BAC One-Eleven
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BAC One-Eleven | |
---|---|
Type | Short-range jetliner |
Manufacturer | British Aircraft Corporation |
Maiden flight | 1963-08-20 |
Introduced | 1965 |
Produced | 1963-1989 |
Number built | 244 |
The BAC One-Eleven was a British short-range jet airliner of the 1960s and 1970s. Conceived by Hunting, it was developed and produced by the British Aircraft Corporation when Hunting merged into it along with other British aircraft makers in 1960.
The One-Eleven was designed to replace the Vickers Viscount. It was the second short-haul jet airliner to enter service, the first being the French Sud Aviation Caravelle. Due to its later service entry, the One-Eleven took advantage of more efficient engines and airline experience of jets. This made it popular, with over half of the sales at its launch being in the largest and most lucrative markets, the United States. The One-Eleven was one of the most successful British airliner designs, and served until its widespread retirement in the 1990s due to noise restrictions.
As of August 2006 a total of 16 BAC One-Eleven aircraft (all variants) remain in airline service with International Trans Air Business (2), Libyan Arab Airlines (2), Aero Asia International (3), Indonesia Air Transport (2), GST Aero (1), Romavia (3) and Mia Airlines (3).
Contents |
[edit] History
In 1956, both Vickers and Hunting started design studies on jet replacements for the Viscount. Vickers offered a 140-seat development of its VC10 project: the VC11. Hunting offered the all-new 100-seat Hunting 107.
In 1960 Hunting merged with Vickers, Bristol, and English Electric to form BAC at government insistence. In 1961, BAC decided to continue work on the Hunting 107 as a private venture. It redesignated it One-Eleven (the first BAC project and the eleventh Vickers civil aircraft). Because of the short delay over the merger, the One-Eleven was able to use the new Rolls-Royce Spey turbofan, greatly improving its fuel economy. BAC was concerned the aircraft was too large to fit the Viscount role in the original Hunting configuration and reduced its capacity to 80 seats. This version became the One-Eleven 200, the original design having retroactively become the 100.
[edit] The One-Eleven 200, 300 and 400
On 9 May 1961 British United Airways (BUA) placed the first order for ten One-Eleven 200s. On 23 October Braniff in the United States ordered six. Other orders followed from Mohawk for four, Kuwait Airways for three, and Central African Airways for two. Braniff subsequently doubled its order to 12, while Aer Lingus ordered four. Western Airlines ordered ten aircraft but later cancelled. Bonanza Airlines also wanted to order One-Elevens at a later stage but was stopped by a protectionist action of the US Department of Transportation.
In May 1963, BAC announced the One-Eleven 300 and 400. The new versions used the Mk. 511 version of the Spey with increased power, allowing more fuel upload and hence longer range. There were a number of other changes, with the main visual difference being in the nose wheel doors. The difference between the 300 and 400 lay in their equipment and avionics, with the 400 intended for sales in the USA and thus equipped with US instruments. American Airlines ordered 15 aircraft on 17 July 1963, bringing the order total to 60, plus options for many more. This was assumed to be enough for BAC to break even on the project. In retrospect, however, many have doubted whether BAC and its successors made money on the One-Eleven.
The prototype (G-ASHG) rolled out of the Hurn assembly hall on 28 July 1963, its first flight following soon on 20 August. This was almost a year ahead of the competing US airliner, the Douglas DC-9. This lead was commercially most important, since — as shown by the Bonanza case — US authorities could refuse to approve sales of foreign aircraft to domestic airlines where an American alternative existed.
The One-Eleven prototype crashed with the loss of all on board on 22 October. The investigation led to the discovery of what became known as deep stall or superstall: a phenomenon which rendered the aircraft uncontrollable in pitch. To obviate this, BAC designed and added devices known as stick shakers and stick pushers to the One-Eleven's control system. It also redesigned the wing's leading edge to smooth airflow into the engines and over the tailplane.
Despite the crash, testing continued and customer confidence remained high. American Airlines and Braniff took up their optional orders and placed further ones in February 1964. Further orders came from Mohawk, Philippine Airlines and Helmut Horten who ordered the first Executive modificationm of the aircraft. By the end of 1964, 13 aircraft had rolled off the production line.
