Boeing 7J7

Last updated
Boeing 7J7
Boeing 7J7.jpg
RoleAirliner
National origin United States
Manufacturer Boeing Commercial Airplanes
StatusDeveloped, never built
Number built0

The Boeing 7J7 was an American short- to medium-range airliner proposed by American aircraft manufacturer Boeing in the 1980s. It would have carried 150 passengers and was touted as the successor to the successful Boeing 727. [1] It was initially planned to enter service in 1992. [1] This was intended as a highly fuel-efficient aircraft employing new technologies, but it was postponed indefinitely as the price of oil dropped during the 1980s.

Contents

Development

The 7J7 was the culmination of Boeing's Seven Dash Seven (7–7) 150-seat aircraft idea, which the company had considered since at least 1981. [2] [3] It was to be Boeing's second attempt at a replacement for the Boeing 727, its successful but aging 150-seat aircraft. The Boeing 757, a larger airplane that Boeing expected existing 727 customers to upgrade to, had unexpectedly slow sales leading to its 1983 entry into commercial service, as airline deregulation resulted in airlines using smaller aircraft at increased frequencies. By vacating the 727's seating capacity, Boeing had a large capacity gap in its aircraft lineup between the larger 757 and smaller Boeing 737.

In 1983, Scandinavian Airlines (SAS), an airline that employed aircraft mostly from McDonnell Douglas, contacted Boeing about the aircraft concept to replace its McDonnell Douglas DC-9s. The airline would become the 7J7's most faithful customer, and it would wield a large influence in the aircraft's cabin design. [4] Japan initially agreed to a Letter of Understanding with Boeing in March 1984 to take a 25-percent share in a future 150-seat airliner, such as Boeing's Seven Dash Seven or Japan's "YXX" project, that would enter service in 1988 using the IAE V2500 turbofan as the engine, [5] which was developed in part by the Japanese Aero Engine Corporation. However, Boeing became increasingly interested in the latest propfan engine research that would yield large double-digit fuel savings, in particular with the gearless unducted fan (UDF) concept from the aviation division of General Electric. By February 1985, Boeing postponed the service entry of the then-unnamed aircraft to the early 1990s so that propfan technology would be ready for the plane; [6] Boeing made the engine change, schedule change, and announcement unilaterally, which surprised and upset its Japanese partners. [7] It also scrapped the 7–7 code name, saying that the moniker was too commonly seen as a possible direct competitor to the Airbus A320, and that the aircraft Boeing had in mind would be a half-generation ahead. [6] The company held a program kickoff meeting for suppliers on May 13, 1985, [8] and then it debuted a model of the aircraft concept at the 1985 Paris Air Show, [9] where Boeing announced that it would start taking orders in 1987–1988 for deliveries starting in the first half of 1992. [10] In August 1985, the code name for the aircraft was changed to the 7J7. [11] On December 20, 1985, Boeing reached an agreement to test the proposed 578-DX geared propfan engine of General Motors subsidiary Allison Engine Company for use on the 7J7. [12]

In March 1986, Boeing officially announced Japan's 25 percent participation in the 7J7. [9] The name of the aircraft reflected this participation, as the "J" in 7J7 represented the Japan Aircraft Development Corporation (JADC), a partnership of the large Japanese industrial firms Kawasaki Heavy Industries, Fuji Heavy Industries, and Mitsubishi Heavy Industries (MHI). [13] Shorts from the United Kingdom and Saab-Scania from Sweden also invested in the program a few weeks later, but with smaller, single-digit percentages. [14] Hawker de Havilland of Australia joined with a similar small percentage in December 1986. [15]

During the same week that Boeing made the Japanese 7J7 announcement, SAS held a 13-member board of directors meeting near Boeing headquarters to inspect Boeing's 7J7 work. The airline also expressed its desire to eliminate middle seats in a six-abreast configuration and asked that the cabin include a seven-abreast option for economy travel. Jan Carlzon, SAS's chairman at the time, dangled the possibility of SAS being a launch customer. He suggested that if the 7J7 were built, SAS could become the largest operator of Boeing aircraft within 10 years. [16] In mid-1986, Ireland-based aircraft leasing firm GPA Group also declared its desire to be a 7J7 launch customer. [17]

On August 20, 1986, the General Electric GE36 UDF engine was tested in flight for the first time, on a Boeing 727-100 testbed. [18] The next month at the Farnborough Air Show, Boeing stated that the early acoustical results were better than expected. The company declared that the test levels were already at an acceptable state for quietness and noise quality, and that the production engine would reduce the noise levels a further 12–15 decibels. Boeing also announced that the company would probably build the 7J7 in two versions; the widely known 150-seat version would be joined by a smaller-capacity, 100-to-115 seat version, which might have a different fuselage size but still be powered by GE's UDF. [19] The miniature concept was called the 7J7-110. It would be developed by the same 7J7 team for commonality savings, and the 7J7-110 would be launched 6–12 months after the larger 7J7's kickoff. [20] In December 1986, however, an official from European airframe rival Airbus claimed that Boeing was offering airlines a 110-seat propfan plane and a 150-or-more seat airliner with ducted fans. [21] The claim seemed to be verified when Boeing publicly announced its consideration of using wing-mounted engines with the International Aero Engines (IAE) SuperFan in January 1987. [22] At the same time, the company also reversed its consideration of the smaller 7J7 model, choosing to promote a new 737 derivative instead. [23] [24] Boeing recommitted to the aft-mounted UDF in April, [25] albeit one day after IAE announced that it could not complete the engine by its previous May 1992 target date. [26] Against the protests of Allison and Pratt & Whitney (which had joined Allison in its propfan effort), Boeing also rejected the 578-DX engine due to insufficient power, even though it had not yet tested the engine in flight. [27]

