Boeing 767-300ER vs. McDonnell Douglas DC-10-30

The Boeing 767-300ER, an extended-range variant of the 767 family, entered service in 1988 as a response to the growing demand for efficient and versatile wide-body aircraft. This model, with its significant enhancements in range and capacity, has become a staple in the fleets of various airlines for long-haul operations. At its peak in the 1990's, a brand new 767-300ER was valued at roughly $85 million.

With a length of 54.9 meters (180.2 feet) and a wingspan of 47.6 meters (156.2 feet), the 767-300ER is designed for operational efficiency in both airport compatibility and aerodynamics. The wing area of 283.3 square meters (3049.4 square feet) contributes to the aircraft's stable and efficient flight characteristics, especially over extended distances.

The -300ER's increased range was made possible by larger fuel tanks and a higher max takeoff weight (MTOW) of 407,000 lbs (185,000 kgs). The updated variant has a fuel capacity of 90,700 liters (23,960 US gallons), allowing it to cover distances of up to 11,070 kilometers (5,977 nautical miles). This capability makes it particularly suitable for transcontinental and transoceanic routes, offering airlines the flexibility to connect distant cities with fewer stops. Engines options for the -300ER included Pratt & Whitney PW4000s, General Electric CF6s, or Rolls-Royce RB211s. These were capable of a total maximum thrust of 548.0 kN (123,000 lbf). The aircraft exhibits robust performance, necessary for long-haul flights carrying a full load of both passengers and cargo.

The cabin of the 767-300ER is designed to typically seat 261 passengers in a dual-class layout, with the potential to accommodate up to 351 passengers in a high-density configuration. The typical layout includes a spacious business class and a larger economy class, often arranged in a 2-3-2 seat configuration, balancing passenger comfort and density.

Competing in the wide-body market, the Boeing 767-300ER has faced competition from aircraft such as the Airbus A330 and the smaller A300. These models offer similar long-range capabilities and passenger capacities, making the market segment highly competitive. Many carriers have operated the 767-300ER, including Delta Air Lines, United Airlines, British Airways, Japan Airlines, and All Nippon Airways. These carriers have leveraged the aircraft's range and capacity to effectively serve a variety of long-haul routes, underlining its role as a versatile and reliable option in their fleet.

The Boeing 767-300ER's introduction and subsequent service record reflect its importance in the evolution of wide-body aircraft, particularly in the context of long-haul commercial aviation. Its combination of range, capacity, and operational flexibility has solidified its position as a significant player in the global aviation industry.

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.