McDonnell Douglas MD-90 - Simple English Wikipedia, the free encyclopedia
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 |
The McDonnell Douglas MD-90 is a twin-engine, short/medium-range commercial jet airliner seating 172 passengers.
![](http://upload.wikimedia.org/wikipedia/commons/thumb/8/80/02142019_Delta_Airlines_MD90_N924DN_KMIA_NASEDIT_%2840237117393%29.jpg/220px-02142019_Delta_Airlines_MD90_N924DN_KMIA_NASEDIT_%2840237117393%29.jpg)
Specifications
[change | change source]2 class seats | 153-158 : 12J@36" + 141/146Y@31-33" |
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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] |
![](http://upload.wikimedia.org/wikipedia/commons/thumb/d/d1/American_Airlines%2C_McDonnell_Douglas_MD-82%2C_N426AA_-_LAX_%2820976375129%29.jpg/220px-American_Airlines%2C_McDonnell_Douglas_MD-82%2C_N426AA_-_LAX_%2820976375129%29.jpg)
References
[change | change source]![](http://upload.wikimedia.org/wikipedia/commons/thumb/7/7c/Allegiant_Airlines_-_Flickr_-_skinnylawyer_%281%29.jpg/220px-Allegiant_Airlines_-_Flickr_-_skinnylawyer_%281%29.jpg)
![](http://upload.wikimedia.org/wikipedia/commons/thumb/d/d3/N949AS_MD-83_Alaska_Airlines_YVR_10JUL04_%2811833233515%29.jpg/220px-N949AS_MD-83_Alaska_Airlines_YVR_10JUL04_%2811833233515%29.jpg)
![](http://upload.wikimedia.org/wikipedia/commons/thumb/2/2e/Hello_MD-90%3B_HB-JIA%40ZRH%3B30.06.2007_473cp_%284292036050%29.jpg/220px-Hello_MD-90%3B_HB-JIA%40ZRH%3B30.06.2007_473cp_%284292036050%29.jpg)
- ↑ "MD-90" (PDF). Startup. Boeing. June 1, 2007.
- ↑ 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. Archived from the original on 2 December 2018. Retrieved 12 January 2019.