Douglas DC-9-20

Douglas/McDonnell Douglas

ICAODC92IATAD92
Douglas DC-9-20 aircraft
Douglas/McDonnell DouglasDouglas DC-9-20
Photo: Aero Icarus from Zürich, Switzerland · CC BY-SA 2.0 · Modified

About

The Douglas DC-9-20 was a specialized variant developed specifically for operations from high-altitude airports and hot climates. Retaining the compact 31.82-meter fuselage of the DC-9-10, it featured more powerful Pratt & Whitney JT8D-11 engines producing 66.7 kN (15,000 lbf) thrust each and improved wing design for better performance in challenging conditions. The DC-9-20 was optimized for airlines serving airports like Denver, Mexico City, and La Paz, where thin air reduced engine performance and increased takeoff distances. SAS (Scandinavian Airlines) launched the variant in 1968, valuing its ability to maintain schedules from mountainous Scandinavian airports during summer heat. The DC-9-20 seated 80-90 passengers and offered a range of 2,963 km (1,605 NM). However, only 10 examples were built due to limited demand—most airlines preferred the larger DC-9-30. The DC-9-20 proved the design's adaptability but remained a niche variant. SAS operated theirs until the late 1980s.

Weightscompared to Boeing 757-300

MRW (Maximum Ramp Weight)

45,813kg
0
50k
100k
124k

MTOW (Maximum Takeoff Weight)

45,359kg
0
50k
100k
124k

MLW (Maximum Landing Weight)

43,227kg
0
50k
102k

MZFW (Maximum Zero Fuel Weight)

38,102kg
0
50k
95k

Empty Weight

23,879kg
0
50k
100k

Capacitycompared to Boeing 757-300

Passenger Capacity

90passengers
0
100
200
295

31% of 757-300 maximum capacity

Crew

Total
4
Cockpit
2
Cabin
2

Dimensions

Length

31.8m

Wingspan

27.3m

Height

8.4m

Wing Area

86.8m²

Catalog Price

Base List Price

$4M USD

1968 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-11

Thrust per Engine

66.7 kN(14995 lbf)

Fuel & Cargo

Fuel Capacity

14,100 L

Cargo Volume

18.7 m³

Production & History

Total Produced

10

Production Status

Out of production

Manufacturing Period

1968–1969

First Flight

September 18, 1968

Entered Service

December 30, 1968

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