The Douglas DC-8 is a four-engined jet airliner, manufactured from 1958 to 1972. Launched later than the competing Boeing 707, the DC-8 nevertheless established Douglas in a strong position in the airliner market, and remained in production until 1972 when much larger designs, including the DC-10, made the DC-8 obsolete. Relegated to second-line duties, details of the DC-8 design allowed it to hold slightly more cargo than the 707; hundreds of re-engined examples remain in freighter service to this day, while commercial 707 service had largely ended by 2000.
- 1 Development
- 2 Variants
- 3 Statistics
- 4 Operators
- 5 Accidents and incidents
- 6 Survivors
- 7 Specifications
- 8 See also
- 9 References
- 10 External links
Development[edit | edit source]
Background[edit | edit source]
In the post-World War II era, Douglas held a commanding position in the commercial aircraft market. Although Boeing had pointed the way to the modern all-metal airliner in 1933 with the 247, it was Douglas that, more than any other company, had made commercial air travel a reality. Douglas produced a succession of piston-engined aircraft through the 1930s, 1940s and 1950s: 138 DC-2s, 10,928 DC-3s (mostly for military service in WWII), 1453 DC-4s, 537 DC-6s and 226 DC-7s.
When De Havilland introduced the first jet-powered airliner, the Comet, in 1949, Douglas took the view that there was no reason to rush into anything new. Their US competitors at Lockheed and Convair felt the same way; that there would be a gradual switch from piston engines to turbines, and that the switch would be to the more fuel-efficient turboprop engines rather than pure jets. All three companies were working on a new generation of piston-engined designs, with an eye to turboprop conversion in the future.
De Havilland's pioneering Comet entered airline service in 1952. Initially it was a success, but a series of fatal crashes in 1953 and 1954 resulted in the type being grounded until the cause could be discovered. Airlines cancelled orders for it, public confidence in the idea of jet transport plummeted, and it would take de Havilland four years to find and fix the problem. The cause of the Comet crashes was nothing to do with jet engines; it was a rapid metal fatigue failure brought on by cycling the high stresses in corners of the near-square windows from pressurizing the cabin to high altitudes and back. A new understanding of metal fatigue that the Comet investigation produced would play a vital part in the good safety record of later types like the DC-8.
In 1952, Douglas remained the most successful of the commercial aircraft manufacturers. They had almost 300 orders on hand for the piston-engined DC-6 and its successor, the DC-7, which had yet to fly and was still two years away from commercial service. The Comet disasters, and the consequent airline lack of interest in jets, seemed to demonstrate the wisdom of their staying with propeller aircraft.
Competition[edit | edit source]
In contrast, Boeing took the bold step of starting to plan a pure-jet airliner as early as 1949. Boeing's military arm had gained extensive experience with large, long-range jets through the B-47 Stratojet (first flight 1947) and the B-52 Stratofortress (1952). With thousands of their big jet bombers on order or in service, Boeing had developed a close relationship with the US Air Force's Strategic Air Command (SAC). Boeing also supplied the SAC's current refueling aircraft, the piston-engined KC-97 Stratotankers, but these proved to be too slow and low flying to easily work with the new jet bombers. The B-52, in particular, had to descend from its cruising altitude and then slow almost to stall speed to work with the KC-97.
Believing that a requirement for a jet-powered tanker was a certainty, Boeing started work on a new all-jet aircraft that would fill this role and also be adaptable into an airliner. In the airliner role it would have similar seating capacity to the Comet, but its swept wing planform would give it considerably higher cruising speeds, and better range. First presented in 1950 as the Model 473-60C, Boeing failed to generate any interest at the airlines. Nevertheless, Boeing remained convinced that the project was worthwhile, and decided to press ahead with a prototype, the "Dash-80". After spending $16 million of their own money (~$120 million 2005 USD) on construction, the Dash-80 rolled out on 15 May 1954, and first flew the next month.
Design phase[edit | edit source]
Boeing's plans became obvious in the industry, in spite of their "code name" intended as a disinformation tactic. Douglas secretly began jet transport project definition studies in mid-1952. By mid-1953 these had developed into a form very similar to the final DC-8; an 80-seat, low-wing aircraft with four Pratt & Whitney JT3C turbojet engines, 30-degree wing sweep, and an internal cabin diameter of exactly 11 feet (3.35 m) to allow five abreast seating. Maximum weight was to be 95 tons, and range was estimated at somewhere between 3,000 and 4,000 miles (4,800 to 6,400 km).
