McDonnell Douglas MD-90

Douglas/McDonnell Douglas

ICAOMD90IATAM90
McDonnell Douglas MD-90 aircraft
Douglas/McDonnell DouglasMcDonnell Douglas MD-90
Photo: Quintin Soloviev · CC BY 4.0 · Modified

About

The McDonnell Douglas MD-90 represents a major modernization of the MD-80 design, featuring new-generation IAE V2500 turbofan engines for dramatically improved fuel efficiency and noise reduction. Introduced in 1994, it retained the 45.06-meter fuselage seating 153-172 passengers but replaced the venerable JT8D engines with V2500-D5 turbofans producing 111 kN (25,000 lbf) thrust each. The modern high-bypass engines reduced fuel consumption by 25%, cut noise levels significantly, and extended range to 4,074 km (2,200 NM). The MD-90 also featured an advanced EFIS glass cockpit, improved wing design, and enhanced flight controls. Delta Air Lines became the launch customer and largest operator with 16 aircraft. However, the MD-90 faced fierce competition from the Boeing 737-800 and Airbus A320 family, which offered similar performance with greater market acceptance. Boeing's 1997 acquisition of McDonnell Douglas further limited MD-90 marketing. Only 116 MD-90s were built before production ended in 2000. China's airlines operated the majority (over 50 examples), where they continued reliable service through the 2010s. The MD-90 proved the DC-9 design's enduring potential but arrived too late to challenge established competitors.

Weightscompared to Boeing 757-300

MRW (Maximum Ramp Weight)

71,214kg
0
50k
100k
124k

MTOW (Maximum Takeoff Weight)

70,760kg
0
50k
100k
124k

MLW (Maximum Landing Weight)

64,410kg
0
50k
102k

MZFW (Maximum Zero Fuel Weight)

58,967kg
0
50k
95k

Empty Weight

39,994kg
0
50k
100k

Capacitycompared to Boeing 757-300

Passenger Capacity

172passengers
0
100
200
295

58% of 757-300 maximum capacity

Crew

Total
6
Cockpit
2
Cabin
4

Dimensions

Length

46.5m

Wingspan

32.9m

Height

9.3m

Wing Area

112.3m²

Catalog Price

Base List Price

$42M USD

1995 catalog price

Note: Actual prices vary based on configuration, options, and negotiations. This represents the manufacturer's base catalog price.

Engine Specifications

Engine Count

2×

Engine Model

IAE V2500-D5

Thrust per Engine

111.2 kN(24999 lbf)

Fuel & Cargo

Fuel Capacity

21,548 L

Cargo Volume

36.8 m³

Production & History

Total Produced

116

Production Status

Out of production

Manufacturing Period

1993–2000

First Flight

February 22, 1993

Entered Service

April 1, 1995

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