McDonnell Douglas

McDonnell Douglas MD-80 "Mad Dog"Maddog

McDonnell Douglas MD-80 • Jet airliner

Built 1988–2000 · end of production 2000 · in service: 0 · retired from airline service 2014

  • First flightOctober 18, 1979
  • IntroductionOctober 18, 1979
  • StatusOperationel
  • Number built1,191

History

The McDonnell Douglas MD-80 is a series of five-abreast single-aisle airliners developed by McDonnell Douglas. It was produced by the developer company until August 1997 and then by Boeing Commercial Airplanes. The MD-80 was the second generation of the DC-9 family, originally designated as the DC-9-80 (DC-9 Series 80) and later stylized as the DC-9 Super 80 (Super 80 for short). With a stretched, enlarged wing and powered by higher bypass Pratt & Whitney JT8D-200 engines, the aircraft program was launched in October 1977. The MD-80 made its first flight on October 18, 1979, and was certified on August 25, 1980. The first airliner was delivered to launch customer Swissair on September 13, 1980, which introduced it into service on October 10, 1980.

Keeping the same fuselage cross-section, longer variants are stretched by up to 14 ft (4.3 m) from the DC-9-50 and have a 28% larger wing.

The larger 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 nautical miles [nmi] (4,720 km; 2,930 mi). The later MD-88 has a modern cockpit with electronic flight instrument system (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; 3,300 mi).

The MD-80 series initially competed with the Boeing 737 Classic and then also with the Airbus A320ceo family. Its successor, introduced in 1995, the MD-90, was a further stretch powered by IAE V2500 high-bypass turbofans, while the shorter MD-95, later known as the Boeing 717, was powered by Rolls-Royce BR715 engines. Production ended in 1999 after 1,191 MD-80s were delivered, of which 116 aircraft remain in service as of August 2022.

Technical data

Specifications

01

Crew & dimensions

Crew
2
Length
147 ft 10 in (45.06 m)
Wingspan
107 ft 8 in (32.82 m) span, 1,209 sq ft (112.3 m2) area, aspect ratio: 9.6
Height
29 ft 7 in (9.02 m
02

Performance

Maximum speed
Mach 0.8 (472 kn; 873 km/h; 543 mph)
Range
2,400–2,900 nmi (4,400–5,400 km; 2,800–3,300 mi)
03

Powerplant

Powerplant
2 jet engines
04

Developed from

Developed from
McDonnell Douglas DC-10