Douglas remained lukewarm about the jet airliner project, but believed that the Air Force tanker contract would go to two companies for two different aircraft, as several USAF transport contracts in the past had done. In May 1954, the USAF circulated its requirement for 800 jet tankers to Boeing, Douglas, Convair, Fairchild, Lockheed, and Martin. Boeing was already just two months away from having their prototype in the air. Just four months after issuing the tanker requirement, the USAF ordered the first 29 KC-135s from Boeing. Even leaving aside Boeing's ability to supply a jet tanker promptly, the flying-boom air-to-air refueling system — as first fitted to the KC-97 — was also a Boeing product: developing the KC-135 had been a safe bet.
Donald Douglas was shocked by the rapidity of the decision which, he said, had been made before the competing companies even had time to complete their bids. He protested to Washington, but without success. Having started on the DC-8 project, Douglas decided that it was better to press on than give up. Consultations with the airlines resulted in a number of changes: the fuselage was widened by 15 inches (380 mm) to allow six-abreast seating. This led to larger wings and tail surfaces and a longer fuselage. The cost of the program was enormous; it was at that time the most expensive venture of any kind ever taken on by a single company.[verification needed] Donald Douglas provided $450 million towards it out of his own pocket.
The DC-8 was officially announced in July 1955. Four versions were offered to begin with, all based on the same 150 ft 6 in (45.9 m) long airframe with a 141 ft 1 in (43 m) wingspan, but varying in engines and fuel capacity, and with maximum weights between 120 and 130 tons. Douglas steadfastly refused to offer different fuselage sizes. The maiden flight was planned for December 1957, with entry into revenue service in 1959. Well aware that they were lagging behind Boeing, Douglas began a major push to market the product.
First orders[edit | edit source]
At the time, Douglas' previous thinking about the airliner market seemed to be coming true; the transition to turbine powered looked likely to be one to turboprops rather than turbojets. The pioneering 40–60-seat Vickers Viscount was already in service and proving enormously popular with both passengers and airlines: it was much faster, quieter and more comfortable than piston-engined types. Another British aircraft, the 90-seat Bristol Britannia, was establishing a fine reputation, and Douglas's main rival in the large, piston-engined passenger aircraft market, Lockheed, had committed to the short/medium range 80–100-seat turboprop Electra, with a launch order from American Airlines for 35 and other major orders flowing in. Meanwhile the Comet remained grounded, the French 90-passenger twin jet Sud Aviation Caravelle prototype had just flown for the first time, and the 707 was not expected to be available until late 1958. The major airlines were reluctant to commit themselves to the huge financial and technical challenge of jet aircraft. On the other hand, no-one could afford not to buy jets if their competitors did.
And there the matter rested until October 1955, when Pan American placed simultaneous orders with Boeing for 20 707s and Douglas for 25 DC-8s. To buy one expensive and untried jet-powered aircraft type was brave: to buy both was at the time, unheard of. In the closing months of 1955, other airlines rushed to follow suit: Air France, American, Braniff, Continental and Sabena ordered 707s; United, National, KLM, Eastern, JAL and SAS chose the DC-8. In 1956 Air India, BOAC, Lufthansa, Qantas and TWA added over 50 to the 707 order book, while Douglas sold 22 DC-8s to Delta, Swissair, TAI, Trans-Canada and UAT. By the start of 1958 Douglas had sold 133 DC-8s as against Boeing's 150 707s.
The first DC-8 was rolled out of the new factory at Long Beach in April 1958 and flew for the first time in May. Later that year an enlarged version of the Comet finally returned to service, but too late to take a substantial portion of the market: de Havilland had just 25 orders. In October Boeing began delivering 707s to Pan Am. Douglas made a massive effort to close the gap with Boeing, using no less than ten individual aircraft for flight testing to achieve FAA certification for the first of the many DC-8 variants in August 1959. Much had needed to be done: the original air brakes on the lower rear fuselage were found ineffective and were simply deleted as engine thrust reversers had become available; unique leading-edge slots were added to improve low-speed lift; the prototype was 25 knots (46 km/h) short of its promised cruising speed and a new, slightly larger wingtip had to be developed to reduce drag.
