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Boeing 767-400ER vs. McDonnell Douglas DC-10-30

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767-400ER

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DC-10-30

Price (USD)
$115 Million$25 Million
First Flight
20001972
Body Type
Wide-bodyWide-body
Length
61 m201 ft
55 m181 ft
Wingspan
51 m170 ft
50 m165 ft
Wing Area
290 m²3,129 ft²
338 m²3,646 ft²
Fuselage Width
5 m16 ft
6 m19 ft
Height
16 m55 ft
17 m57 ft
Max Takeoff Weight
204,100 kg449,963 lbs
251,744 kg555,001 lbs
Number of Engines
23
Engine Options
General Electric CF6 / Pratt & Whitney 4000General Electric CF6
Max Thrust Per Engine
270 kN60,600 lbf
226 kN51,000 lbf
Max Total Thrust
540 kN121,200 lbf
680 kN102,000 lbf
Fuel Capacity
90,700 l23,960 gal
137,509 l36,326 gal
Range
10,400 km5,616 nm
9,600 km5,184 nm
Cruise Speed
850 km/h528 mph
908 km/h564 mph
Typical Seating
296 pax270 pax
Max Seating
375 pax380 pax

What Are the Differences Between the Boeing 767-400ER and McDonnell Douglas DC-10-30

Boeing 767-400ER vs McDonnell Douglas DC-10-30 Size Comparison

  • At 61.40 meters, the Boeing 767-400ER is 6 meters longer than the McDonnell Douglas DC-10-30.
  • With a wingspan of 51.90 meters, the Boeing 767-400ER is 1.50 meters wider from wingtip to wingtip.
  • The Boeing 767-400ER and McDonnell Douglas DC-10-30 have heights of 16.90 meters and 17.60 meters respectively - making the McDonnell Douglas DC-10-30 0.70 meters taller.

Boeing 767-400ER vs McDonnell Douglas DC-10-30 Range

  • Boeing 767-400ER’s range of 10,400 kilometers is greater than McDonnell Douglas DC-10-30’s range of 9,600 kilometers. Therefore, the Boeing 767-400ER can fly nonstop approximately 800 kilometers further.
  • The McDonnell Douglas DC-10-30 can hold 36,326 gallons of fuel, which is 12,366 gallons more than the Boeing 767-400ER’s tank capacity of 23,960 gallons.

Boeing 767-400ER vs McDonnell Douglas DC-10-30 Seating

  • In a typical seating configuration, the Boeing 767-400ER can accommodate 296 passengers, which is about 26 passengers more than McDonnell Douglas DC-10-30’s seating capacity.
  • The McDonnell Douglas DC-10-30’s max seating capacity is 380 passengers, compared to 375 passengers of the Boeing 767-400ER.

About the Boeing 767-400ER

The Boeing 767-400ER is an advanced, wide-body aircraft developed by Boeing as part of the evolution of the 767. Introduced at the beginning of the 21st century, this variant is an extension of the popular 767 family, designed to address the increasing demands of the airline industry for higher capacity and extended range.

As a later addition to the 767 series, the -400ER variant built upon the established reputation of its predecessors by offering enhancements in both size and performance. The development and subsequent introduction of this model into the commercial market were part of Boeing's strategic response to the competitive dynamics of the aviation industry. The 767-400ER's production started in the late 1990s, with the aim of providing airlines with an aircraft that combined operational efficiency with increased passenger capacity.

The aircraft measures 61.4 meters (201.3 feet) in length, featuring an extended fuselage to accommodate more passengers. The wingspan of the 767-400ER is 51.9 meters (170.3 feet), and it has a wing area of 290.7 square meters (3129.1 square feet). These dimensions contribute to the aircraft's aerodynamic efficiency, particularly important for long-distance travel. Equipped with a choice of General Electric CF6 or Pratt & Whitney 4000 series engines, the 767-400ER offers robust performance with a total maximum thrust of 540.0 kN (121,200 lbf). This thrust capacity, combined with a fuel storage of 90,700 liters (23,960 US gallons), enables the aircraft to cover a range of about 10,400 kilometers (5,616 nautical miles), making it well-suited for extended-range operations.

In terms of passenger capacity, the typical layout of the 767-400ER seats up to 296 passengers, with a maximum capacity of 375 passengers in a high-density configuration. The cabin is generally arranged in a dual-class setup, featuring a standard 7 abreast, 2-3-2 seat arrangement in economy class.

Competing with the Airbus A330-200, the 767-400ER was introduced to provide airlines with a modernized option of the 767, balancing the familiar operational characteristics of its predecessors with the needs of contemporary long-haul travel. Notable airlines of the Boeing 767-400ER include Continental (United Airlines) and Delta Air Lines. The aircraft's combination of extended fuselage, increased passenger capacity, and range efficiency mark it as a significant evolution within the 767 family, catering to the specific requirements of modern commercial aviation. Only 37 units of the -400ER were ever produced.

About the McDonnell Douglas DC-10-30

The McDonnel Douglas DC-10-30, is a wide-body trijet airliner designed for long-haul commercial flights. As a member of the DC-10 series, the DC-10-30 was developed to extend the range and capacity of its predecessors, meeting the growing demands of global air travel. The -10-30 was a later, longer range model, and turned out to be the most variant produced. In addition to being a popular passenger aircraft, the DC-10 was also extensively used in the freight industry during its peak.

One of the DC-10's most distinctive features is its three engine configuration, with two engines mounted under the wings and a third engine at the base of the vertical stabilizer. This design was a key differentiator from other wide-body airliners of its time, such as the Boeing 747. The DC-9 made its first flight on August 29, 1970, and was introduced to the commercial aviation market on August 5, 1971 with American Airlines.

Measuring 55.4 meters (181.6 feet) in length, the DC-10-30 was among the larger aircraft of its time, capable of operating on transatlantic and transpacific routes. The aircraft features a wingspan of 50.4 meters (165.3 feet), which supports its long-range flight capabilities and stability at high altitudes. Equipped to hold over 137,500 liters (36,320 US gallons) of fuel, the DC-10-30 was designed for extended range missions, offering a maximum range of 9,600 kilometers (5,184 nautical miles). This capability enabled airlines to operate non-stop intercontinental flights over vast distances. The aircraft's propulsion system consists of 3 GE CF6-50C engines capable of delivering a combined thrust of 680.6 kN (102,000 lbf), providing the power needed for long-haul flights carrying a full complement of passengers and cargo. The DC-10-30's cruise speed of 908 km/h (564 mph) further underscores its efficiency in covering great distances swiftly.

The typical configuration for the DC-10-30 seats up to 270 passengers. Some airliners opted for higher density layouts including 3-4-2, 2-5-2, and 3-3-3. In the market for wide-body aircraft, the McDonnel Douglas DC-10-30 competed with other long-range airliners like the Lockheed L-1011 TriStar and the Boeing 747. The DC-10-30's introduction was a significant contribution to the wide-body aircraft segment, providing airlines with a versatile option for long-haul, high-capacity routes. Prominent operators of the DC-10-30 included airlines such as Continental Airlines, Garuda Indonesia, and Northwest Airlines. Other notable carriers were KLM, British Airways, Iberia, Lufthansa, and Malaysia Airlines.

The McDonnel Douglas DC-10-30's production and operational history reflect its role as a key player in the evolution of long-haul air travel. Its design, performance, and capacity made it a vital asset in the fleets of global airlines, contributing to the expansion and accessibility of international air travel during a critical period of growth in commercial aviation.

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Values shown may not be 100% accurate, as some metrics are averages or only represent certain production years and configurations. Engine specs are based on the best options available.

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