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Airbus A300-600 vs. McDonnell Douglas DC-9-30

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A300-600

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DC-9-30

Price (USD)
$100 Million$10 Million
First Flight
19831966
Body Type
Wide-bodyNarrow-body
Length
54 m177 ft
36 m119 ft
Wingspan
44 m147 ft
28 m93 ft
Wing Area
260 m²2,798 ft²
93 m²1,001 ft²
Fuselage Width
5 m18 ft
3 m11 ft
Height
16 m54 ft
8 m27 ft
Max Takeoff Weight
171,700 kg378,536 lbs
48,988 kg108,000 lbs
Number of Engines
22
Engine Options
General Electric CF6 / Pratt & Whitney PW4000Pratt & Whitney JT8D
Max Thrust Per Engine
262 kN59,000 lbf
67 kN15,000 lbf
Max Total Thrust
524 kN118,000 lbf
134 kN30,000 lbf
Fuel Capacity
68,150 l18,003 gal
13,900 l3,672 gal
Range
7,500 km4,050 nm
2,800 km1,512 nm
Cruise Speed
897 km/h557 mph
897 km/h557 mph
Typical Seating
257 pax115 pax
Max Seating
345 pax127 pax

What Are the Differences Between the Airbus A300-600 and McDonnell Douglas DC-9-30

Airbus A300-600 vs McDonnell Douglas DC-9-30 Size Comparison

  • At 54.10 meters, the Airbus A300-600 is 17.70 meters longer than the McDonnell Douglas DC-9-30.
  • With a wingspan of 44.80 meters, the Airbus A300-600 is 16.40 meters wider from wingtip to wingtip.
  • The Airbus A300-600 and McDonnell Douglas DC-9-30 have heights of 16.50 meters and 8.50 meters respectively - making the Airbus A300-600 8 meters taller.

Airbus A300-600 vs McDonnell Douglas DC-9-30 Range

  • Airbus A300-600’s range of 7,500 kilometers is greater than McDonnell Douglas DC-9-30’s range of 2,800 kilometers. Therefore, the Airbus A300-600 can fly nonstop approximately 4,700 kilometers further.
  • The Airbus A300-600 can hold 18,003 gallons of fuel, which is 14,331 gallons more than the McDonnell Douglas DC-9-30’s tank capacity of 3,672 gallons.

Airbus A300-600 vs McDonnell Douglas DC-9-30 Seating

  • In a typical seating configuration, the Airbus A300-600 can accommodate 257 passengers, which is about 142 passengers more than McDonnell Douglas DC-9-30’s seating capacity.
  • The Airbus A300-600’s max seating capacity is 345 passengers, compared to 127 passengers of the McDonnell Douglas DC-9-30.

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 McDonnell Douglas DC-9-30

The McDonnel Douglas DC-9-30, a narrow-body jet airliner first introduced in 1966, stands as a significant aircraft in the evolution of commercial aviation. Designed during an era of rapid growth in air travel, the DC-9-30 was developed to meet the demands of short to medium-haul routes, offering airlines a more efficient and practical alternative to the larger jetliners of the time. The Series 30 of the DC-9 included four main sub-variants, -31, -32, -33, and -34. During its production, the -30 was by far the most popular model of the DC-9 with 585 units delivered.

This aircraft was initially developed as the Douglas DC-9, prior to August 1967 merger with McDonnell Aircraft. The DC-9-30 measures in at 36.4 meters (119.3 feet) in length. This size enabled it to operate efficiently in smaller airports and on shorter runways - a niche that was underserved at the time of its introduction. Powered by a pair of Pratt & Whitney PWJTD engines, the DC-9-30 has a total thrust output of 134.0 kN (30,000 lbf). Its fuel capacity of 13,900 liters (3,672 US gallons) gives the DC-9-30 a range of approximately 2,800 kilometers (1,512 nautical miles). This range was particularly advantageous for airlines looking to serve regional networks with an efficient and reliable jet.

The DC-9-30's typical five abreast seating layout can fit around 115 passengers, with a maximum of 127 in a high-density layout.

In its market segment, the McDonnel Douglas DC-9-30 was a key competitor to other short-haul aircraft of the era. Its introduction provided airlines with a jetliner that was not only smaller and more versatile than the larger, long-haul aircraft but also more efficient and economical for short to medium-range routes.

Airlines such as Delta Air Lines, Eastern Air Lines, and TWA were prominent operators of the DC-9-30, utilizing its capabilities to enhance their regional route networks. The aircraft's role in these fleets demonstrated its effectiveness in bridging the gap between propeller-driven airliners and larger jets, contributing significantly to the growth of regional air travel.

The McDonnel Douglas DC-9-30's production and service history highlight its importance as a practical and versatile aircraft in commercial aviation. The last DC-9 to ever be built was delivered in 1982. After its retirement, McDonnell Douglas went on to produce the MD-80 and the MD-95.

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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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