Potential customers, who could afford to be choosier in an oversupplied world aircraft market, [28] were concerned about the economics and noise of the unproven propfan engines, though. The frequent major changes in the aircraft's design also discouraged airplane buyers from committing. [29] Boeing neglected to survey the needs of different airlines before visiting them on a road show, so it was surprised by the unenthusiastic overall response to the 7J7 after the airframer had put so many resources into development. [30] However, by May 1987, the 7J7 was on schedule to begin its official marketing campaign on July 1 [27] and to start manufacturing on September 1 of that year. [31] Boeing did attract public interest in the spring from British Airways, [32] which was considering the 7J7 to replace its 35 Boeing 737-200 aircraft. [33] Also, despite its chairman Robert Crandall saying 12 months earlier that fuel prices were too low to order any propfan aircraft by 1991, [34] American Airlines announced in early August 1987 that it was investigating larger, stretched versions of the 7J7 for a possible order of 100 aircraft. [35]

Postponement

Later that month, Boeing pushed back the scheduled certification of the 7J7 from 1992 to 1993, [36] saying that the market needed time to decide whether it wanted a 140-seat or a 170-seat airplane. [37] In justifying the decision, Boeing mentioned that SAS, British Airways, and American Airlines were the most enthusiastic prospective buyers, but the two European carriers chose a smaller plane, while American wanted the larger size. [36] Other reports had only mentioned SAS preferring the smaller size, but favoring the bigger plane was a consensus of either US-based airlines or a core group of about a dozen airlines that had expressed the most desire in the aircraft. [38] [39] Boeing also expressed worry that if the 7J7 were initially designed at the larger size, the GE UDF would be able to accommodate it, but the UDF engine core might not be capable enough to power future stretches of the 7J7. [40]

On December 16, 1987, Boeing delayed the availability date of the 7J7 indefinitely. [41] The number of engineers devoted to the 7J7, which had already been reduced from 1,000 to 900 in October and then to 600 by December, would be reduced again to 300 in the following weeks. [42] Although SAS publicly stated that it was still ready to order 100 7J7 aircraft in April 1988, [43] the lack of a similar-sized domestic order led Boeing to instead concentrate its resources on further developments of the Boeing 737 and the Boeing 757. By May 25, 1988, while announcing an order for 50 Boeing 757s and 50 further options from American Airlines, Boeing said that it had begun a total rethink about the 7J7 project, dropping the 7J7 name in favor of the more generic term "new medium-sized jet transport." [44]

The 7J7 project technically continued for a long time afterward, although it never again came close to an official launch. In December 1990, the Japanese government was still urging Boeing to build the 7J7, saying that they preferred it to the 777. [45] Two months later, Boeing confirmed that it was still meeting with its Japanese partners twice a year to discuss the 7J7, which was now framed as an eventual replacement for the 737. The aircraft had also devolved to fill a 100 to 170-seat category, a much less narrowly defined market target than before, and Boeing was no longer sure whether it should be a single-aisle or twin-aisle aircraft. [46] Boeing chairman Frank Shrontz renewed the joint 7J7 development agreement with the Japanese firms in Hawaii, and planned to modify their memorandum of understanding. [47] By 1994, Boeing still denied reports that Japan had ended funding of the 7J7, stating that Boeing and Japan each had five people working on the project. [48] Although the demise of the 7J7 project disappointed their aviation industry, Japanese companies contributed significantly larger percentages of subsequent Boeing projects (about 15% of the Boeing 767 and 25% of the Boeing 777). Japanese industry is also a primary foreign partner on the Boeing 787 Dreamliner.

Rudy Hillinga, who in 1985 tried unsuccessfully to sell the 7J7 to Lufthansa as Boeing's head of sales in Germany, [29] later said that he helped kill the 7J7 with Lufthansa's support. Hillinga claimed that if Boeing had continued with the 7J7 effort, the 737 never would have accumulated 10,000 aircraft sales by the early 2010s. [49] However, Alan Mulally, who was director of engineering for the 7J7 and would become the CEO of Ford Motor Company two decades later, stated that the 7J7 was one of the best research and development investments that Boeing ever made. [50]

Competition

Competing with the 7J7 for airline interest was McDonnell Douglas's proposed MD-91 and MD-92, two propfan-powered derivatives of the MD-80; the proposed clean-sheet aircraft MD-94X, another McDonnell Douglas aircraft powered by propfans; [51] the Airbus A320; and Boeing's own 737. The A320 featured a lot of similar advanced technology and electronics but was powered by conventional turbofan engines, as Airbus had rejected propfan technology in 1980, before the A320 was conceived. [52] Both McDonnell Douglas and Airbus believed that Boeing never intended to build the 7J7. [53] [29] The Boeing 737 Next Generation and the 777 incorporate many of the proposed 7J7 improvements.

