet (36.3 m), providing 
            seats for up to 115 passengers and cargo space to 895 cubic feet 
            (25.3 m3). Series 30 wingspan was increased to 93.3 feet 
            (28.4 m), and a high-lift wing system of leading edge slats gives 
            the Series 30 excellent short-field performance. The first of the 
            type began airline service in February 1967.
            Most of the Series 
            30s are powered by either JT8D-7 or JT8D-9 engines. Others are 
            equipped with JT8D-11 or the JT8D-15, with 15,500 pounds of thrust. 
            The Series 30 is the most widely used member of the DC-9 family, 
            accounting for approximately 60 percent of the entire fleet. 
            
            
            Series 40: 
            To again meet airline demands for a DC-9 with more capacity, the 
            Series 40 was developed with a fuselage length of 125.6 feet (38.3 
            m). Seating is available for up to 125 passengers, 10 more than the 
            popular Series 30s. Below-floor cargo space totals 1,019 cubic feet 
            (28.8 m3). The Series 40 uses the same wing as the Series 
            30. Series 40 engines are JT8D-9s, JT8D-11s or JT8D-15s. The model 
            entered service in March 1968.
            
            Series 50: 
            The fifth and largest DC-9 version is extended to 133.6 feet (40.7 
            m) long, permitting installation of five more rows of seats than the 
            Series 30. Maximum passenger capacity is up to 139, with cargo 
            capacity increased similarly. Wingspan is the same as for the Series 
            30. Engines are either JT8D-15s or JT8D-17s, which are rated at 
            16,000 pounds. Airline operations with the Series 50 began in August 
            1975.
            
            All Models: 
            Common to all versions of the DC-9 are the features that make them 
            ideal for short- and medium-range flights providing direct service 
            between small or large airports. All have built-in boarding stairs 
            for use where jetways are not available. The low ground clearance 
            puts the lower deck cargo bays at waist height, to allow loading and 
            unloading without a conveyor or loading platform. The cockpit is 
            designed for a two-member crew.
            Passenger cabins of 
            the DC-9s are designed for optimum passenger comfort and 
            convenience. Economy class seating is five across -- an arrangement 
            consistently preferred in passenger surveys to the six-across 
            seating in other single-aisle jetliners. A "wide look" interior 
            introduced in 1973 provides a greater feeling of spaciousness than 
            in earlier models and offers enclosed overhead racks for carry-on 
            bags.
            Thirty years after 
            beginning operations and more than a decade after the final aircraft 
            rolled off the assembly line, DC-9s remain a mainstay in many 
            airlines, still building a worldwide reputation for reliability and 
            durability unmatched by any other aircraft. The fleet makes more 
            than 3,500 flights per day, with each aircraft averaging more than 
            five hours of revenue service daily.