The DC-8 entered revenue service with both Delta Air Lines and United in September 1959. By March 1960, Douglas had reached their planned production rate of eight DC-8s a month. Despite the large number of DC-8 early models available, all used the same basic airframe, differing only in engines, weights and details. In contrast, Boeing's rival 707 range offered several fuselage lengths: the original 44 m 707-120, a 41 m version that sacrificed space to gain longer range, and the stretched 707-320, which at 46.5 m overall had 3 m more cabin space than the DC-8. Douglas' refusal to offer different fuselage sizes made it less adaptable, and the DC-8 gradually lost market share to Boeing. After an excellent start, 1962 DC-8 sales dropped to just 26, followed by 21 in 1963 and 14 in '64, and most of these were for the Jet Trader rather than the more prestigious passenger versions. In 1967 Douglas merged with McDonnell Aircraft Corporation to become McDonnell Douglas (MDC).
On August 21 1961 a Douglas DC-8 broke the sound barrier at Mach 1.012 or 660 mph while in a controlled dive through 41,000 feet. The flight was to collect data on a new leading-edge design for the wing. The DC-8 became the first civilian jet to make a supersonic flight. The aircraft was a DC-8-43 later delivered to Canadian Pacific Air Lines as CF-CPG.
Further developments[edit | edit source]
In April 1965, Douglas announced belated fuselage stretches for the DC-8, with not just one but three new models, known as the Super Sixties. The DC-8 program had been in danger of closing with fewer than 300 aircraft sold, but the Super Sixties brought fresh life to it. By the time production ceased in 1972, 262 of the stretched DC-8s had been made. With the ability to seat 269 passengers, the DC-8 was easily the largest airliner available, and remained so until the Boeing 747 arrived in 1970.
All the earlier jetliners were noisy by modern standards. Increasing traffic densities and changing public attitudes led to complaints about aircraft noise and moves to introduce restrictions. As early as 1966 the New York Port Authority expressed concern about the noise to be expected from the then still unbuilt DC-8-61, and operators had to agree to operate it from New York at lower weights to reduce noise. By the early 1970s, legislation for aircraft noise standards was being introduced in many countries, and the 60 Series DC-8s were particularly at risk of being banned from major airports.
In the early 1970s several airlines approached McDonnell Douglas for noise reduction modifications to the DC-8 but nothing was done. Third parties had developed aftermarket hushkits but there was no real move to keep the DC-8 in service. Finally, in 1975, General Electric began discussions with major airlines with a view to fitting the new and vastly quieter Franco-American CFM56 engine to both DC-8s and 707s. MDC remained reluctant but eventually came on board in the late 1970s and helped develop the 70 Series DC-8s.
The Super Seventies were a great success: roughly 70% quieter than the 60-Series and, at the time of their introduction, the world's quietest four-engined airliner. As well as being quieter and more powerful, the CFM56 was roughly 20% more fuel efficient than the JT3D, which reduced operating costs and extended the range.
Legacy[edit | edit source]
Throughout its production life the DC-8 was often regarded, unfairly, as little more than a copy of the Boeing 707, which outsold it by roughly two to one. But in the longer term the DC-8 proved its value. By 2002, of the 1032 707s and 720s manufactured for commercial use, just 80 remained in service — though many of those 707s wound up converted for USAF use, either in service or for spare parts. Of the 556 DC-8s made, around 200 were still in commercial service in 2002, including about 25 50-Series, 82 of the stretched 60-Series, and 96 out of the 110 re-engined 70-Series. Most of the surviving DC-8s are now used as freighters.
Variants[edit | edit source]
Early models[edit | edit source]
- DC-8 Series 10 For U.S. domestic use and powered by 60.5 kN Pratt & Whitney JT3C-6 turbojets. The initial DC-8-11 model had the original, high-drag wingtips and all examples were subsequently converted to DC-8-12 standard. The DC-8-12 had the new wingtips and leading-edge slots inboard of each pylon. These unique devices were actuated by doors on the upper and lower surfaces that opened for low speed flight and closed for cruise. The maximum weight increased from 120 tonnes to 123 tonnes. 28 DC-8-10s were manufactured. This model was originally named "DC-8A" until the series 30 was introduced.