Design

(Note: This section reflects what was known about the 7J7 concept in August 1987, right before its envisioned entry date was delayed. At that moment, the aircraft was most likely to be launched and was defined to its greatest detail.)

The aircraft was planned to include advanced technology and electronics, [1] such as:

The sum of all these features promised better fuel consumption by 60 percent compared to any existing large passenger aircraft technology at the time. [55] 43 percentage points of those savings would be due to the propfan engines, 11 percentage points from aerodynamic refinements, four percentage points from structural changes, and two percentage points from systems improvements. [56] Computer technology would reduce the amount of wires and connectors by half, saving about 1,300 pounds (590 kg) in wire weight from 46 miles (74 kilometres) of wiring removed, and 250 pounds (110 kg) in connector weight. [57]

Boeing planned to save 2,000 to 2,500 pounds (910 to 1,130 kg) in weight through the use of aluminum-lithium (Al–Li) and composites. [56] The airframer hoped to build the 7J7's wings out of aluminum-lithium, despite the material costing about three times more to use than conventional aluminum alloys. [58] Claiming greater knowledge of Al–Li than its competitors, [9] Boeing expected that aluminum-lithium alloys, which were then in their second generation of commercial availability, [59] would save eight percent in weight compared with current aluminum alloys, [57] or about 800 lb (360 kg). The aircraft could also have many parts built out of composites, including most of the structure behind the aft pressure bulkhead. [56] In the primary structure, Boeing planned to use carbon fiber for the vertical fin, horizontal fin, beams, and stanchions. The secondary structure would contain carbon fiber in the rudder, elevator, aileron, flaps, nose gear and main landing gear doors, engine cowling, and wingtips. Combined carbon and glass fiber would be used for the fixed trailing edges of the wings and empennage, the flap track fairings, wing-to-body fairings, and engine strut fairings. [60]

Cabin

The 7J7 was to have a twin-aisle [1] (2+2+2) seating configuration, giving a wide and spacious cabin for its class, with no passenger more than one seat from an aisle. Alternatively, the aircraft could fit a high-density, seven-abreast (2+3+2) seating configuration with 17-inch wide (43 cm) seats and 18-inch wide (46 cm) aisles. The fuselage diameter of 188 inches (478 cm) [61] is wider than earlier candidates, such as a 164-inch diameter (417 cm), six-abreast design (with a single aisle, although a twin-aisle configuration was considered) [10] and a 180-inch diameter (457 cm), six-abreast twin-aisle design. [62] However, Boeing retained a backup option of a 155-inch diameter (394 cm), single-aisle fuselage design, [31] as the widebody design caused a 6,000 lb (2,700 kg) increase in operating weight compared to a narrowbody design. [63]

The twin-aisle setup would reduce passenger onboarding and deboarding times by ten minutes, [64] allowing airlines to plan for 50-percent faster turnaround times compared to its competitors; [31] Boeing's research found that even two 18-inch skinny aisles (46 cm) turned passengers around faster than one 26-inch wide aisle (66 cm). [65] The cabin contained modular seat elements so that seat pitch (distance between rows), seat width, and armrest width could be adjusted. [10] It also offered an airline the ability to easily change between six-abreast and seven-abreast configurations overnight. [66]

Flight capability

Boeing also provided a higher gross weight option for the plane by configuring the in-fuselage part of the wing to hold fuel. This option increased the 7J7's range from 2,700 to 4,250 nautical miles (3,110 to 4,890 mi; 5,000 to 7,870 km) for a standard (six-abreast) seating configuration, and from 2,250 to 3,900 nautical miles (2,590 to 4,490 mi; 4,170 to 7,220 km) for a high-density (seven-abreast) seating configuration. [67] Boeing's 7J7 design had the UDF as the baseline engine with a cruise speed of Mach 0.83, according to General Electric, [68] and the aircraft would cruise at an altitude of 41,000 feet (12,000 m). [64]

Storage

A volume of 1,800 cubic feet (50.9 m3) was available for storage. [69] 937 cu ft (26.54 m3) was available in the forward hold, and 555 cu ft (15.72 m3) was available in the aft hold. [70] It could be used for bulk storage or to hold standard LD3-46 unit load devices, a smaller size of air cargo container that was entering usage with the debut of the Airbus 320. [66] The amount of available cabin stowage would be 3 cu ft (85 L) per passenger, an increase from the per passenger standard of 2 cu ft (57 L) at the time. [64]

Specifications

General characteristics

Performance

See also

Related development

Aircraft of comparable role, configuration, and era

Related Research Articles

<span class="mw-page-title-main">McDonnell Douglas MD-90</span> Single-aisle airliner by McDonnell Douglas

The McDonnell DouglasMD-90 is an American five-abreast single-aisle airliner developed by McDonnell Douglas from its successful model MD-80. The airliner was produced by the developer company until 1997 and then by Boeing Commercial Airplanes. It was a stretched derivative of the MD-80 and thus part of the DC-9 family. After the more fuel-efficient IAE V2500 high-bypass turbofan was selected, Delta Air Lines became the launch customer on November 14, 1989. The MD-90 first flew on February 22, 1993, and the first delivery was in February 1995 to Delta.

