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Airbus A300-600 vs. Douglas DC-8

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A300-600

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DC-8

Price (USD)
$100 Million$7 Million
First Flight
19831966
Body Type
Wide-bodyNarrow-body
Length
54 m177 ft
57 m187 ft
Wingspan
44 m147 ft
45 m148 ft
Wing Area
260 m²2,798 ft²
271 m²2,926 ft²
Fuselage Width
5 m18 ft
3 m13 ft
Height
16 m54 ft
12 m42 ft
Max Takeoff Weight
171,700 kg378,536 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
68,150 l18,003 gal
88,552 l23,393 gal
Range
7,500 km4,050 nm
5,900 km3,186 nm
Cruise Speed
897 km/h557 mph
895 km/h556 mph
Typical Seating
257 pax220 pax
Max Seating
345 pax259 pax

What Are the Differences Between the Airbus A300-600 and Douglas DC-8

Airbus A300-600 vs Douglas DC-8 Size Comparison

  • At 57.10 meters, the Douglas DC-8 is 3 meters longer than the Airbus A300-600.
  • With a wingspan of 45.20 meters, the Douglas DC-8 is 0.40 meters wider from wingtip to wingtip.
  • The Airbus A300-600 and Douglas DC-8 have heights of 16.50 meters and 12.90 meters respectively - making the Airbus A300-600 3.60 meters taller.

Airbus A300-600 vs Douglas DC-8 Range

  • Airbus A300-600’s range of 7,500 kilometers is greater than Douglas DC-8’s range of 5,900 kilometers. Therefore, the Airbus A300-600 can fly nonstop approximately 1,600 kilometers further.
  • The Douglas DC-8 can hold 23,393 gallons of fuel, which is 5,390 gallons more than the Airbus A300-600’s tank capacity of 18,003 gallons.

Airbus A300-600 vs Douglas DC-8 Seating

  • In a typical seating configuration, the Airbus A300-600 can accommodate 257 passengers, which is about 37 passengers more than Douglas DC-8’s seating capacity.
  • The Airbus A300-600’s max seating capacity is 345 passengers, compared to 259 passengers of the Douglas DC-8.

About the Airbus A300-600

The Airbus A300-600 is a wide-body, twin-engine jet airliner developed by Airbus as part of the A300 aircraft family. Introduced to the commercial aviation market in the 1980s, the A300-600 represents a significant evolution in Airbus's wide-body offerings, catering to medium to long-haul routes. This model showcases advancements in aerospace technology and design, reflecting the changing needs of the global aviation industry during that period.

Measuring 177.5 feet (54.1 meters) in length with a wingspan of 147.1 feet (44.84 meters), the A300-600 is designed to transport a large number of passengers over considerable distances. Typically, the aircraft can seat around 250-290 passengers in a standard three-class configuration, although seating arrangements can vary based on airline specifications. This capacity makes it suitable for various operations, ranging from high-density short-haul routes to more extended intercontinental flights. The A300-600 incorporates a number of design improvements over its predecessors in the A300 series. Notably, the aircraft features an increased use of composites and advanced alloys in its structure, enhancing its efficiency and reducing overall weight. It is powered by General Electric CF6-80C2 or Pratt & Whitney PW4000 engines, which provide the necessary thrust for its operations. The aircraft's maximum takeoff weight is approximately 375,000 lbs, and it has a range of about 4,050 nautical miles. Inside the cabin, the A300-600 offers a comfortable and spacious environment for passengers, with a focus on maximizing cabin space and providing amenities that enhance the travel experience. The cockpit design incorporates advanced avionics and electronic flight instrumentation, consistent with Airbus's commitment to leveraging technology for improved flight operations and safety.

Over its production life, the Airbus A300-600 was ordered and operated by several airlines around the world. Key operators have included carriers such as Lufthansa, Thai Airways, and Saudi Arabian Airlines, who have deployed the aircraft across a variety of routes. Its versatility and capacity have made it a valuable asset for airlines needing a wide-body aircraft capable of handling diverse operational demands. The A300-600's significance in the Airbus lineup lies in its role as a bridge between the first generation of wide-body jets and the newer, more technologically advanced models that followed. Its introduction was a step forward in the evolution of commercial aircraft, combining increased passenger capacity with improved efficiency and range.

The Airbus A300-600 remains a notable model in the history of commercial aviation, demonstrating Airbus's ability to innovate and adapt to the changing landscape of air travel. While its production has since ceased, the A300-600 continues to be recognized for its contributions to the development of modern wide-body aircraft.

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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