Draft:McDonnell Douglas MD-90-10
| Submission declined on 7 February 2024 by Alalch E. (talk). Thank you for your submission, but the subject of this article already exists in Wikipedia. You can find it and improve it at McDonnell Douglas MD-90 instead.
Where to get help
How to improve a draft
You can also browse Wikipedia:Featured articles and Wikipedia:Good articles to find examples of Wikipedia's best writing on topics similar to your proposed article. Improving your odds of a speedy review To improve your odds of a faster review, tag your draft with relevant WikiProject tags using the button below. This will let reviewers know a new draft has been submitted in their area of interest. For instance, if you wrote about a female astronomer, you would want to add the Biography, Astronomy, and Women scientists tags. Editor resources
|  |
Comment: See McDonnell Douglas MD-90#Proposed variants. This should not be a separate article per WP:NOPAGE and WP:MERGEREASON. Any information found here and not there can be merged from here to there. —Alalch E. 09:03, 7 February 2024 (UTC)
| McDonnell Douglas MD-90-10 | |
|---|---|
| Role | Narrow-body jet airliner |
| National origin | United States |
| Manufacturer | McDonnell Douglas |
| Status | Never built |
| Developed from | McDonnell Douglas MD-80 |
The McDonnell Douglas MD-90-10 was a proposed variant of the McDonnell Douglas MD-90 aircraft that was meant to be built by McDonnell Douglas. However, it was never built.[1]
Design[edit]
The McDonnell Douglas MD-90-10 was designed to be a shorter variant with the same length as the MD-87, carrying from 114 passengers in a three-class layout to 139 passengers in a high-density configuration.[1]
It was designed to have a maximum takeoff weight (MTOW) of 69.49 short tons (63,040 kilograms; 63,040,000 grams; 63.04 tonnes; 138,980 pounds) and a range of 2,410 nautical miles (2,770 miles; 4.46×109 millimetres; 176,000,000 inches; 446,000,000 centimetres; 4,460,000 metres; 4,460 kilometres) with fuel reserves.[1]
The MD-90-10's engine thrust would be 22,000 lbf (99 kN).[2]
References[edit]
- ^ a b c "MD-90 family will include 180-seater 40 variant" (PDF). Technical: Air Transport. Flight International. December 12, 1989. p. 16. Archived (PDF) from the original on 2017-12-07.
- ^ "Commercial aircraft of the world". Flight International. September 4–10, 1991. p. 62.[dead link]