<span class="mw-page-title-main">Libyan Airlines</span> Flag carrier of Libya

Libyan Airlines, formerly known as Libyan Arab Airlines over several decades, is the flag carrier of Libya. Based in Tripoli, it operates scheduled passenger and cargo services within Libya and to Europe, North Africa and the Middle East, the majority of which leave from Tripoli International Airport. Benina International Airport in Benghazi serves as a secondary base. Libyan Airlines also operates Hajj services. The company is wholly owned by the government of Libya.

<span class="mw-page-title-main">Propfan</span> Type of aircraft engine

A propfan, also called an open rotor engine, open fan engine or unducted fan, is a type of aircraft engine related in concept to both the turboprop and turbofan, but distinct from both. The design is intended to offer the speed and performance of a turbofan, with the fuel economy of a turboprop. A propfan is typically designed with a large number of short, highly twisted blades, similar to the (ducted) fan in a turbofan engine. For this reason, the propfan has been variously described as an "unducted fan" (UDF) or an "ultra-high-bypass (UHB) turbofan".

<span class="mw-page-title-main">Tupolev Tu-334</span> Airliner by Tupolev

The Tupolev Tu-334 was a Russian short-to-medium range airliner project that was developed to replace the aging Tu-134s and Yak-42s in service around the world. The airframe was based on a shortened Tu-204 fuselage and a scaled-down version of that aircraft's wing. Unlike the Tu-204, however, the Tu-334 has a T-tail and engines mounted on the sides of the rear fuselage instead of under the wings. With the nationalisation of the Russian aircraft companies in 2009 to form United Aircraft Corporation it was decided not to continue with the programme.

<span class="mw-page-title-main">McDonnell Douglas MD-94X</span> Proposal for a propfan-powered airliner

The McDonnell Douglas MD-94X was a planned propfan-powered airliner, intended to begin production in 1994. Announced in January 1986, the aircraft was to seat between 160 and 180 passengers, possibly using a twin-aisle configuration. An all-new design that was investigated internally since at least 1984, the MD-94X was developed in the mid-1980s to compete with the similar Boeing 7J7. The price of oil would have to be at least US$1.40 per gallon for McDonnell Douglas to build the plane, though. Configuration was similar to the MD-80, but advanced technologies such as canard noseplanes, laminar and turbulent boundary layer control, side-stick flight control, and aluminum-lithium alloy construction were under consideration. Airline interest in the brand-new propfan technology was weak despite claims of up to a 60% reduction in fuel use, and both aircraft were canceled.

<span class="mw-page-title-main">General Electric GE36</span> US experimental propfan

The General Electric GE36 was an experimental aircraft engine, a hybrid between a turbofan and a turboprop, known as an unducted fan (UDF) or propfan. The GE36 was developed by General Electric Aircraft Engines, with its CFM International equal partner Snecma taking a 35 percent share of development. Development was cancelled in 1989.

IAE International Aero Engines AG is a Zürich-registered joint venture aeroengine manufacturing company.

<span class="mw-page-title-main">Nigeria Airways</span> Defunct airline (1958–2003)

Nigeria Airways Ltd., more commonly known as Nigeria Airways, was a one-time Nigerian airline. The company was founded in 1958 after the dissolution of West African Airways Corporation (WAAC). It held the name West African Airways Corporation Nigeria until 1971, when it was renamed, until it ceased operations in 2003. The government of Nigeria owned a majority of the airline (51%) until 1961, when it boosted its shareholding in the company to 100% and made it the country's flag carrier. At the time of dissolution, the airline's headquarters were at Airways House in Abuja. Operations were concentrated at Murtala Muhammed International Airport and served both domestic and international destinations mainly concentrated in West Africa; the network also had points in Europe, North America and Saudi Arabia. The airline was managed by a number of foreign companies, including British Airways, KLM and South African Airways.

The Yakovlev Yak-46 was a proposed aircraft design based on the Yak-42 with two contra-rotating propellers on the propfan located at the rear. The specification of the Samara turbofans was in the 11,000 kg thrust range. Though proposed in the 1990s, production of the Yak-46 never commenced.

<span class="mw-page-title-main">Embraer/FMA CBA 123 Vector</span> Regional airliner prototype

The Embraer/FMA CBA 123 Vector was a 1990 turboprop aircraft designed for regional flights, to carry up to 19 passengers. The program arose from a partnership between the Brazilian company Embraer and the Argentine FMA. The project was an advanced turboprop aircraft for its time, including advanced technology in avionics, aerodynamics, and propulsion.

