McDonnell Douglas DC-10/MD-11

Douglas/McDonnell Douglas

ICAODC10IATAD10
McDonnell Douglas DC-10/MD-11 aircraft
Douglas/McDonnell DouglasMcDonnell Douglas DC-10/MD-11
Photo: Eddie Maloney from North Las Vegas, USA · CC BY-SA 2.0 · Modified

Details

The McDonnell Douglas DC-10 and MD-11 family represents a lineage of tri-jet wide-body aircraft designed for medium to long-haul routes. The DC-10, introduced in 1971, was McDonnell Douglas's answer to the Boeing 747, offering a smaller wide-body alternative with three engines: two underwing-mounted and one in the tail vertical stabilizer. This tri-jet configuration provided excellent range and payload flexibility, making it popular with airlines worldwide. The DC-10 came in three main variants: DC-10-10 (domestic), DC-10-30 (long-range international), and DC-10-40 (similar to -30 but with different engines). A total of 386 DC-10s were built between 1968 and 1989. The MD-11, introduced in 1990, was a modernized, stretched development of the DC-10 featuring winglets, improved aerodynamics, a modern glass cockpit, and increased fuel capacity. Despite these improvements, the MD-11 faced competition from more efficient twin-engine aircraft like the Boeing 777. Production ended in 2001 after 200 aircraft were built. Both types continue flying today, primarily as cargo freighters valued for their large payload capacity and proven reliability.

2

Variants

586

Built

Weightscompared to Airbus A380-800

MRW (Maximum Ramp Weight)

274,650kg
0
200k
400k
577k

MTOW (Maximum Takeoff Weight)

273,289kg
0
200k
400k
575k

MLW (Maximum Landing Weight)

195,045kg
0
150k
300k
395k

MZFW (Maximum Zero Fuel Weight)

181,437kg
0
150k
300k
369k

Empty Weight

128,809kg
0
100k
200k
280k

Capacitycompared to Airbus A380-800

Passenger Capacity

410passengers
0
300
600
853

48% of A380 maximum capacity

Crew

Total
12
Cockpit
2
Cabin
10

Dimensions

Length

61.2m

Wingspan

51.7m

Height

17.6m

Wing Area

338.9m²

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

GE CF6 / PW JT9D / PW4000

Thrust per Engine

274.0 kN(61598 lbf)

Fuel & Cargo

Fuel Capacity

146,165 L

Cargo Volume

203 m³

Production & History

Total Produced

586

Production Status

Out of production

Manufacturing Period

1968–2001

First Flight

August 29, 1970

Entered Service

August 5, 1971

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