McDonnell Douglas MD-90

· McDonnell Douglas · 2 × IAE V2500

Airplanes

Length

46.5125 m

Flat Wing Span

32.8574 m

Height

9.3269 m

Max Seating

153

Max Ceiling

11277.6 m

Number of Engines

Aircraft Engine

First Flight

1993-02-22

Entry Into service

1995-01-01

Number Built

116

Maximum Take-Off Weight

70.7604 t (paragliders: kg)

Maximum Range

3787.34 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
McDonnell Douglas MD-90	70.7604	3787.34

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Boeing 7J7	General Electric GE36	43.5864	36.8808		Compare
727-200	Pratt & Whitney JT8D	40.5384	32.9184	106	Compare
Antonov An-180	Progress D-27	40.9	35.83		Compare
Ilyushin Il-276	Aviadvigatel PD-14	37.7	35.5	70	Compare
Fokker F.29		39.41	32.88	138	Compare
Yakovlev Yak-46	Progress D-27	41	35.5		Compare

All data (25 fields)

Name: McDonnell Douglas MD-90
Manufacturer: McDonnell Douglas
Description: 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: McDonnell Douglas
Type: Narrow-body jet airliner
Length (m): 46.5125
Height (m): 9.3269
Max Seating: 153
Max Ceiling (m): 11277.6
Capacity Description: 153–158: 12J@36" + 141/146Y@31-33"
National Origin: United States of America
Number Built: 116
Powerplant Description: IAE V2525-D5 or V2528-D5
Primary Users: Delta Air Lines (historical), Saudi Arabian Airlines (historical) , Japan Airlines (historical) , NASA (X-66)
Status: Retired from commercial use
Wikipedia Article (URL): en.wikipedia.org/wiki/McDonnell_Douglas_MD-90
Flat Wing Span (m): 32.8574
Wake Category: M
Aircraft Engine: IAE V2500
Number of Engines: 2