<span class="mw-page-title-main">Progress D-27</span> Propfan engine

The Progress D-27 is a three-shaft propfan engine developed by Ivchenko Progress, and manufactured by Motor Sich in Ukraine. The gas generator was designed using experience from the Lotarev D-36 turbofan. The D-27 engine was designed to power more-efficient passenger aircraft such as the abandoned Yakovlev Yak-46 project, and it was chosen for the Antonov An-70 military transport aircraft. As of 2019, the D-27 is the only contra-rotating propfan engine to enter service.

<span class="mw-page-title-main">General Electric GE38</span> Gas turbine

The General Electric GE38 is a gas turbine developed by GE Aviation for turboprop and turboshaft applications. It powers the Sikorsky CH-53K King Stallion as the T408.

<span class="mw-page-title-main">Antonov An-180</span> Type of aircraft

The Antonov An-180 was a Ukrainian design for a twin-aisle medium-range propfan airliner. Although the design was completed by the Antonov Design Bureau in 1994, the type was not built.

<span class="mw-page-title-main">Pratt & Whitney/Allison 578-DX</span> Experimental aircraft engine

The Pratt & Whitney/Allison 578-DX was an experimental aircraft engine, a hybrid between a turbofan and a turboprop known as a propfan. The engine was designed in the 1980s to power proposed propfan aircraft such as the Boeing 7J7 and the MD-91 and MD-92 derivatives of the McDonnell Douglas MD-80. As of 2019, it is still one of only four different contra-rotating propfan engines to have flown in service or in flight testing.

MPC 75 was an aircraft project of MPC Aircraft GmbH, a subsidiary of Deutsche Airbus. Work on the project was done mainly between 1988 and 1992 in Hamburg, Germany. Predevelopment work was finished, however the project never got the "go ahead" and never made it into full development.

The IAE V2500SF SuperFan was a design study for a high-bypass geared turbofan derived from the IAE V2500. It was offered as the primary engine option for the Airbus A340-200 and 300 in January 1987. Although several customers signed preliminary contracts for this variant, the International Aero Engines board decided in April 1987 to stop the development of the SuperFan, which forced Airbus to partly re-design the A340.

<span class="mw-page-title-main">Progress D-236</span> Propfan engine

The Progress D-236 was an experimental aircraft engine, a hybrid between a turbofan and a turboprop known as a propfan. Also known as the Lotarev D-236T, the three-shaft geared engine was designed in the 1980s and 1990s to power proposed propfan aircraft such as the Tupolev Tu-334, Ilyushin Il-118, and Ilyushin Il-88.

<span class="mw-page-title-main">Kuznetsov NK-93</span> 1980s Soviet propfan aircraft engine

The Kuznetsov NK-93 was a civilian aircraft engine, a hybrid between a turbofan and a turboprop known as a propfan. The engine was also unique in having a separate duct around the contra-rotating propellers, as most other propfans are unducted. Once described in a respected aviation encyclopedia as "potentially the most fuel-efficient aircraft jet engine ever to be tested", the NK-93 was targeted for derivatives of Soviet/Russian airliners such as the Ilyushin Il-96, Tupolev Tu-204, and Tupolev Tu-330. Five in-flight engine tests were conducted on the NK-93 from December 2006 to December 2008.

The Ilyushin Il-90 was a twin-engine, widebody aircraft proposed by the Ilyushin Design Bureau. First mentioned at the Farnborough air show in 1988, the Il-90 was a replacement for the Ilyushin Il-62M long-range narrowbody airliner. The Il-90 was designed to carry 200 passengers a distance of 5,900 to 7,000 nautical miles. On a 540 nmi sector, per-passenger fuel consumption would be 18 to 19 grams per kilometre. Powerplant choices included the NK-92, an 18,000-kilogram-force thrust ducted propfan engine that was related to the Kuznetsov NK-93.

The Rolls-Royce RB529 Contrafan was a high-thrust aircraft engine proposed by Rolls-Royce in the 1980s to power long-range wide-body airliners.

