| Manufacturer |
Boeing |
McDonnell Douglas |
| Description |
The Boeing 7J7 was an American short- to medium-range airliner proposed by American aircraft manufacturer Boeing in the 1980s. |
The McDonnell Douglas (later Boeing) MD-90 is a retired American five-abreast single-aisle airliner developed by McDonnell Douglas from the earlier MD-80. |
| ICAO Code |
|
MD90 |
| First Flight |
|
1993-02-22 |
| Entry Into service |
|
1995-01-01 |
| Production End |
|
2000-01-01 |
| Service End |
|
2020-06-02 |
| Designer |
Boeing |
McDonnell Douglas |
| Type |
|
Narrow-body jet airliner |
| Length (m) |
43.5864 |
46.5125 |
| Height (m) |
10.668 |
9.3269 |
| Max Seating |
|
153 |
| Max Ceiling (m) |
|
11277.6 |
| Capacity Description |
147 in standard 2+2+2 seating; 166 in high-density 2+3+2 seating |
153–158: 12J@36" + 141/146Y@31-33" |
| Max Mach (Mach) |
0.83 |
|
| National Origin |
United States of America |
United States of America |
| Number Built |
0 |
116 |
| Powerplant Description |
2 × General Electric GE36-C25 propfans |
IAE V2525-D5 or V2528-D5 |
| Primary Users |
|
Delta Air Lines (historical), Saudi Arabian Airlines (historical) , Japan Airlines (historical) , NASA (X-66) |
| Status |
Developed, never built |
Retired from commercial use |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Boeing_7J7 |
en.wikipedia.org/wiki/McDonnell_Douglas_MD-90 |
| Flat Wing Span (m) |
36.8808 |
32.8574 |
| Flat Wing Area (m²) |
139.1688 |
|
| Flat Wing Aspect Ratio |
10.3 |
|
| Wake Category |
|
M |
| Aircraft Engine |
General Electric GE36 |
IAE V2500 |
| Number of Engines |
2 |
2 |