The One-Eleven was certificated and the first handover, of G-ASJI to BUA, was on 22 January 1965. After several weeks of route proving flights, the first revenue service flew on 9 April from Gatwick to Genoa. Braniff took delivery of their first aircraft on 11 March, while Mohawk received their first on 15 May. Deliveries continued, and by the end of 1965 34 aircraft had been received by customers. Demand continued to be buoyant, with a second production line set up at Weybridge.
[edit] The One-Eleven 500 and 475
In 1967 a larger 119-seat version was introduced as the One-Eleven 500 (also known as Super One-Eleven). This "stretched" version was delayed for at least a year while its launch customer BEA assessed its requirements. This gave competing US aircraft (the DC-9 and Boeing 737) the chance to make up for the One-Eleven's early penetration of their domestic market. The British aircraft's initial one-year advantage now turned into a one-year delay and the 500 failed to sell in the USA. Compared with earlier versions, the One-Eleven 500 was longer by 8ft 4in (2.54 m) ahead of the wing and 5ft 2in (1.57 m) behind it. The wing span was increased by 5 ft (1.5 m), and the latest Mk. 512 version of the Spey was used. The new version sold reasonably well across the world, particularly to European charter airlines. In 1971 it received an incremental upgrade to reduce drag and improve airfield performance.
BEA/British Airways 500 series aircraft varied significantly from other 1-11s on their request. The One-Eleven 510ED had a modified cockpit which incorporated instrumentation and avionics from or similar to that of the Hawker Siddeley HS.121 Trident, for better commonality with the type (which at the time was the BEA/BA shorthaul workhorse). Their additional equipment included a more sophisticated autoflight system, which allowed CAT II autolandings and included an autothrottle (autoland functionality was removed from most aircraft later on in their careers). The modifications went as far as reversing the "on" position of most switches to match that of the Trident, indeed he 510ED was so different from other One-Elevens and 500 series aircraft that a different type rating was required to fly it, despite the fact that aside from the flightdeck is was basically identical to all other 500 series aircraft [1].
Having faced competition "from above" with the aforementioned US aircraft by 1966, by 1970 the One-Eleven also faced competition "from below." The new competitor was the Fokker F.28. Available as a four-member "family," it was lighter, less complex, and cheaper. The One-Eleven 475 of 1970 was launched to compete with the F.28. It combined the 400 fuselage with the higher power and larger wing of the 500 and was intended for hot and high operations. Only ten One-Eleven 475s were sold. In 1977, the One-Eleven 670, a quiet and updated 475, was offered to the Japanese domestic market, failing to sell.
Total deliveries for 1966 stood at 46 aircraft, and another 120 were delivered by 1971. At this point orders slowed to a trickle. British production continued until 1982. There were two reasons why the production line was kept open for just 35 aircraft delivered over 11 years. First, BAC hoped that Rolls-Royce would develop the Spey, making possible further One-Eleven developments. Second, throughout the early part of the period Romania was negotiating to buy the entire One-Eleven programme and transfer production of the type to Bucharest.
[edit] Development projects
By 1974, BAC invested very significant effort into launching the One-Eleven 700. This had a longer body with a 134-seat interior and the projected Spey 67 engine producing greater power. It was approximately the same size as the latest DC-9s and 737s and would have been available in time to prevent large-scale defections by One-Eleven clients to McDonnell-Douglas and Boeing. Rolls-Royce was still recovering from bankruptcy, however, and the uprated Spey failed to materialise. An altogether less ambitious 700 made a reappearance in 1978 as a 500 with specially "hush-kitted" Speys which would be replaced by the proposed RB432 in the mid-1980s. This was offered to British Airways in competition with Boeing 737-200s and rejected.
In 1977, BAC merged with Hawker Siddeley to form British Aerospace (BAe) and the One-Eleven 800 was proposed with CFM-56 engines. It would have accommodated some 150 passengers in a mixed class layout. The One-Eleven 800's fate was involved with the development of a European competitor to ubiquitous US short/medium range airliners and it did not progress to the design stage.
[edit] The Rombac deal
In 1979, Romanian president Nicolae Ceauşescu signed the contract for One-Eleven licence production in Romania. This was to involve the delivery of three complete One-Elevens plus the construction of at least 22 in Bucharest, with reducing British content. It also involved Romanian production of Spey engines and certification of the aircraft to British and US standards. A market for up to 60 or even 80 cheap Romanian-built aircraft was mooted at the time, largely in China, the Third World and possibly Eastern Europe. The aircraft was redesignated Rombac 111.
