McDonnell Douglas DC-10

McDonnell Douglas Out of production since 1989
1970First flight
446Units built
255Typical passengers
9,630 kmRange
298On Vuelopedia
McDonnell Douglas DC-10 illustration Illustrative image; it may differ from the actual aircraft.

The McDonnell Douglas DC-10 is an American trijet wide-body aircraft manufactured by McDonnell Douglas. The DC-10 was intended to succeed the DC-8 for long-range flights. It first flew on August 29, 1970; it was introduced on August 5, 1971, by American Airlines. The trijet has two turbofans on underwing pylons and a third one at the base of the vertical stabilizer. The twin-aisle layout has a typical seating for 270 in two classes. The initial DC-10-10 had a 3,500-nautical-mile [nmi] (6,500 km; 4,000 mi) range for transcontinental flights. The DC-10-15 had more powerful engines for hot and high airports. The DC-10-30 and –40 models (with a third main landing gear leg to support higher weights) each had intercontinental ranges of up to 5,200 nmi (9,600 km; 6,000 mi).

Specifications

Figures for the DC-10-30 variant, the most representative of the family · it is 53% the length of a football pitch

Length55.4 m182 ft
Wingspan50.4 m165 ft
Height17.6 m58 ft
Range9,630 km5,200 NMWith a typical passenger load
Cruise speed871 km/h470 ktMach 0.82
Service ceiling12,800 m41,995 ftIt flies above Everest (1.4 times its height)
Maximum take-off weight267,619 kg589,998 lb
Maximum payload146,877 kg323,808 lbIts 255 passengers with baggage would weigh about 25.5 t; the rest is fuel and cargo
Typical capacity255 passengersUp to 380 in a high-density layout
Endurance11 h 03 minAt cruise speed, non-stop

The type first flew in 1970 (56 years ago) · About 446 units built · Production ended in 1989

Figures for the type, not for this particular aircraft: each variant and each configuration changes something. They are shown in both systems used in aviation.

The story of the type

Development

Background

Following an unsuccessful proposal for the United States Air Force's CX-HLS (Heavy Logistics System) in 1965, Douglas Aircraft began design studies based on its CX-HLS submission. The aviation author John H. Fielder notes that the company was under competitive pressure to produce a wide-body aircraft, having been somewhat slow in the previous decade to introduce its first jetliners. In 1966, American Airlines offered a specification to manufacturers for a twin-engine wide-body aircraft smaller than the Boeing 747 yet capable of flying similar long-range routes from airports with shorter runways; this specification would be highly influential in the design of what would become the DC-10. It would become McDonnell Douglas's first commercial airliner after the merger between McDonnell Aircraft Corporation and Douglas Aircraft Company in 1967.

An early DC-10 design proposal was for a four-engine double-deck wide-body jet airliner with a maximum seating capacity of 550 passengers and similar in length to a DC-8. The proposal was shelved in favor of a trijet single-deck wide-body airliner with a maximum seating capacity of 399 passengers, and similar in length to the DC-8 Super 60. The choice of three engines was influenced by surveys of potential customers other than American Airlines, together with a desire to enhance hot and high climb performance after an engine failure—a serious concern at Stapleton International Airport, which was heavily used by United Airlines, one of the major anticipated buyers. Large portions of the detailed design work, particularly that of the fuselage, were subcontracted to external companies, such as the American aerospace company Convair. The legal relationship between McDonnell Douglas, Convair, and the Federal Aviation Administration (FAA) would later serve to complicate matters; specifically, Convair was forbidden from contacting the regulator no matter the severity of any safety concerns it had in the DC-10's design.

McDonnell Douglas management became seriously concerned about the viability of the DC-10 after learning about the competing Lockheed L-1011, which was very similar and was being offered to the same customers. On February 19, 1968, in what was supposed to be a knockout blow to Lockheed, George A. Spater, President of American Airlines, and James S. McDonnell of McDonnell Douglas announced American Airlines' intention to acquire the DC-10. This was a shock to Lockheed and there was general agreement within the US aviation industry that American Airlines had left its competitors at the starting gate. According to Fielder, McDonnell Douglas had been urgently pursuing the DC-10's completion in light of the prospective competition and the high financial stakes involved. Together with American Airlines' announcement of the DC-10 order, it was also reported that American Airlines had declared its intention to have the British Rolls-Royce RB211 turbofan engine on its DC-10 airliners. The DC-10 was first ordered by launch customers American Airlines with 25 orders, and United Airlines with 30 orders and 30 options in 1968. The DC-10's similarity to the Lockheed L-1011 in design, passenger capacity, and launch date resulted in a sales competition that affected the profitability of both aircraft.

