McDonnell Douglas MD-11

Douglas/McDonnell Douglas

ICAOMD11IATAM11
McDonnell Douglas MD-11 aircraft
Douglas/McDonnell DouglasMcDonnell Douglas MD-11
Photo: Te00 16:12, 23 September 2006 (UTC) · Public domain · Modified

About

The McDonnell Douglas MD-11 is a modernized, stretched, and re-engined development of the DC-10 tri-jet wide-body, featuring advanced technology and improved performance. Introduced in 1990, the MD-11 stretched the DC-10 fuselage by 5.7 meters to 61.2 meters, added distinctive winglets for improved fuel efficiency, incorporated a modern two-crew glass cockpit with EFIS displays eliminating the flight engineer, and featured more powerful and efficient engines (GE CF6-80C2 or PW4000 series producing 274 kN each). Additional fuel tanks increased capacity to 146,165 liters (38,615 USG), extending range to 13,150 km (7,100 NM). The MD-11 could seat 298 passengers in three-class configuration or up to 410 in high-density layouts. Despite these improvements, the MD-11 faced fierce competition from more fuel-efficient twin-engine wide-bodies like the Boeing 777 and Airbus A330. Airlines found the tri-jet configuration less economical in an era of ETOPS-certified twins. Production ended in 2001 after 200 aircraft were delivered. However, the MD-11 found tremendous success as a freighter, with FedEx and UPS operating large fleets. The MD-11F remains highly valued in cargo operations for its large payload capacity (up to 95 tons), proven reliability, and excellent hot-and-high performance.

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

$140M USD

1995 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 CF6-80C2 or PW4000

Thrust per Engine

274.0 kN(61598 lbf)

Fuel & Cargo

Fuel Capacity

146,165 L

Cargo Volume

203 m³

Production & History

Total Produced

200

Production Status

Out of production

Manufacturing Period

1988–2001

First Flight

January 10, 1990

Entered Service

December 20, 1990

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