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Airbus A310 vs. Douglas DC-8

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A310

vs.

DC-8

Price (USD)
$60 Million$7 Million
First Flight
19821966
Body Type
Wide-bodyNarrow-body
Length
46 m152 ft
57 m187 ft
Wingspan
43 m144 ft
45 m148 ft
Wing Area
219 m²2,357 ft²
271 m²2,926 ft²
Fuselage Width
5 m18 ft
3 m13 ft
Height
15 m51 ft
12 m42 ft
Max Takeoff Weight
157,000 kg346,126 lbs
147,400 kg324,961 lbs
Number of Engines
24
Engine Options
General Electric CF6 / Pratt & Whitney PW4000Pratt & Whitney JT3D
Max Thrust Per Engine
262 kN59,000 lbf
80 kN18,000 lbf
Max Total Thrust
524 kN118,000 lbf
320 kN36,000 lbf
Fuel Capacity
61,070 l16,133 gal
88,552 l23,393 gal
Range
8,050 km4,347 nm
5,900 km3,186 nm
Cruise Speed
850 km/h528 mph
895 km/h556 mph
Typical Seating
220 pax220 pax
Max Seating
230 pax259 pax

What Are the Differences Between the Airbus A310 and Douglas DC-8

Airbus A310 vs Douglas DC-8 Size Comparison

  • At 57.10 meters, the Douglas DC-8 is 10.50 meters longer than the Airbus A310.
  • With a wingspan of 45.20 meters, the Douglas DC-8 is 1.30 meters wider from wingtip to wingtip.
  • The Airbus A310 and Douglas DC-8 have heights of 15.80 meters and 12.90 meters respectively - making the Airbus A310 2.90 meters taller.

Airbus A310 vs Douglas DC-8 Range

  • Airbus A310’s range of 8,050 kilometers is greater than Douglas DC-8’s range of 5,900 kilometers. Therefore, the Airbus A310 can fly nonstop approximately 2,150 kilometers further.
  • The Douglas DC-8 can hold 23,393 gallons of fuel, which is 7,260 gallons more than the Airbus A310’s tank capacity of 16,133 gallons.

Airbus A310 vs Douglas DC-8 Seating

  • The Airbus A310 and the Douglas DC-8 have the same seating capacity at 220 pax
  • The Douglas DC-8’s max seating capacity is 259 passengers, compared to 230 passengers of the Airbus A310.

About the Airbus A310

The Airbus A310 is a wide-body, twin-engine jetliner developed by Airbus in the early 1980s as a smaller variant of the A300, its first airliner. The A310 was designed to meet the demands of airlines for a smaller, more efficient aircraft for medium to long-haul routes. This development marked Airbus's expansion in the wide-body aircraft market, offering a versatile option for various airline operations.

With a length of 153 feet (46.7 meters) and a wingspan of 144 feet (43.9 meters), the A310 is notably smaller than the A300, making it suitable for routes with lower passenger demand. The aircraft typically accommodates around 220 passengers in a standard three-class configuration, though it can be configured to carry more in a high-density layout. This flexibility in seating allows airlines to optimize the A310 for both high passenger volume short-haul flights and longer, less densely populated routes.

The A310's design incorporates significant advancements over the A300, including a shortened fuselage and redesigned wing, which contribute to its improved aerodynamics and fuel efficiency. It is equipped with either General Electric CF6-80 or Pratt & Whitney JT9D engines, providing a balance of power and efficiency. The A310 has a maximum takeoff weight of approximately 336,000 lbs and a range of up to 4,350 nautical miles, depending on the variant and configuration. Inside, the A310 offers a comfortable passenger experience with a spacious cabin and advanced features for its time, such as an optional two-crew glass cockpit. This innovative cockpit design reduced the flight crew requirement from three to two, a significant shift in commercial aviation operations.

The Airbus A310 was well-received in the commercial aviation market, with orders from several airlines worldwide. Notable operators included Lufthansa, Air France, and KLM, among others. These airlines utilized the A310 for its intended purpose, taking advantage of its capacity and range for diverse route networks. The A310's production and service history reflect its role in the evolution of Airbus's wide-body offerings. It bridged the gap between the larger A300 and the later A330 and A340 models, demonstrating Airbus's capability to adapt to market needs. The A310 was instrumental in establishing Airbus as a major competitor in the wide-body aircraft segment.

Though production of the A310 has ceased, its legacy continues in the aviation industry. The aircraft is remembered for its contributions to the development of wide-body jets, particularly in terms of efficiency, versatility, and technological advancements in aircraft design.

About the Douglas DC-8

The Douglas DC-8, is a long-range, narrow-body jet airliner developed by American Douglas Aircraft Company. Introduced in the mid-1960s, the DC-8 was among the first generation of commercial jetliners, marking a significant transition in air travel from propeller-driven to jet-powered aircraft. This model was developed during a period of rapid advancement in aviation technology, driven by the growing demand for faster and more efficient air travel.

The DC-8's design features a length of 57.1 meters (187.3 feet), which, at the time of its introduction, was one of the longest for any airliner. This length, coupled with a wingspan of 45.2 meters (148.4 feet), reflects the aircraft's capacity to handle long-haul routes, a key requirement during the jet age's early years. The DC-8's size was a response to the airline industry's needs for greater passenger capacity and range. Equipped with four Pratt & Whitney JT3D turbojet engines, the DC-8 could achieve a total thrust of 320.0 kN (36,000 lbf). This power output was instrumental in enabling the aircraft to reach a range of approximately 5,900 kilometers (3,186 nautical miles), making it suitable for transcontinental and transatlantic routes. The DC-8's speed and range capabilities were significant advancements at the time, contributing to the reduction of travel times on international routes.

The cabin of the DC-8 was designed to seat around 220 passengers in a typical two-class configuration with six seats across. This capacity allowed airlines to transport more passengers per flight compared to earlier propeller-driven airliners, significantly increasing operational efficiency. The interior of the DC-8 was designed with comfort in mind, offering features that were considered state-of-the-art during its era.

In the commercial aviation market, the Douglas DC-8 competed with the other early quadjet, the Boeing 707. The introduction of the DC-8 was part of the broader trend towards jet-powered air travel, which revolutionized the airline industry by offering faster and more comfortable flights over longer distances. Airlines that operated the DC-8 were United Airlines, Delta Air Lines, Thai Airways, and Pan American World Airways. The DC-8's operational role was marked by its ability to serve long-haul routes with improved efficiency and speed, a factor that contributed significantly to the growth of global air travel during the 1960s and 1970s. The DC-8 was produced until 1972, with 556 aircraft built. As the model aged out, it was superseded by larger wide-body Douglas' DC-10 trijet.

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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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