Into flight

On August 29, 1970, the first DC-10, a series 10, conducted its maiden flight. An extensive flight test program was carried out, totaling 929 flights and 1,551 flight hours; the test program was not incident-free: during one ground test in 1970, an outwardly-opening cargo door blew out. The rapid de-pressurization of the cargo hold caused the main cabin's floor to collapse. This discovery and first effort at rectification led to a contract dispute between McDonnell Douglas and Convair over what changes were necessary and financial liability. Fielder alleges that McDonnell Douglas consistently sought to minimize and postpone any design changes to the DC-10, although this attitude was not an explicit policy. In July 1971, Convair outlined the situation in a formal memo; almost a year later, it internally expressed concerns that the inadequate resolution would lead to loss of aircraft. Tragically, the initial rectification work would prove to be inadequate.

On July 29, 1971, the FAA issued the type certificate for the DC-10, permitting its entry into revenue service. It entered commercial service with American Airlines on August 5, 1971, with the initial flight being a round-trip flight between Los Angeles and Chicago. United Airlines also commenced DC-10 flights later that same month. American's DC-10s were configured to seat a maximum of 206 passengers while United's seated 222; both had six-across seating in first-class and eight-across (four pairs) in coach.

Variants

Domestic variants

DC-10-10

The DC-10-10 is the initial passenger version introduced in 1971, produced from 1970 to 1981. The DC-10-10 was equipped with GE CF6-6 engines, which was the first civil engine version from the CF6 family. A total of 122 were built.

DC-10-10CF

The –10CF is a convertible passenger and cargo transport version of the –10. Eight were delivered to Continental Airlines and one to United Airlines.

DC-10-15

The –15 variant was designed for use at hot and high airports. The -15 is a –10 fitted with higher-thrust GE CF6-50C2F (derated DC-10-30 engines) powerplants. The –15 was first ordered in 1979 by Mexicana and Aeroméxico. Seven were completed between 1981 and 1983.

Long-range variants

DC-10-30

A long-range model and the most common model produced. It was built with General Electric CF6-50 turbofan engines, with larger fuel tanks and a larger wingspan to increase range and fuel efficiency, and with a set of rear center landing gear to support the increased weight. It was very popular with European flag carriers. A total of 163 were built from 1972 to 1988 and delivered to 38 different customers. The model was first delivered to KLM and Swissair on November 21, 1972, and first introduced in service on December 15, 1972, by the latter.

DC-10-30CF

The convertible cargo/passenger transport version of the DC-10-30. The first deliveries were to Overseas National Airways (ONA) and Trans International Airlines in 1973. A total of 27 were built.

DC-10-30ER

The extended-range version of the DC-10-30. The –30ER aircraft has a higher maximum takeoff weight of 590,000 pounds (270 t); is powered by three GE CF6-50C2B engines each producing 54,000 lbf (240 kN) of thrust; and is equipped with an additional fuel tank in the rear cargo hold. It has an additional 700 mi of range to 6,600 mi (5,730 nmi; 10,620 km). The first of this variant was delivered to Finnair in 1981. A total of six were built and five –30s were later converted to –30ERs.

DC-10-30AF

Also known as the DC-10-30F. This was the all-freight version of the –30. Production was to start in 1979, but Alitalia did not confirm its order then. Production began in May 1984 after the first aircraft order from FedEx. A total of 10 were built.

DC-10-40

Initial long-range model fitted with Pratt & Whitney JT9D engines, developed for Northwest Orient Airlines. The company wanted its aircraft to be equipped with the same engines as its Boeing 747s for fleet commonality. Originally designated DC-10-20, this model was renamed DC-10-40 at the airline's request, as its leadership did not want it to be perceived as inferior to the series 30 then in development. The aircraft was much improved compared to its original design, with a higher MTOW (on par with the Series 30) and more powerful engines, and retains the increased wingspan from the DC-10-30.

Northwest Orient Airlines and Japan Airlines were the only airlines to order the Series 40, ordering 22 and 20 aircraft, respectively. Northwest's aircraft used JT9D-20 engines producing 50,000 lbf (220 kN) of thrust and an MTOW of 555,000 pounds (252 t). The DC-10-40s delivered to Japan Airlines were equipped with improved JT9D-59A engines that produced increased thrust of 53,000 lbf (240 kN) and allowed a higher MTOW of 565,000 pounds (256 t).

Forty-two DC-10-40s were built from 1973 to 1983. Externally, the DC-10-40 can be distinguished from the DC-10-30 by a slight bulge near the front of the nacelle for the #2 (tail) engine.

DC-10-40D

A domestic variant for Japan Airlines

Proposed variants
DC-10-20

A proposed version of the DC-10-10 with extra fuel tanks, 3-foot (91 cm) extensions on each wingtip, and a rear center landing gear. It was to use Pratt & Whitney JT9D-15 turbofan engines, each producing 45,500 lbf (202 kN) of thrust, with a maximum takeoff weight of 530,000 pounds (240 t). However, engine improvements led to increased thrust and increased takeoff weight. Northwest Orient Airlines, one of the launch customers for this longer-range DC-10 requested the name change to DC-10-40.

