McDonnell Douglas MD-80
Jump to navigation
Jump to search
This aircraft article is a stub. You can help the wiki by expanding it. |
![]() | |
---|---|
![]() The MD-80 | |
Type | Airliner |
Configuration | Low wing aircraft, Monoplane aircraft, Retractable gear aircraft, Tricycle landing gear aircraft |
Propulsion | Twinjet (Jet aircraft, Twin-engine aircraft) |
Manufacturer | McDonnell Douglas Corporation |
Author(s) |
|
FDM | JSBSim |
Status | Advanced production |
FDM |
![]() |
Systems |
![]() |
Cockpit |
![]() |
Model |
![]() |
Supports |
![]() ![]() |
Development | |
Repository |
![]() |
Download |
![]() |
Forum |
![]() |
|
This includes the following variants: MD-88 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.
This aircraft is equipped with IT-AUTOFLIGHT.
Development status/Issues/Todo
Inside:
- Overhead panel
- General stuff
|