McDonnell Douglas MD-80: Difference between revisions
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== Variants == | == Variants == | ||
There are two variants modeled in [[FlightGear]]: | |||
* '''MD-83 (DC-9-83):''' long-range version with 21,000 lb thrust JT8D-219 engines. | * '''MD-83 (DC-9-83):''' long-range version with 21,000 lb thrust JT8D-219 engines. | ||
* "[[MD-81]]" Normal version developed from the DC-9. Also with JTD8D-219' s. | |||
== Development status/Issues/Todo == | == Development status/Issues/Todo == | ||
'''Inside:''' | '''Inside:''' | ||
Revision as of 18:47, 28 January 2013
| This aircraft article is a stub. You can help the wiki by expanding it. |
This includes the following variants: MD-80, MD-83
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| Type | Airliner |
|---|---|
| Author(s) | Adam Smith |
| FDM | JSBSim |
| Status | Under development |
The McDonnell Douglas MD-80 series are twin-engine, medium-range, single-aisle commercial jet airliners. The MD-80 aircraft were lengthened and updated from the DC-9. The MD-80 series can seat from 130 up to 172 passengers depending on variant and seating arrangement.
The MD-80 series was introduced commercially in October 1980 by Swissair. The MD-80 series was followed into service in modified form by the MD-90 in 1995 and the MD-95/Boeing 717 in 1999.
Variants
There are two variants modeled in FlightGear:
- MD-83 (DC-9-83): long-range version with 21,000 lb thrust JT8D-219 engines.
- "MD-81" Normal version developed from the DC-9. Also with JTD8D-219' s.
Development status/Issues/Todo
Inside:
- No 3D cockpit
External links
- Model description in Adams hangar
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