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Airbus A330-200 vs. McDonnell Douglas DC-9-30

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A330-200

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DC-9-30

Price (USD)
$231 Million$10 Million
First Flight
19971966
Body Type
Wide-bodyNarrow-body
Length
58 m193 ft
36 m119 ft
Wingspan
60 m197 ft
28 m93 ft
Wing Area
361 m²3,892 ft²
93 m²1,001 ft²
Fuselage Width
5 m18 ft
3 m11 ft
Height
17 m57 ft
8 m27 ft
Max Takeoff Weight
251,000 kg553,360 lbs
48,988 kg108,000 lbs
Number of Engines
22
Engine Options
General Electric CF6 / Pratt & Whitney PW4000 / Rolls-Royce Trent 700Pratt & Whitney JT8D
Max Thrust Per Engine
316 kN71,100 lbf
67 kN15,000 lbf
Max Total Thrust
632 kN142,200 lbf
134 kN30,000 lbf
Fuel Capacity
139,100 l36,746 gal
13,900 l3,672 gal
Range
13,450 km7,262 nm
2,800 km1,512 nm
Cruise Speed
870 km/h541 mph
897 km/h557 mph
Typical Seating
273 pax115 pax
Max Seating
406 pax127 pax

What Are the Differences Between the Airbus A330-200 and McDonnell Douglas DC-9-30

Airbus A330-200 vs McDonnell Douglas DC-9-30 Size Comparison

  • At 58.80 meters, the Airbus A330-200 is 22.40 meters longer than the McDonnell Douglas DC-9-30.
  • With a wingspan of 60.30 meters, the Airbus A330-200 is 31.90 meters wider from wingtip to wingtip.
  • The Airbus A330-200 and McDonnell Douglas DC-9-30 have heights of 17.40 meters and 8.50 meters respectively - making the Airbus A330-200 8.90 meters taller.

Airbus A330-200 vs McDonnell Douglas DC-9-30 Range

  • Airbus A330-200’s range of 13,450 kilometers is greater than McDonnell Douglas DC-9-30’s range of 2,800 kilometers. Therefore, the Airbus A330-200 can fly nonstop approximately 10,650 kilometers further.
  • The Airbus A330-200 can hold 36,746 gallons of fuel, which is 33,074 gallons more than the McDonnell Douglas DC-9-30’s tank capacity of 3,672 gallons.

Airbus A330-200 vs McDonnell Douglas DC-9-30 Seating

  • In a typical seating configuration, the Airbus A330-200 can accommodate 273 passengers, which is about 158 passengers more than McDonnell Douglas DC-9-30’s seating capacity.
  • The Airbus A330-200’s max seating capacity is 406 passengers, compared to 127 passengers of the McDonnell Douglas DC-9-30.

About the Airbus A330-200

Introduced in 1998, the Airbus A330-200 is a wide-body, twin-engine jetliner for medium to long-haul flights. This model, with its shorter fuselage than the A330-300, offers enhanced range capabilities, making it a versatile option for international airlines.

Spanning 193 feet (58.8 meters) in length with a wingspan of 197.8 feet (60.3 meters), the A330-200 accommodates up to 247 passengers in a standard three-class configuration. Its design prioritizes cabin flexibility, allowing airlines to customize seating layouts to suit various route requirements. The aircraft's interior features modern amenities, contributing to passenger comfort and satisfaction. Powered by a choice of engines from Rolls-Royce, General Electric, or Pratt & Whitney, the A330-200 achieves a balance of power and efficiency. It boasts a maximum takeoff weight of about 533,500 lbs and can cover distances up to 7,250 nautical miles. This extended range is instrumental in connecting distant city pairs and expanding airlines' route networks. The A330-200 integrates Airbus's advanced avionics and fly-by-wire technology, features that enhance flight performance and safety. The two-person cockpit is equipped with an electronic flight instrument system and sophisticated navigation tools, making flight operations more efficient and intuitive.

Airlines like Delta Air Lines, Turkish Airlines, and Etihad Airways have utilized the A330-200 extensively. Its operational flexibility makes it suitable for a variety of routes, from dense, high-demand corridors to specialized long-haul flights. The aircraft's ability to efficiently operate on transcontinental routes has been particularly beneficial for airlines expanding their global presence. The A330-200's market introduction responded to the need for a wide-body aircraft with optimized range and capacity. The -200 competes with the Boeing 767-400ER, as well as with the Boeing 787-8. While production for A330 CEOs ceased in 2021, the model is now being built in the newer-800 and -900 variants.

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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