McDonnell Douglas MD-87

Douglas/McDonnell Douglas

ICAOMD87IATAM87
McDonnell Douglas MD-87 aircraft
Douglas/McDonnell DouglasMcDonnell Douglas MD-87
Photo: Atsushi Yoshioka · CC BY 2.0 · Modified

About

The McDonnell Douglas MD-87 represents a unique shorter-fuselage variant of the MD-80 family, designed for airlines needing medium-range capability with reduced capacity. Announced in January 1985, it featured a fuselage shortened by 5.31 meters to 39.75 meters overall, seating 109-130 passengers depending on configuration. This capacity positioned it between the DC-9-50 and MD-80 mainline variants. The MD-87 retained the MD-80's advanced wing, powerful JT8D-217C engines (89 kN each), and modern avionics, offering impressive range of 4,630 km (2,500 NM)—longer than the larger MD-82. The combination of reduced passenger count and full fuel capacity enabled long thin-route operations. Austrian Airlines, Finnair, and Iberia operated the MD-87 on European routes, while Japan Airlines and AeroMexico used it for regional services. The variant's economics proved challenging as airlines preferred higher-capacity options for most routes. Only 75 MD-87s were built before production ended in 1992. Despite modest sales, the MD-87 demonstrated the family's adaptability to different market segments.

Weightscompared to Boeing 757-300

MRW (Maximum Ramp Weight)

68,266kg
0
50k
100k
124k

MTOW (Maximum Takeoff Weight)

67,812kg
0
50k
100k
124k

MLW (Maximum Landing Weight)

58,967kg
0
50k
102k

MZFW (Maximum Zero Fuel Weight)

50,802kg
0
50k
95k

Empty Weight

33,965kg
0
50k
100k

Capacitycompared to Boeing 757-300

Passenger Capacity

130passengers
0
100
200
295

44% of 757-300 maximum capacity

Crew

Total
5
Cockpit
2
Cabin
3

Dimensions

Length

39.8m

Wingspan

32.9m

Height

9.3m

Wing Area

112.3m²

Catalog Price

Base List Price

$26M USD

1988 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

Pratt & Whitney JT8D-217C

Thrust per Engine

89.0 kN(20008 lbf)

Fuel & Cargo

Fuel Capacity

21,095 L

Cargo Volume

30.8 m³

Production & History

Total Produced

75

Production Status

Out of production

Manufacturing Period

1986–1992

First Flight

December 4, 1986

Entered Service

December 11, 1987

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