- DC-8 Series 20 Higher-powered 70.8 kN Pratt & Whitney JT4A-3 turbojets allowed a weight increase to 125 tonnes. 34 DC-8-20s were manufactured. This model was originally named "DC-8B" but was renamed when the series 30 was introduced.
- DC-8 Series 30 For intercontinental routes, the three Series 30 variants combined JT4A engines with a one-third increase in fuel capacity and strengthened fuselage and landing gear. The DC-8-31 was certified in March 1960 with 75.2 kN JT4A-9 engines for 136 tonnes maximum weight. The DC-8-32 was similar but allowed 140 tonnes weight. The DC-8-33 of November 1960 substituted 78.4 kN JT4A-11 turbojets, a modification to the flap linkage to allow a 1.5 degree setting for more efficient cruise, stronger landing gear, and 143 tonne maximum weight. Many -31 and -32 DC-8s were upgraded to this standard. A total of 57 DC-8-30s were produced.
- DC-8 Series 40 The first turbofan-powered airliner in the world, the -40 was essentially the same as the -30 but with 78.4 kN Rolls-Royce Conway turbofans for better efficiency, less noise and less smoke. The Conway was a significant improvement over the turbojets that preceded it, but the Series 40 sold poorly both because of the traditional reluctance of U.S. airlines to buy a foreign product and because the still more advanced Pratt & Whitney JT3D turbofan was due in early 1961. The DC-8-41 and DC-8-42 had weights of 136 and 140 tonnes, the 143 tonne DC-8-43 had the 1.5 degree flap setting of the -33 and introduced a new 4% leading edge wing extension to allow a small fuel capacity increase and a significant drag reduction — the new wing design improved range by 8%, lifting capacity by 3 tonnes, and cruising speed by better than 10 knots (19 km/h). It would be included in all future DC-8s. A total of 32 DC-8-40s were manufactured.
- DC-8 Series 50 The definitive short-fuselage DC-8 with the same engine that powered the vast majority of 707s, the JT3D. Many earlier DC-8s were converted to this standard. All bar the -55 were certified in 1961. The DC-8-51, DC-8-52 and DC-8-53 all had 76.1 kN JT3D-1 or 80.6 kN JT3D-3B engines, varying mainly in their weights: 126, 138 and 142 tonnes respectively. The DC-8-55 arrived in June 1964, retaining the JT3D-3B engines but with strengthened structure from the freighter versions and 147 tonne maximum weight. 88 DC-8-50s were manufactured.
- DC-8 Jet Trader Douglas approved development of specialized freighter versions of the DC-8 in May 1961, based on the Series 50. An original plan to fit a fixed bulkhead separating the forward two-thirds of the cabin for freight, leaving the rear cabin for 54 passenger seats was soon replaced by a more practical one to use a movable bulkhead and allow anywhere between 25 and 114 seats with the remainder set aside for cargo. A large cargo door was fitted into the forward fuselage, the cabin floor was reinforced and the rear pressure bulkhead was moved by nearly 2 m to make more space. Airlines were offered the option of a windowless cabin, though only one, United, took this up, with an order for 15 in 1964. The DC-8F-54 had a maximum takeoff weight of 143 tonnes and the DC-8F-55 147 tonnes. Both used 80.6 kN JT3D-3B powerplants.
Super sixties[edit | edit source]
- The DC-8 Series 61 was designed for high capacity and medium range. It had the same wings, engines and pylons as the -53, and sacrificed range to gain capacity. Having decided to stretch the DC-8, Douglas inserted a 6 m plug in the forward fuselage and a 5 m plug aft, taking overall length to 57 m and giving the aircraft a very long, lean look that was (and is still) unique. Bending forces required strengthening of the structure, but the basic DC-8 design already had sufficient ground clearance to permit the one-third increase in cabin size without requiring longer landing gear. It was certificated in September 1966 and typically carried 210 passengers, or 269 in high-density configuration. A total of 88 were sold.
