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ATR 42-600 vs. McDonnell Douglas DC-10-30

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42-600

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DC-10-30

Price (USD)
$20 Million$25 Million
First Flight
19841972
Body Type
Narrow-bodyWide-body
Length
22 m74 ft
55 m181 ft
Wingspan
24 m80 ft
50 m165 ft
Wing Area
54 m²586 ft²
338 m²3,646 ft²
Fuselage Width
2 m8 ft
6 m19 ft
Height
7 m24 ft
17 m57 ft
Max Takeoff Weight
18,600 kg41,006 lbs
251,744 kg555,001 lbs
Number of Engines
23
Engine Options
Pratt & Whitney Canada PW100General Electric CF6
Max Thrust Per Engine
1,800 kW2,400 shp
226 kN51,000 lbf
Max Total Thrust
3,600 kW4,800 shp
680 kN102,000 lbf
Fuel Capacity
5,730 l1,514 gal
137,509 l36,326 gal
Range
1,326 km716 nm
9,600 km5,184 nm
Cruise Speed
556 km/h345 mph
908 km/h564 mph
Typical Seating
44 pax270 pax
Max Seating
50 pax380 pax

What Are the Differences Between the ATR 42-600 and McDonnell Douglas DC-10-30

ATR 42-600 vs McDonnell Douglas DC-10-30 Size Comparison

  • At 55.40 meters, the McDonnell Douglas DC-10-30 is 32.70 meters longer than the ATR 42-600.
  • With a wingspan of 50.40 meters, the McDonnell Douglas DC-10-30 is 25.80 meters wider from wingtip to wingtip.
  • The ATR 42-600 and McDonnell Douglas DC-10-30 have heights of 7.60 meters and 17.60 meters respectively - making the McDonnell Douglas DC-10-30 10 meters taller.

ATR 42-600 vs McDonnell Douglas DC-10-30 Range

  • McDonnell Douglas DC-10-30’s range of 9,600 kilometers is greater than ATR 42-600’s range of 1,326 kilometers. Therefore, the McDonnell Douglas DC-10-30 can fly nonstop approximately 8,274 kilometers further.
  • The McDonnell Douglas DC-10-30 can hold 36,326 gallons of fuel, which is 34,812 gallons more than the ATR 42-600’s tank capacity of 1,514 gallons.

ATR 42-600 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 226 passengers more than ATR 42-600’s seating capacity.
  • The McDonnell Douglas DC-10-30’s max seating capacity is 380 passengers, compared to 50 passengers of the ATR 42-600.

About the ATR 42-600

The ATR 42-600 is a twin-engine, turboprop aircraft is designed for regional travel. Its role in the aviation industry focuses on connecting regional and remote areas, making air travel accessible to smaller communities. The ATR 42 is most recognizable by its high-wing design , T-tail, and propeller engines.

The ATR 42 was originally introduced in 1984, with the -600 variant beginning flight in 2010. The -600 comes in at 22.7 meters (74.4 feet) long with a wingspan of 24.6 meters (80.6 feet). Its wing area of 54.5 square meters (586.6 square feet) is designed to provide efficient lift for short-runway takeoffs and landings. With a typical seating arrangement for 44 passengers, the ATR 42-600 is an optimal choice for airlines serving regional routes with lower passenger volumes. Powered by two Pratt & Whitney Canada PW120s, the aircraft delivers a total output of 3222 kW (4,320 shp), ensuring reliable performance for its operational requirements. The ATR 42-600 has a fuel capacity of 5,730 liters (1,514 US gallons), contributing to its range of 1,326 kilometers (716 nautical miles). Its cruise speed of 556 km/h (345 mph) enables efficient travel times for regional connections.

In the competitive landscape of regional aviation, the ATR 42-600 contends with aircraft like the Bombardier Q400, Fokker 50, an Embraer EMB 120 Brasilia. Its appeal lies in its operational efficiency and suitability for short-haul routes, particularly in regions where larger jet aircraft are not viable. Airlines that have integrated the ATR 42-600 into their fleets include Silver Airways and Logan Air. These carriers utilize the aircraft to serve regional networks, capitalizing on its capacity to operate efficiently on shorter routes and provide essential connectivity.

The development of the ATR 42-600 was driven by the growing need for efficient, reliable aircraft in the regional market. Its introduction into service has been instrumental in expanding the reach of air travel to smaller markets, underscoring the importance of regional connectivity in the broader aviation industry.

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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