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ATR 72-600 vs. McDonnell Douglas DC-10-30

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72-600

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DC-10-30

Price (USD)
$26 Million$25 Million
First Flight
19881972
Body Type
Narrow-bodyWide-body
Length
27 m89 ft
55 m181 ft
Wingspan
27 m88 ft
50 m165 ft
Wing Area
61 m²656 ft²
338 m²3,646 ft²
Fuselage Width
2 m8 ft
6 m19 ft
Height
7 m25 ft
17 m57 ft
Max Takeoff Weight
23,000 kg50,706 lbs
251,744 kg555,001 lbs
Number of Engines
23
Engine Options
Pratt & Whitney Canada PW100General Electric CF6
Max Thrust Per Engine
1,846 kW2,475 shp
226 kN51,000 lbf
Max Total Thrust
3,692 kW4,750 shp
680 kN102,000 lbf
Fuel Capacity
6,400 l1,691 gal
137,509 l36,326 gal
Range
1,528 km825 nm
9,600 km5,184 nm
Cruise Speed
510 km/h317 mph
908 km/h564 mph
Typical Seating
62 pax270 pax
Max Seating
74 pax380 pax

What Are the Differences Between the ATR 72-600 and McDonnell Douglas DC-10-30

ATR 72-600 vs McDonnell Douglas DC-10-30 Size Comparison

  • At 55.40 meters, the McDonnell Douglas DC-10-30 is 28.20 meters longer than the ATR 72-600.
  • With a wingspan of 50.40 meters, the McDonnell Douglas DC-10-30 is 23.30 meters wider from wingtip to wingtip.
  • The ATR 72-600 and McDonnell Douglas DC-10-30 have heights of 7.70 meters and 17.60 meters respectively - making the McDonnell Douglas DC-10-30 9.90 meters taller.

ATR 72-600 vs McDonnell Douglas DC-10-30 Range

  • McDonnell Douglas DC-10-30’s range of 9,600 kilometers is greater than ATR 72-600’s range of 1,528 kilometers. Therefore, the McDonnell Douglas DC-10-30 can fly nonstop approximately 8,072 kilometers further.
  • The McDonnell Douglas DC-10-30 can hold 36,326 gallons of fuel, which is 34,635 gallons more than the ATR 72-600’s tank capacity of 1,691 gallons.

ATR 72-600 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 208 passengers more than ATR 72-600’s seating capacity.
  • The McDonnell Douglas DC-10-30’s max seating capacity is 380 passengers, compared to 74 passengers of the ATR 72-600.

About the ATR 72-600

The ATR 72-600, part of the renowned ATR aircraft family, is a twin-engine, high-wing turboprop airliner designed primarily for regional and short-haul flights. First flown in 1988, this model has become a popular choice for airlines operating in small markets.

ATR, the manufacturer of the ATR 72, has produced over 1800 units through 2023. The -600 variant is the latest model to be designed, making its first flight in 2007. Compared to the smaller ATR 42, the ATR 72 has a longer fuselage and wider wingspan. At 27.2 meters (89.1 feet) from nose to tail and a width of 27.1 meters (88.7 feet), the ATR 72-600 is characterized by its compact and efficient design, suitable for operations at smaller airports. It has a max takeoff weight of 23,000 kg (50,706 lbs), and a max payload of 7,400 kg (16,313 lbs). The ATR 72-600 is powered by two engines, delivering a total output of 3692 kW (4,950 shp), providing reliable performance for its operational requirements. It has a fuel capacity of 6,400 liters (1,691 US gallons), which contributes to its range of 1,528 kilometers (825 nautical miles). With a cruise speed of 510 km/h (317 mph), the ATR 72-600 offers an efficient travel option for regional airlines, connecting smaller communities and cities.

In the regional aviation sector, the ATR 72-600 competes with aircraft like the Bombardier Q400 and Embraer E-Jets. Its advantage lies in its operational cost-effectiveness, making it an appealing choice for airlines serving regional routes with moderate passenger volumes. Airlines such as Air New Zealand, IndiGo, SAS, and TAROM operate the ATR 72-600, utilizing its capabilities to serve regional networks. These carriers value the aircraft for its ability to provide efficient, reliable service on shorter routes, which are crucial for maintaining regional connectivity. The introduction of the ATR 72-600 to the market was driven by the need for an economical, versatile aircraft that could effectively serve the regional aviation segment. Its operational role has been defined by its capacity to offer cost-efficient solutions for airlines operating on less dense routes.

Today, the ATR 72-600 remains a significant player in the regional aircraft market, demonstrating its continued relevance in connecting smaller cities and communities.

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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