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Airbus A310 vs. McDonnell Douglas DC-9-30

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A310

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DC-9-30

Price (USD)
$60 Million$10 Million
First Flight
19821966
Body Type
Wide-bodyNarrow-body
Length
46 m152 ft
36 m119 ft
Wingspan
43 m144 ft
28 m93 ft
Wing Area
219 m²2,357 ft²
93 m²1,001 ft²
Fuselage Width
5 m18 ft
3 m11 ft
Height
15 m51 ft
8 m27 ft
Max Takeoff Weight
157,000 kg346,126 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
61,070 l16,133 gal
13,900 l3,672 gal
Range
8,050 km4,347 nm
2,800 km1,512 nm
Cruise Speed
850 km/h528 mph
897 km/h557 mph
Typical Seating
220 pax115 pax
Max Seating
230 pax127 pax

What Are the Differences Between the Airbus A310 and McDonnell Douglas DC-9-30

Airbus A310 vs McDonnell Douglas DC-9-30 Size Comparison

  • At 46.60 meters, the Airbus A310 is 10.20 meters longer than the McDonnell Douglas DC-9-30.
  • With a wingspan of 43.90 meters, the Airbus A310 is 15.50 meters wider from wingtip to wingtip.
  • The Airbus A310 and McDonnell Douglas DC-9-30 have heights of 15.80 meters and 8.50 meters respectively - making the Airbus A310 7.30 meters taller.

Airbus A310 vs McDonnell Douglas DC-9-30 Range

  • Airbus A310’s range of 8,050 kilometers is greater than McDonnell Douglas DC-9-30’s range of 2,800 kilometers. Therefore, the Airbus A310 can fly nonstop approximately 5,250 kilometers further.
  • The Airbus A310 can hold 16,133 gallons of fuel, which is 12,461 gallons more than the McDonnell Douglas DC-9-30’s tank capacity of 3,672 gallons.

Airbus A310 vs McDonnell Douglas DC-9-30 Seating

  • In a typical seating configuration, the Airbus A310 can accommodate 220 passengers, which is about 105 passengers more than McDonnell Douglas DC-9-30’s seating capacity.
  • The Airbus A310’s max seating capacity is 230 passengers, compared to 127 passengers of the McDonnell Douglas DC-9-30.

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 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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