References

  1. 1 2 3 4 5 6 7 Green, William; Gordon Swanborough; John Mowinski (1987). Modern Commercial Aircraft. New York, NY USA: Crown Publishers, Inc. p. 85. ISBN   0-517-63369-8.
  2. "Boeing's 150-seat 7 Dash 7 programme advanced?". Flight International. July 4, 1981. p. 7. ISSN   0015-3710.
  3. Learmount, David (June 13, 1981). "Is three a crowd?". Flight International. Vol. 3762, no. 119. p. 1811. ISSN   0015-3710.
  4. Jouzaitis, Carol (June 14, 1988). "McDonnell-Douglas gets $1.5 billion order". Chicago Tribune . ISSN   1085-6706.
  5. Donne, Michael (March 16, 1984). "Boeing-Japan airbus rival move". World Trade News. Financial Times . No. 29273. p. 6. ISSN   0307-1766.
  6. 1 2 "Boeing reveals its plans for the 1990s". Air Transport. Flight International . Vol. 127, no. 3947. February 16, 1985. pp. 4–5. ISSN   0015-3710.
  7. Harris, Roy J. Jr.; Wysocki, Bernard Jr. (January 14, 1986). "Ready for takeoff? Venture with Boeing is likely to give Japan big boost in aerospace - Seattle firm plans to share technology that makes it a major U.S. exporter - Goal: A new airliner in 1992". Wall Street Journal. p. 1. ISSN   0099-9660.
  8. "Propfans ready by 1990". Paris Report. Flight International. June 8, 1985. p. 5. ISSN   0015-3710. Archived (PDF) from the original on September 25, 2014. Retrieved March 28, 2019.
  9. 1 2 3 Gavaghan, Helen (March 13, 1986). "Joint venture brings back propellers". Technology. New Scientist . Vol. 109, no. 1499. p. 27. ISSN   0028-6664.
  10. 1 2 3 Moxon, Julian (October 26, 1985). "7J7: Boeing sets the pace". Flight International . Vol. 128, no. 3983. pp. 25–28. ISSN   0015-3710.
  11. "Boeing, 3 aircraft makers mull future passenger plane". Machinery. Nihon Keizai Shinbun . August 27, 1985. p. 10. ISSN   0021-4388.
  12. "Boeing to test new Allison engines for use in airliners". Finance. Indianapolis Star . December 21, 1985. p. 33. ISSN   1930-2533 via Newspapers.com.
  13. Moll, Nigel (May 1987). "7J7: The next new Boeing". Flying . Vol. 114, no. 5. pp. 37, 39. ISSN   0015-4806.
  14. "Shorts and Saab board 7J7". Air Transport. Flight International . April 5, 1986. p. 6. ISSN   0015-3710.
  15. Donne, Michael (December 3, 1986). "Australians to have stake in new Boeing". World Trade News. Financial Times . No. 30100. p. 5. ISSN   0307-1766.
  16. Lane, Polly (March 11, 1986). "Scandinavian airline eyes Boeing's 7J7: SAS chairman wants new jet to stress passenger comfort". Economy. Seattle Times . p. B1. ISSN   0745-9696. ProQuest   385060695.
  17. Donoghue, J. A. (July 1986). "GPA ready for airline rush to leasing". Air Transport World . Vol. 23, no. 7. pp. 36+. ISSN   0002-2543. Gale   A4397886.
  18. "GE's UDF flies again" (PDF). Air Transport. Flight International . Vol. 130, no. 4027. September 6, 1986. p. 23. ISSN   0015-3710.
  19. "Boeing delighted with UDF" (PDF). Farnborough First News. Flight International. Vol. 130, no. 4027. September 6, 1986. p. 14. ISSN   0015-3710.
  20. "Boeing exploring smaller 7J7". News Digest. Airline Executive. Vol. 10, no. 12. December 1986. p. 9. ISSN   0278-6702.
  21. "SuperFan-powered A340 a possibility" (PDF). Air Transport. Flight International . Vol. 130, no. 4040. December 6, 1986. p. 4. ISSN   0015-3710.
  22. Hamilton, Martha M. (February 8, 1987). "Firms give propellers a new spin". Business. Washington Post . pp. H1, H4. ISSN   0190-8286. Archived from the original on April 2, 2019. Alt URL
  23. Donne, Michael (January 23, 1987). "Boeing alters strategy to offer engine choice on 7J7 airliner" (PDF). Financial Times . No. 30141. p. 18. ISSN   0307-1766.
  24. O'Lone, Richard G. (January 26, 1987). "Designs for the 7j7" . Air Transport. Aviation Week & Space Technology . Vol. 126, no. 4. pp. 31–32. ISSN   0005-2175.
  25. "Boeing selects GE fan engine for use on new 7J7 airliners" . Washington Post . April 8, 1987. ISSN   0190-8286.
  26. Gavaghan, Helen (April 16, 1987). "Superfan loses favour among airline companies". This Week. New Scientist . Vol. 114, no. 1556. p. 14. ISSN   0028-6664.
  27. 1 2 3 Warwick, Graham; Moxon, Julian (May 23, 1987). "The power of persuasion". Flight International . pp. 39–41. ISSN   0015-3710.
  28. Labich, Kenneth; Prewitt, Edward (September 28, 1987). "Boeing battles to stay on top: To maintain its lofty status, this renowned aerospace giant will have to beat back ferocious competitors and persuade its restive shareholders to stand by for big earnings. Neither task will be easy for the company's new chief executive". Fortune.
  29. 1 2 3 4 Sweetman, Bill (September 2005). "The short, happy life of the prop-fan". Air & Space Magazine . Vol. 20, no. 3. pp. 42–49. ISSN   0886-2257. OCLC   109549426.