- The long-range DC-8 Series 62 followed in April 1967. It had a much more modest stretch of just 2 m (with 1 m plugs fore and aft), the same JT3D engines as the -53 and -61, and a number of modifications to provide greater range. One-meter wingtip extensions reduced drag and added fuel capacity, and Douglas redesigned the engine pods, extending the pylons and substituting new shorter and neater nacelles, all in the cause of drag reduction. Slightly heavier than the -53 or -61 at 151 tonnes, and able to seat 159 passengers, the -62 had a range with full payload of about 5200 nautical miles (9,600 km), or about the same as the -53 but with 40 extra passengers. A total of 67 were built.
- The DC-8 Series 63 was the final new build variant and entered service in June 1968. It combined the aerodynamic refinements and increased fuel capacity of the -62 with the very long fuselage of the -61, and added 85 kN JT3D-7 turbofans, giving a maximum take off weight of almost 159 tonnes and a range with full payload of 4,110 nautical miles (7,600 km). A total of 107 were built, a little over half of them convertibles or dedicated freighters.
Super seventies[edit | edit source]
- The DC-8-72 and the DC-8-73 were straightforward conversions of the -62 and -63, replacing the JT3D engines with 98.5 kN CFM56-2 high-bypass turbofans in new housings built by Grumman. The DC-8-71 achieved the same end but required considerably more modification because the -61 did not already have the improved wings and relocated engines of the -62 and -63. Maximum takeoff weights remained the same but there was a slight reduction in payload because of the heavier engines. All three models were certified in 1982 and a total of 110 60-Series DC-8s were converted by the time the program ended in 1988.
Statistics[edit | edit source]
First flights[edit | edit source]
- DC-8-10 May 30, 1958
- DC-8-20 November 29, 1958
- DC-8-30 February 21, 1959
- DC-8-40 July 23, 1959
- DC-8-50 December 20, 1960
- DC-8-55 October 20, 1962
- DC-8-61 March 14, 1966
- DC-8-62 August 29, 1966
- DC-8-63 April 10, 1967
- (DC-8-61) DC-8-71 August 15, 1981
- (DC-8-62) DC-8-72 December 5, 1981
- (DC-8-63) DC-8-73 March 4, 1982
Operators[edit | edit source]
- Main article: List of Douglas DC-8 operators
Civilian[edit | edit source]
In August 2008 a total of 124 DC-8 aircraft (all variants) were in airline service with the following airlines:
Military[edit | edit source]
Military organizations that use or have used the DC-8 as of March 2006:
- Armée de l'Air (retired from service)
- Peruvian Air Force - a DC-8 in service
- Spanish Air Force (retired from service)
- US Navy: a DC-8 converted to simulate C3I threats under the designation C-24A (now retired from service).
Former operators[edit | edit source]
Accidents and incidents[edit | edit source]
Notable accidents[edit | edit source]
- On November 29 1963 Trans-Canada Air Lines Flight 831, a DC-8, crashed shortly after takeoff from Montréal/Dorval Airport, killing all 118 people on board.
- On February 25 1964 Eastern Air Lines Flight 304, a DC-8 flying from New Orleans International Airport to Washington Reagan National Aiport crashed into Lake Pontchartrain killing all 51 passengers and 7 crew aboard.
- On March 4 1966 Canadian Pacific Airlines Flight 402 (CP402), a DC-8-43 crashed on landing at Tokyo International Airport in Japan, killing 64 passengers and crew, 8 passengers survive.
- On July 1 1968 Seaboard World Airlines Flight 253, a DC-8, is forced to land in the Soviet Union. On board are over 200 American troops bound for Vietnam.
- On January 13 1969 Scandinavian Airlines Flight 933, a DC-8, crashed into the Pacific Ocean west of Los Angeles International Airport.
- On July 5 1970 Air Canada Flight 621, a DC-8, exploded following a failed landing at Toronto Pearson International Airport, with 109 fatalities.
- On October 6 1976 Cubana Flight 455, a DC-8, is bombed by anti-Castro terrorists and crashes near Bridgetown, Barbados, killing all 73 people on board.
- On September 28 1977 Japan Airlines Flight 472, a DC-8, is hijacked after taking off from Mumbai, India by Japanese Red Army (JRA) terrorists. The terrorists force the airplane to land in Dhaka, Bangladesh, where they demand US$6 million and the release of nine imprisoned JRA members being held in Japan. The Japanese government complies and all of the hostages are eventually released.
