McDonnell Douglas DC-10-30

Douglas/McDonnell Douglas

ICAODC10IATAD10
McDonnell Douglas DC-10-30 aircraft
Douglas/McDonnell DouglasMcDonnell Douglas DC-10-30
Photo: contri from Yonezawa-Shi, Yamagata, Japan · CC BY-SA 2.0 · Modified

About

The McDonnell Douglas DC-10-30 is the long-range international variant of the DC-10 tri-jet wide-body, designed to compete with the Boeing 747 on intercontinental routes. Introduced in 1972, the DC-10-30 featured more powerful General Electric CF6-50C engines (233 kN each), additional fuel capacity (137,770 liters), and an extended wingspan with increased wing area for better performance at high altitudes. The -30 could seat 250-380 passengers in typical three-class to high-density configurations, with a maximum range of 11,520 km (6,220 NM) allowing non-stop transatlantic and transpacific services. The tri-jet configuration offered excellent redundancy and payload flexibility, with two engines mounted under the wings and one in the tail. The DC-10-30 proved extremely popular with international carriers including KLM, Lufthansa, Air France, and Japan Airlines. A total of 163 DC-10-30s were built, making it the most common DC-10 variant. Many were later converted to freighters and continue operating cargo services today, valued for their large payload capacity of up to 81,720 kg and proven reliability on long-haul routes.

Weightscompared to Airbus A380-800

MRW (Maximum Ramp Weight)

253,105kg
0
200k
400k
577k

MTOW (Maximum Takeoff Weight)

251,744kg
0
200k
400k
575k

MLW (Maximum Landing Weight)

182,798kg
0
150k
300k
395k

MZFW (Maximum Zero Fuel Weight)

166,922kg
0
150k
300k
369k

Empty Weight

120,742kg
0
100k
200k
280k

Capacitycompared to Airbus A380-800

Passenger Capacity

380passengers
0
300
600
853

45% of A380 maximum capacity

Crew

Total
12
Cockpit
3
Cabin
9

Dimensions

Length

55.5m

Wingspan

50.4m

Height

17.7m

Wing Area

367.7m²

Catalog Price

Base List Price

$28M 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

3×

Engine Model

General Electric CF6-50C

Thrust per Engine

233.0 kN(52380 lbf)

Fuel & Cargo

Fuel Capacity

137,770 L

Cargo Volume

188 m³

Production & History

Total Produced

163

Production Status

Out of production

Manufacturing Period

1972–1988

First Flight

June 21, 1972

Entered Service

November 15, 1972

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