  30. Carrison, Dan (2003). "Chapter 5: Boeing's race to deliver the 777 wide body". Deadline!: How premier organizations win the race against time. American Management Association. p.  170. ISBN   0-8144-0726-9. OCLC   937571153.
  31. 1 2 3 "7J7 double aisle for Paris". Industry. Flight International . May 23, 1987. ISSN   0015-3710.
  32. Donne, Michael (April 15, 1987). "British Airways spreads its wings in 6 billion pound spending spree: A newly privatised airline's plans for re-equipping its ageing jet fleet" (PDF). UK News. Financial Times. p. 10.
  33. Lane, Polly (May 27, 1987). "British Airways may be first in line for new Boeing 7J7". Business. Seattle Times . p. G1. ISSN   0745-9696. ProQuest   384846553. British Airways, a major Boeing Co. customer, is considering replacing its fleet of 35 Boeing 737-200 jetliners with the company's proposed 150-seat 7J7. The London-based airline may be one of the first customers for the new jet, said Colin Marshall, president. He was here yesterday to review Boeing's plans and timing for the new jet and to talk about potential orders for other Boeing jets.
  34. Banks, Howard (August 11, 1986). "Though still on the drawing boards, Boeing's new passenger jet is already in trouble. No sweat on the technology, but the giant got... Mugged by $10 oil". Forbes . Vol. 138, no. 3. pp. 30–33. ISSN   0015-6914.
  35. "American Airlines expects to place order for 100 jets". Wall Street Journal. August 7, 1987. p. 1. ISSN   0099-9660. American said two of the models -- the Boeing 7J7 and the McDonnell Douglas MD-91/92 -- exist only in design. Each would use new propfan engines, which are powered by high-speed propellers and are significantly more fuel efficient than current jet engines. American said it is studying "stretch" versions of the aircraft, which would carry 15 to 25 more passengers than the 150-passenger Boeing 727, because it believes air traffic constraints may eventually force the industry to fly fewer planes.
  36. 1 2 Joseph, Gloria (September 3, 1987). "Why Boeing shelved the 7J7" . The Journal of Commerce.
  37. Gavaghan, Helen (September 17, 1987). "Communication standards take to the air". Technology. New Scientist . Vol. 115, no. 1578. p. 44. ISSN   0028-6664.
  38. Kaletsky, Anatole (August 25, 1987). "Doubts over cost and size delay Boeing propfan project" (PDF). American News. Financial Times . No. 30320. p. 4. ISSN   0307-1766.
  39. Moxon, Julian (September 5, 1987). "Boeing delays 7J7 certification" (PDF). Air Transport. Flight International. Vol. 132, no. 4078. p. 4. ISSN   0015-3710. Archived from the original (PDF) on May 1, 2016.
  40. Hamilton, Scott (November 1987). "War of the three plane-makers". Euromoney . Euromoney Trading Limited. pp. SS52+. ISSN   0014-2433. Gale   A6159334.
  41. "Company news; staff cutbacks for Boeing jet" . New York Times. December 16, 1987. p. D3.
  42. Donne, Michael (December 21, 1987). "New delay to prop-fan project" (PDF). Overseas News. Financial Times . No. 30420. p. 8. ISSN   0307-1766.
  43. Bailey, John (April 9, 1988). "SAS: Moments of truth: Although SAS failed in its bid for partial control of British Caledonian, the exercise did demonstrate determination to become one of Europe's 'Big Five' carriers after 1992". Flight International . pp. 22–25, 28. ISSN   0015-3710. Archived from the original on November 11, 2012.
  44. Oram, Roderick (May 27, 1988). "Boeing wins second 757 airliner order in two days". World Trade News. Financial Times . No. 30549. p. 7. ISSN   0307-1766.
  45. Iritani, Evelyn (December 28, 1990). "Japanese aren't giving up on the 7J7 - funding continues - $70 million, so far". News. Seattle Post-Intelligencer . p. A1.
  46. Bailey, John (February 27, 1991). "Boeing and Japanese continue 7J7 studies". Headlines. Flight International . Vol. 139, no. 4256. p. 4. ISSN   0015-3710. Gale   A10424015.
  47. "Boeing eyes reviving propfan-powered 7J7 --- GE has no word, but says it stands ready if called". Commercial. Aerospace Propulsion. Vol. 2, no. 5. McGraw-Hill. March 7, 1991. p. 1A. ISSN   1050-5245 via Factiva.
  48. "Boeing denies dropping studies for 150-seat 7J7". Seattle Times . January 6, 1994. ISSN   0745-9696. ProQuest   384103968.
  49. Hillinga, Rudy (July 12, 2012). "[Response] It's official: United orders 150 firm Boeing jets (100 Max, 50 900ERs)". Archived from the original on September 28, 2015. Retrieved August 19, 2019 via Leeham News and Analysis.
  50. "For the love of flying". Design News. March 4, 1996. Archived from the original on April 10, 2019. Retrieved August 20, 2019.
  51. Haggerty, James J. (August 1987). "Toward future flight" (PDF). Spinoff (1987 ed.). NASA. pp. 30–33. Archived from the original on April 12, 2009.
