McDonnell Douglas MD-90
The McDonnell Douglas MD-90 is a twin-engine, short/medium-range commercial jet airliner seating 172 passengers.
MD-90 | |
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Japan Airlines MD-90-30 on final approach at Tokyo Haneda Airport | |
Role | Narrow-body jet airliner |
National origin | United States |
Manufacturer | McDonnell Douglas Boeing Commercial Airplanes |
First flight | February 22, 1993 |
Introduction | 1995 with Delta Air Lines |
Status | Retired |
Primary users | Delta Air Lines Saudi Arabian Airlines (historical) Japan Airlines (historical) EVA Air (historical) |
Produced | 1993–2000 |
Number built | 116 |
Unit cost | US$41.5–48.5 million |
Developed from | McDonnell Douglas MD-80 |
Variants | McDonnell Douglas MD-94X |
Specifications
2 class seats | 153-158 : 12J@36" + 141/146Y@31-33" |
---|---|
1 class seats | 163-172Y@29-33" |
Cargo | 1,300 cu ft (36.8 m3) ER: 1,177 cu ft (33.3 m3) |
Length | 152.6 ft (46.51 m) |
Fuselage height | 142 in (360.7 cm)[2] |
Fuselage width | 131.6 in (334.3 cm) |
Wing span | 107.8 ft (32.86 m) |
Height | 30.6 ft (9.33 m) |
MTOW | 156,000 lb (70,760 kg) ER: 166,000 lb (75,296 kg) |
Empty weight | 88,200 lb (40,007 kg) ER: 88,400 lb (40,098 kg)[a] |
Max payload | 41,800 lb (18,960 kg) ER: 43,600 lb (19,777 kg) |
Fuel Capacity | 39,128 lb (17,748 kg)[b] |
Turbofans (2×) | 25,000 lbf (111.21 kN) IAE V2525-D5[c] |
VMO | Mach 0.84 (506 kn; 937 km/h) at 27,240 ft (8,303 m)[3] |
Cruise | Mach 0.74 (427 kn; 790 km/h) at 34,777 ft (10,600 m)[4] |
Ceiling | 37,000 ft (11,278 m)[3] |
Range, 153 pax | 2,045 nmi (3,787 km) ER: 2,237 nmi (4,143 km)[d] |
Takeoff | 7,000 ft (2,134 m) at 156,000 lb, ISA, SL[2] |
McDonnell Douglas MD-90 Media
McDonnell Douglas MD-94X
An MD-81 testbed for propfan engines at Farnborough Airshow 1988
China Eastern MD-90-30 showing a bottom view
initial MD-90s EFIS cockpit of Delta Air Lines
Enhanced MD-90s glass cockpit of Saudi Arabian Airlines
International Aero Engines V2500 engine powering the MD-90
References
- ↑ "MD-90". Startup (Boeing). June 1, 2007. http://www.boeing.com/resources/boeingdotcom/company/about_bca/startup/pdf/historical/md90-passenger.pdf.
- ↑ 2.0 2.1 "MD-90-30 airplane characteristics for airport planning" (PDF). Boeing. Oct 2002.
- ↑ 3.0 3.1 "Type Certificate Data Sheet" (PDF). FAA. March 25, 2014. Archived from the original (PDF) on December 28, 2016. Retrieved January 12, 2019.
- ↑ John Bailey (6 December 1989). "Douglas uses MD-80 to speed MD-90". Flight International. https://www.flightglobal.com/pdfarchive/view/1989/1989%20-%203788.html. Retrieved 12 January 2019.