X-Plane 11 EGKK to LEMD Rotate MD 80 Landing
The McDonnell Douglas MD-80 is a series of single-aisle airliners developed by McDonnell Douglas from the earlier DC-9. Stretched, heavier, and with higher bypass Pratt & Whitney JT8D-200 engines, the DC-9 Series 80 was launched in October 1977. It made its first flight on October 18, 1979 and was certified on August 25, 1980. It was first delivered to launch customer Swissair on September 13, 1980, which introduced it into commercial service on October 10, 1980.
Keeping the five-abreast coach seating, longer variants are stretched by 14 ft (4.3 m) from the DC-9-50 and have a 28% larger wing. The long variants (MD-81/82/83/88) are 148 ft (45.1 m) long to seat 155 passengers in coach and, with varying weights, can cover up to 2,550 nmi (4,720 km). The later MD-88 has a modern cockpit with EFIS displays. The MD-87 is 17 ft (5.3 m) shorter for 130 passengers in economy and has a range up to 2,900 nmi (5,400 km).
It competed with the Boeing 737 Classic and the Airbus A320. Introduced in 1995, the MD-90 is a further stretch powered by IAE V2500 high-bypass turbofans, while the shorter MD-95, the later Boeing 717, was powered by Rolls-Royce BR715 engines. MD-80 production ended in 1999 after 1,191 were built.
Douglas Aircraft developed the DC-9 in the 1960s as a short-range companion to their larger DC-8.[2] The DC-9 was an all-new design, using two rear fuselage-mounted turbofan engines, and a T-tail. The DC-9 has a narrow-body fuselage design with five-abreast seating, and holds 80 to 135 passengers depending on seating arrangement and aircraft version.
The DC-9 family was produced in 2441 units: 976 DC-9s, 1191 MD-80s, 116 MD-90s and 155 Boeing 717s.[3]
MD-80 series
The development of MD-80 series began in the 1970s as a lengthened, growth version of the DC-9-50, with a higher maximum take-off weight (MTOW) and a higher fuel capacity. Availability of newer versions of the Pratt & Whitney JT8D engine with higher bypass ratios drove early studies including designs known as Series 55, Series 50 (refanned Super Stretch), and Series 60. The design effort focused on the Series 55 in August 1977. With the projected entry into service in 1980, the design was marketed as the "DC-9 Series 80". Swissair launched the Series 80 in October 1977 with an order for 15 plus an option for five.[2]
The MD-80 is a mid-size, medium-range airliner. The series featured a fuselage 14 ft 3 in (4.34 m) longer than the DC-9-50. The DC-9's wing design was enlarged by adding sections at the wing root and tip for a 28% larger wing. It was the second generation of the DC-9, originally called the DC-9-80 and the DC-9 Super 80.[4] It has two rear fuselage-mounted turbofan engines, small, highly efficient wings, and a T-tail. The aircraft has five-abreast seating in the coach class. The aircraft series was designed for frequent, short-haul flights for 130 to 172 passengers depending on airplane version and seating arrangement.
The MD-80 versions have cockpit, avionics and aerodynamic upgrades along with the more powerful, more efficient and quieter JT8D-200 series engines, which are a significant upgrade over the smaller JT8D-15, -17, -11, and -9 series. The MD-80 series aircraft also have longer fuselages than their earlier DC-9 counterparts, as well as longer range. Some customers, such as American Airlines, still refer to the planes in fleet documentation as "Super 80". Comparable airliners to the MD-80 series include the Boeing 737-400 and Airbus A320.
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