  52. "Technical considerations: Strategy of Airbus development (translation of Aviazione, April 1986, pp. 177–179)". Europe report: Science and technology. October 6, 1986. pp. 3–7. OCLC   45509880.
    • "Technical considerations: Strategy of Airbus development". Europe report: Science and technology. October 6, 1986. pp. 3–7. Archived from the original on August 19, 2019. Retrieved August 19, 2019 via Defense Technical Information Center.
  53. O'Guin, Michael; Kelly, Kim (2012). "9: Collecting intelligence and deciphering the competition". Winning the big ones: How teams capture large contracts. Lulu.com. pp. 274–275. ISBN   978-1-300-41334-9. OCLC   927369135.
  54. "GEC AVIONICS NEWS No. 081 :: Rochester Avionic Archives". rochesteravionicarchives.co.uk. Retrieved 2021-03-18.
  55. Jouzaitis, Carol (January 26, 1986). "Boeing flies in face of odds". Chicago Tribune . ISSN   1085-6706.
  56. 1 2 3 Woolsey, James P. (March 1986). "Boeing continues effort to leapfrog current transport offerings; manufacturer is stressing lower unit costs and greater emphasis on passenger appeal in attempts to put program together for 1992". Air Transport World . Vol. 23. pp. 44+. ISSN   0002-2543. Gale   A4154715.
  57. 1 2 "Boeing gives 7J7 details". Globe & Mail. Toronto, Ontario, Canada. March 27, 1986. p. B14. ISSN   0319-0714.
  58. "Aluminium-lithium into service" (PDF). World News. Flight International . Vol. 130, no. 4021. July 26, 1986. p. 2. ISSN   0015-3710.
  59. Rioja, Roberto J.; Liu, John (September 2012). "The evolution of Al-Li base products for aerospace and space applications" (PDF). Metallurgical and Materials Transactions A. 43 (9). Springer US (published 31 March 2012): 3325–3337. Bibcode:2012MMTA...43.3325R. doi:10.1007/s11661-012-1155-z. ISSN   1073-5623. S2CID   136580310. Archived from the original on 20 February 2019. Retrieved 9 March 2019.
  60. National Aeronautics and Space Administration (NASA) (April 10, 1987). "7J7 materials technology: Graphite composites". Department of Housing and Urban Development and certain independent agencies appropriations for fiscal year 1988: Hearings before a subcommittee of the Committee on Appropriations, United States Senate, One Hundredth Congress, first session, on H.R. 2783 (Report). Vol. 2. 100th Congress, United States Senate Committee on Appropriations, Subcommittee on HUD—Independent Agencies. p. 1137. hdl:2027/mdp.39015028791492.
  61. Learmount, David (June 13, 1987). "Propfan: the price factor". Flight International . pp. 76–79. ISSN   0015-3710. Archived from the original on March 7, 2016.
  62. Schefter, Jim (April 1987). "Engineering tomorrow's airliners". Popular Science . Vol. 230, no. 4. pp. 49, 52, 98. ISSN   0161-7370.
  63. "Propfan progress has airlines planning for the future". Research & Development . Advantage Business Media. July 1987. pp. 41+. ISSN   0746-9179.
  64. 1 2 3 Gapay, Les (June 9, 1987). "Boeing hopes air show clears its 7J7 for takeoff". Business. Seattle Post-Intelligencer. p. B8.
  65. Cawley, Janet; Rice, William (October 26, 1986). "Care in the air: You say that flying is more punishment than pleasure? Well, things are looking up" . Sunday Travel Magazine. Chicago Tribune . p. 6. ISSN   1085-6706.
  66. 1 2 Donoghue, J. A. (September 1987). "Boeing 7J7 cabin an innovation greenhouse". Air Transport World . Vol. 24, no. 9. pp. 40–44. ISSN   0002-2543. OCLC   16640763. Gale   A5149805.
  67. 1 2 3 Learmount, David (May 2, 1987). "Boeing offers long-range 7J7". World News. Flight International . p. 2. ISSN   0015-3710.
  68. 1 2 "Manufacturers positioning for coming competitive battles". Air Transport World . Vol. 23, no. 9. September 1986. pp. 20–25. ISSN   0002-2543. Gale   A4426985.
  69. 1 2 Condom, Pierre (January 1987). "Boeing 7J7 design to be frozen in July". Interavia (in French). Vol. 42, no. 1. pp. 23–26. ISSN   0020-5168. OCLC   15149609. Archived from the original on January 31, 2018. Retrieved March 25, 2019 via ACTUALITE Aéronautique.
  70. 1 2 3 4 5 6 Sutcliffe, Peter L. (November 13, 1987). The Boeing 7J7—The evolution of technology and design. International Pacific Air and Space Technology Conference and Exposition. SAE 1987 Transactions: Aerospace. Melbourne, Australia: SAE International (published September 1988). pp. 73+. doi:10.4271/872405. ISSN   0148-7191. JSTOR   44473078. OCLC   5817963573.
  71. 1 2 3 "Boeing 7J7". Interavia (in French). August 1987. ISSN   0020-5168. Archived from the original on January 31, 2018. Retrieved March 25, 2019 via ACTUALITE Aéronautique.
  72. Warwick, Graham (August 15, 1987). "UHB: the acid test". Flight International. pp. 22–23. Retrieved March 22, 2019.
  73. "Dowty to build UDF blades". World News. Flight International . Vol. 132, no. 4085. October 24, 1987. p. 3. ISSN   0015-3710.

Bibliography