McDonnell Douglas MD-90
Airliner
Photo ©: Karsten Palt
The McDonnell Douglas MD-90 is a twin-engined short-to-medium-range narrowbody airliner with a capacity of maximum 172 passengers produced by the American manufacturer McDonnell Douglas.
The McDonnell Douglas MD-90 is a improved and enlarged development of the
McDonnell Douglas MD-80 and was produced in the versions MD-90-30 & MD-90-30ER only. The engine options are
International Aero Engines (IAE) V2525-D5 (see above) or V2528-D5 (124,6 kn / 28000 lbf). The shortened variant
MD-95 was renamed to
Boeing 717-200 after the merger of McDonnell Douglas and Boeing.
| Crew | 2 |
| Passengers | 153, max. 172 |
| Propulsion | 2 Turbofan Engines |
| Engine Model | IAE International Aero Engines V2525-D5 |
| Engine Power (each) | 111,2 kN | 25000 lbf |
| Speed | 900 km/h | 486 kts
559 mph |
| Service Ceiling | 11.278 m | 37.000 ft |
| Range | 3.860 km | 2.084 NM
2.398 mi. |
| Empty Weight | 39.994 kg | 88.171 lbs |
| max. Takeoff Weight | 70.760 kg | 156.000 lbs |
| max. Landing Weight | 64.410 kg | 142.000 lbs |
| Wing Span | 32,87 m | 107 ft 10 in |
| Wing Area | 112,3 m² | 1209 ft² |
| Length | 46,50 m | 152 ft 7 in |
| Height | 9,40 m | 30 ft 10 in |
| First Flight | 22.02.1993 |
| Production Status | out of production |
| Production Range | 1993-2000 |
| Total Production | 170 |
| Developed from | McDonnell Douglas MD-80 |
| ICAO Code | MD90 |
| IATA Code | M90 |
| FAA TCDS | A6WE |
| Data for (Version) | McDonnell Douglas MD-90-30 |
| Variants | MD-90-30, MD-90-30ER |