- On November 15 1978 Icelandic Airlines Flight LL 001, a DC-8 on a charter flight, crashed into a coconut plantation while on approach to Katunayake, Sri Lanka for a refueling stop. 184 out of 264 people on board are killed.
- On December 28 1978 United Airlines Flight 173, a DC-8, ran out of fuel while circling near Portland, Oregon, United States in order for the crew to investigate a light indicating a problem with the landing gear. The airplane crashed in a wooded area, killing 10 and injuring 24 of the 181 on board.
- On February 9 1982 Japan Airlines Flight 350, a DC-8-61, crashed on approach to Tokyo International Airport (Haneda). Among the 166 passengers and 8 crew, 24 passengers are killed.
- On December 12 1985 Arrow Air Flight 1285, a DC-8, crashed after takeoff in Gander, Newfoundland, killing all 256 passengers and crew on board, making it currently the worst air disaster to occur in Canada; the cause is determined to be a stall most likely due to wing icing.
- On June 7 1989 Surinam Airways Flight PY764, a DC-8, crashed while attempting to land in heavy fog at Paramaribo, Suriname. The plane hits trees and flips upside down, killing 176 of 187 people on board.
- On July 11 1991 Nigeria Airways Flight 2120, a Nationair DC-8-61 chartered by Nigeria Airways to transport Nigerian pilgrims to Mecca, crashed shortly after takeoff from Jeddah, Saudi Arabia, due to a fire caused by tire failure. All 261 on board die, including 14 Canadian crew members.
Survivors[edit | edit source]
NASA's DC-8 airborne laboratory will be housed at Grand Forks Air Force Base as of Fall 2005, through an agreement between the University of North Dakota and NASA.
Specifications[edit | edit source]
|Length||150 ft 6 in (45.87 m)||187 ft 4 in (57.10 m)|
|Wingspan||142 ft 5 in (43.41 m)||148 ft 5 in (45.24 m)|
|Height||43 ft 4 in (13.21 m)||43 ft 0 in (13.11 m)|
|Fuselage width||12 ft 3 in (3.73 m)|
|Wing Area||2,771 ft² (257.4 m²)||2,927 ft² (271.9 m²)|
|Empty Weight||134,000 lb (60,800 kg)||146,300 lb (66,360 kg)|
|Max. Takeoff Weight||310,000 lb (140,600 kg)||355,000 lb (161,000 kg)|
|Powerplants (4x)||Pratt & Whitney JT4A-9 turbojets,
16,800 lbf (74.7 kN) each
|Pratt & Whitney JT3D-7 turbofans,|
19,000 lbf, (84.5 kN) each
|Max. Cruise Speed||588 mph (946 km/h)||596 mph (959 km/h)|
|Range with Max. Payload||4,605 miles (7,410 km)||2,140 miles (3,445 km)|
|Wing Loading||111.9 lb/ft² (546.2 kg/m²)||121.3 lb/ft² (592.2 kg/m²)|
|Thrust/Weight Ratio||0.217||0.21 (derived)|
See also[edit | edit source]
Aircraft of comparable role, configuration and era
References[edit | edit source]
- Error on call to Template:cite book: Parameter title must be specifiedNorris, Guy; Wagner, Mark (1999). . MBI Publishing.
- "World Airliner Census", Flight International, 19-25 August 2008.
- Douglas DC-8 incidents, Aviation-Safety.net, 26 August 2008.
- Douglas DC-8 summary, Aviation-Safety.net.
- Douglas DC-8 Accident Statistics, Aviation-Safety.net, 3 December 2007.
- Francillon, René (1979). McDonnell Douglas Aircraft Since 1920: Volume I. London: Putnam. ISBN 0-87021-428-4
[edit | edit source]
- DC-8 page on Airliners.net
- DC-8 page on aerospaceweb.org
- DC-8 Airborne Laboratory fact sheet on NASA/Dryden FRC's site
- DC-8 page on zap16.com
- DC-8 Logbook Photo Gallery
- An early DC-8 concept from 1940s & DC-8 video clips on dc8.org