DC-10-50

A proposed version with Rolls-Royce RB211-524 engines for British Airways.

Where this type is seen

From our logbook: 23 aircraft of this type documented at 36 airports.

A count of our own aircraft profiles, year by year, from the public United States flight records: it reflects what we have documented, not the airport’s total traffic.

Overview and history adapted from Wikipedia (CC BY-SA) · technical figures from the manufacturer’s published specifications and standard aviation references

Cite

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This page was last updated on October 10, 2026

APA

Vuelopedia. (2026, October 10). McDonnell Douglas DC-10. Retrieved October 16, 2026, from https://vuelopedia.org/en/model/dc10

MLA

“McDonnell Douglas DC-10.” Vuelopedia, Fundación Poderia, 10 Oct. 2026, vuelopedia.org/en/model/dc10. Accessed 16 Oct. 2026.

Chicago

Vuelopedia. “McDonnell Douglas DC-10.” Fundación Poderia. Last modified October 10, 2026. https://vuelopedia.org/en/model/dc10.

Harvard

Vuelopedia (2026) McDonnell Douglas DC-10. Available at: https://vuelopedia.org/en/model/dc10 (Accessed: 16 October 2026).

BibTeX

@misc{vuelopedia_en_model_dc10,
  author       = {{Vuelopedia}},
  title        = {{McDonnell Douglas DC-10}},
  publisher    = {Fundación Poderia},
  year         = {2026},
  date         = {2026-10-10},
  url          = {https://vuelopedia.org/en/model/dc10},
  howpublished = {\url{https://vuelopedia.org/en/model/dc10}},
  urldate      = {2026-10-16},
  note         = {Accessed 2026-10-16}
}

Wikipedia

{{cite web |url=https://vuelopedia.org/en/model/dc10 |title=McDonnell Douglas DC-10 |website=Vuelopedia |publisher=Fundación Poderia |date=2026-10-10 |access-date=2026-10-16 |language=en}}

Aircraft of this type · 298

DC10-46752 · Northwest AirlinesMcDonnell Douglas DC-10-40ScrappedDC10-465415X-DAS · DAS Air CargoMcDonnell Douglas DC-10-30FUnknownDC10-469525X-ONE · Africa OneMcDonnell Douglas DC-10-30Ex-flotaDC10-469339G-ANC · Ghana AirwaysMcDonnell Douglas DC-10-30ScrappedDC10-467129G-AND · Ghana AirwaysMcDonnell Douglas DC-10-30ScrappedDC10-479229J-AFN · Zambia Airways (old)McDonnell Douglas DC-10-30FScrappedDC10-46543C-GCPF · United AirlinesMcDonnell Douglas DC-10-30ScrappedDC10-48285C-GCPG · United AirlinesMcDonnell Douglas DC-10-30ScrappedDC10-48288C-GCPH · United AirlinesMcDonnell Douglas DC-10-30UnknownDC10-46921C-GKFA · Kelowna Flightcraft Air CharterMcDonnell Douglas DC-10-30FScrappedDC10-46949C-GKFB · Kelowna Flightcraft Air CharterMcDonnell Douglas DC-10-30ScrappedDC10-46903CP-2489 · TAB Transportes Aereos BolivianosMcDonnell Douglas MD-10-10FUnknownDC10-46937CP-2555 · TAB Transportes Aereos BolivianosMcDonnell Douglas DC-10-30FUnknownDC10-47926D-ADGO · Kuwait AirwaysMcDonnell Douglas DC-10-30ScrappedDC10-47928D-ADJO · LufthansaMcDonnell Douglas DC-10-30FScrappedDC10-46917D-ADLO · CondorMcDonnell Douglas DC-10-30ScrappedDC10-46965D-ADMO · SabenaMcDonnell Douglas DC-10-30FScrappedDC10-48252D-ADSO · LufthansaMcDonnell Douglas DC-10-30ScrappedDC10-46925EC-CBN · IberiaMcDonnell Douglas DC-10-30Written offDC10-47980EC-CEZ · IberiaMcDonnell Douglas DC-10-30ScrappedDC10-47982EC-DEA · IberiaMcDonnell Douglas DC-10-30ScrappedDC10-47834EC-DHZ · IberiaMcDonnell Douglas DC-10-30ScrappedDC10-46972EC-GTC · IberiaMcDonnell Douglas DC-10-30ScrappedDC10-46958EI-DLA · Continental AirlinesMcDonnell Douglas DC-10-30Unknown
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