Douglas DC-9-30

Douglas/McDonnell Douglas

ICAODC93IATAD93
Douglas DC-9-30 aircraft
Douglas/McDonnell DouglasDouglas DC-9-30
Photo: Steve Knight · CC BY 2.0 · Modified

About

The Douglas DC-9-30 became the most successful DC-9 variant, representing the ideal balance of capacity, range, and economics for short-to-medium-haul operations. Introduced in 1967, it featured a 4.54-meter fuselage stretch to 36.37 meters, seating 100-115 passengers in typical configuration. The DC-9-30 incorporated a wider wingspan (28.47m) for improved efficiency and offered engine options ranging from JT8D-7 (64.5 kN) to JT8D-17 (71.2 kN) for varying performance needs. Airlines valued its operational flexibility—capable of serving both dense short routes and thinner medium-haul markets with a range of 2,778 km (1,500 NM). The variant proved immensely popular, with 662 built for operators worldwide including Eastern Airlines, Ozark Air Lines, and Swissair. The DC-9-30's reliability and low operating costs made it a workhorse for domestic networks throughout the 1970s-1990s. Many were later converted to freighters. The DC-9-30 established the template for subsequent stretched variants including the MD-80 series.

Weightscompared to Boeing 757-300

MRW (Maximum Ramp Weight)

49,442kg
0
50k
100k
124k

MTOW (Maximum Takeoff Weight)

48,988kg
0
50k
100k
124k

MLW (Maximum Landing Weight)

44,906kg
0
50k
102k

MZFW (Maximum Zero Fuel Weight)

39,463kg
0
50k
95k

Empty Weight

25,789kg
0
50k
100k

Capacitycompared to Boeing 757-300

Passenger Capacity

115passengers
0
100
200
295

39% of 757-300 maximum capacity

Crew

Total
5
Cockpit
2
Cabin
3

Dimensions

Length

36.4m

Wingspan

28.5m

Height

8.4m

Wing Area

93.0m²

Catalog Price

Base List Price

$4.5M USD

1972 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-9/15/17

Thrust per Engine

66.7 kN(14995 lbf)

Fuel & Cargo

Fuel Capacity

15,520 L

Cargo Volume

27.4 m³

Production & History

Total Produced

662

Production Status

Out of production

Manufacturing Period

1966–1982

First Flight

August 1, 1966

Entered Service

February 1, 1967

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