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