Douglas DC-9-50

Douglas/McDonnell Douglas

ICAODC95IATAD95
Douglas DC-9-50 aircraft
Douglas/McDonnell DouglasDouglas DC-9-50
Photo: Anidaat · CC BY-SA 4.0 · Modified

About

The Douglas DC-9-50 represents the maximum-capacity variant of the original DC-9 family, featuring the longest fuselage at 40.70 meters and seating up to 139 passengers. Introduced in 1975, it targeted airlines needing dense short-haul operations without transitioning to widebody aircraft. The DC-9-50 incorporated a slightly wider wingspan (28.50m) for better wing loading and was powered by Pratt & Whitney JT8D-17 turbofans producing 71.2 kN (16,000 lbf) thrust each. Swissair launched the variant in 1975, operating it on intra-European trunk routes. The DC-9-50 offered airlines maximum utilization of the proven DC-9 platform while maintaining commonality for training and maintenance. With a range of 2,778 km (1,500 NM), it excelled on high-frequency shuttle operations. Eastern Air Lines became a major operator, deploying dozens on East Coast routes. A total of 96 DC-9-50s were built before production concluded in 1982. The design directly influenced the MD-80 series development, which stretched the concept even further with more powerful engines.

Weightscompared to Boeing 757-300

MRW (Maximum Ramp Weight)

55,338kg
0
50k
100k
124k

MTOW (Maximum Takeoff Weight)

54,885kg
0
50k
100k
124k

MLW (Maximum Landing Weight)

49,895kg
0
50k
102k

MZFW (Maximum Zero Fuel Weight)

44,679kg
0
50k
95k

Empty Weight

29,336kg
0
50k
100k

Capacitycompared to Boeing 757-300

Passenger Capacity

139passengers
0
100
200
295

47% of 757-300 maximum capacity

Crew

Total
6
Cockpit
2
Cabin
4

Dimensions

Length

40.7m

Wingspan

28.5m

Height

8.5m

Wing Area

93.0m²

Catalog Price

Base List Price

$8M USD

1975 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-17

Thrust per Engine

71.2 kN(16006 lbf)

Fuel & Cargo

Fuel Capacity

15,900 L

Cargo Volume

33.5 m³

Production & History

Total Produced

96

Production Status

Out of production

Manufacturing Period

1974–1982

First Flight

December 17, 1974

Entered Service

August 24, 1975

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