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McDonnell Douglas DC-9-30 vs. McDonnell Douglas DC-10-30

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DC-9-30

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DC-10-30

Price (USD)
$10 Million$25 Million
First Flight
19661972
Body Type
Narrow-bodyWide-body
Length
36 m119 ft
55 m181 ft
Wingspan
28 m93 ft
50 m165 ft
Wing Area
93 m²1,001 ft²
338 m²3,646 ft²
Fuselage Width
3 m11 ft
6 m19 ft
Height
8 m27 ft
17 m57 ft
Max Takeoff Weight
48,988 kg108,000 lbs
251,744 kg555,001 lbs
Number of Engines
23
Engine Options
Pratt & Whitney JT8DGeneral Electric CF6
Max Thrust Per Engine
67 kN15,000 lbf
226 kN51,000 lbf
Max Total Thrust
134 kN30,000 lbf
680 kN102,000 lbf
Fuel Capacity
13,900 l3,672 gal
137,509 l36,326 gal
Range
2,800 km1,512 nm
9,600 km5,184 nm
Cruise Speed
897 km/h557 mph
908 km/h564 mph
Typical Seating
115 pax270 pax
Max Seating
127 pax380 pax

What Are the Differences Between the McDonnell Douglas DC-9-30 and McDonnell Douglas DC-10-30

McDonnell Douglas DC-9-30 vs McDonnell Douglas DC-10-30 Size Comparison

  • At 55.40 meters, the McDonnell Douglas DC-10-30 is 19 meters longer than the McDonnell Douglas DC-9-30.
  • With a wingspan of 50.40 meters, the McDonnell Douglas DC-10-30 is 22 meters wider from wingtip to wingtip.
  • The McDonnell Douglas DC-9-30 and McDonnell Douglas DC-10-30 have heights of 8.50 meters and 17.60 meters respectively - making the McDonnell Douglas DC-10-30 9.10 meters taller.

McDonnell Douglas DC-9-30 vs McDonnell Douglas DC-10-30 Range

  • McDonnell Douglas DC-10-30’s range of 9,600 kilometers is greater than McDonnell Douglas DC-9-30’s range of 2,800 kilometers. Therefore, the McDonnell Douglas DC-10-30 can fly nonstop approximately 6,800 kilometers further.
  • The McDonnell Douglas DC-10-30 can hold 36,326 gallons of fuel, which is 32,654 gallons more than the McDonnell Douglas DC-9-30’s tank capacity of 3,672 gallons.

McDonnell Douglas DC-9-30 vs McDonnell Douglas DC-10-30 Seating

  • In a typical seating configuration, the McDonnell Douglas DC-10-30 can accommodate 270 passengers, which is about 155 passengers more than McDonnell Douglas DC-9-30’s seating capacity.
  • The McDonnell Douglas DC-10-30’s max seating capacity is 380 passengers, compared to 127 passengers of the McDonnell Douglas DC-9-30.

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.

About the McDonnell Douglas DC-10-30

The McDonnel Douglas DC-10-30, is a wide-body trijet airliner designed for long-haul commercial flights. As a member of the DC-10 series, the DC-10-30 was developed to extend the range and capacity of its predecessors, meeting the growing demands of global air travel. The -10-30 was a later, longer range model, and turned out to be the most variant produced. In addition to being a popular passenger aircraft, the DC-10 was also extensively used in the freight industry during its peak.

One of the DC-10's most distinctive features is its three engine configuration, with two engines mounted under the wings and a third engine at the base of the vertical stabilizer. This design was a key differentiator from other wide-body airliners of its time, such as the Boeing 747. The DC-9 made its first flight on August 29, 1970, and was introduced to the commercial aviation market on August 5, 1971 with American Airlines.

Measuring 55.4 meters (181.6 feet) in length, the DC-10-30 was among the larger aircraft of its time, capable of operating on transatlantic and transpacific routes. The aircraft features a wingspan of 50.4 meters (165.3 feet), which supports its long-range flight capabilities and stability at high altitudes. Equipped to hold over 137,500 liters (36,320 US gallons) of fuel, the DC-10-30 was designed for extended range missions, offering a maximum range of 9,600 kilometers (5,184 nautical miles). This capability enabled airlines to operate non-stop intercontinental flights over vast distances. The aircraft's propulsion system consists of 3 GE CF6-50C engines capable of delivering a combined thrust of 680.6 kN (102,000 lbf), providing the power needed for long-haul flights carrying a full complement of passengers and cargo. The DC-10-30's cruise speed of 908 km/h (564 mph) further underscores its efficiency in covering great distances swiftly.

The typical configuration for the DC-10-30 seats up to 270 passengers. Some airliners opted for higher density layouts including 3-4-2, 2-5-2, and 3-3-3. In the market for wide-body aircraft, the McDonnel Douglas DC-10-30 competed with other long-range airliners like the Lockheed L-1011 TriStar and the Boeing 747. The DC-10-30's introduction was a significant contribution to the wide-body aircraft segment, providing airlines with a versatile option for long-haul, high-capacity routes. Prominent operators of the DC-10-30 included airlines such as Continental Airlines, Garuda Indonesia, and Northwest Airlines. Other notable carriers were KLM, British Airways, Iberia, Lufthansa, and Malaysia Airlines.

The McDonnel Douglas DC-10-30's production and operational history reflect its role as a key player in the evolution of long-haul air travel. Its design, performance, and capacity made it a vital asset in the fleets of global airlines, contributing to the expansion and accessibility of international air travel during a critical period of growth in commercial aviation.

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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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