The first flight of a Rombac 111 was on 18 September 1982 and production continued until 1989 at a much slower pace than foreseen in the contract: nine aircraft were delivered. The reasons why the Rombac initiative failed are three. First, Romania's economy and international position deteriorated to the point where supplies for One-Eleven manufacture slowed to a trickle. Second, the market foreseen by the Romanians failed to show an interest, though some Rombac machines were leased out to European operators. Third, the One-Eleven's noise level and fuel economy had failed to keep pace with US and West European competition. With reference to the last reason, Rolls-Royce repeatedly refused to allow its Tay engine to be used on Romanian One-Elevens. This reluctance is assumed to reflect fears that the Fokker 100, the Tay's launch airframe, would suffer from Romanian competition.
[edit] Operational history
Total production of the One-Eleven in British and Romanian factories was 244, with two airframes left incomplete in Romania. A major initiative to reengine corporate One-Elevens with Tay engines gathered pace in the USA in the late 1980s and early 1990s but came to nought after several successful test flights. Passive opposition from the engine maker among other factors is claimed to have sabotaged its chances of success.
One-Elevens served widely in the USA until displaced by indigenous Douglas DC-9 and Boeing 737 in the early 1970s. In Europe they were common, continuing in widespread use until the mid-1980s and into the 1990s. Many One-Elevens then moved to smaller airlines, notably in the Far East and Africa. The last major operations were in Nigeria, where they were grounded after a crash in 2002. Today only a handful are still operating, mainly in Africa, though corporate versions survive in the USA and Europe. A further nail in the coffin for the One-Eleven in Europe was the Stage III noise abatement regulations which took effect from March 2003. The costs in bringing the Rolls Royce Spey engines to in line with this with the development of an uprated hush kit proved an expensive prospect for the smaller operators still using this aircraft type. So very few were fitted with them and most European operators disposed of the type from their fleet. Several dozen One-Elevens are in storage and for sale around the world.
British Airways Flight 5390 had to make an emergency landing on 10 June 1990 when its windscreen blew out at altitude after the wrong bolts had been used to secure it. Captain Tim Lancaster was sucked half out of the cockpit by the pressure differential but survived, as did all the crew and passengers.
[edit] Variants
- BAC One-Eleven 200 - initial version, widely sold; individual customer designations within this series
- BAC One-Eleven 300 - uprated engines, more fuel for longer range; individual customer designations within this series
- BAC One-Eleven 400 - Series 300 with US instrumentation and equipment; the definitive short-body version; individual customer designations within this series
- BAC One-Eleven 475 - Series 400 body with Series 500 wing and powerplant plus rough-airfield landing gear and body protection
- Rombac 111-495 - Romanian-built version of the Series 475
- BAC One-Eleven 500 - extended body version with up to 119 seats; new engines; individual customer designations within this series
- BAC One-Eleven 510ED - Variant of the 500 series built for BEA/British Airways. Size and engines same as other 500s, cockpit modified to provide more commonality with HS.121 Trident and required a different type rating from all other 500 series One-Elevens.
- Rombac 111-560 - Romanian-built version of the Series 500
- BAe One-Eleven 670 - series 475 with improved aerodynamics and reduced noise; one converted from Series 475
[edit] British operators
- AB Airlines (incl. AB Shannon and Air Bristol)
- Autair
- British Airways
- British Caledonian
- British Eagle International
- British European Airways
- British United Airways
- Court Line Aviation
- Dan Air
- European Aviation Air Charter
- Laker Airways
- Monarch Airlines
[edit] Military operators
- Australia
- Brazil
- Oman
- U.K.
- Royal Air Force - Empire Test Pilot School
[edit] Specifications (BAC One-Eleven 200)
General characteristics
- Crew: 2 pilots and 3 flight attendants
- Capacity: 89 passengers in charter layout
- Length: 92 ft 6 in (28.2 m)
- Wingspan: 88 ft 6 in (26.9 m)
- Height: 23 ft 9 in (7.2 m)
- Wing area: 1,003 ft² (93.2 m²)
- Empty weight: 46,405 lb (21,049 kg)
- Max takeoff weight: 74,500 lb (33,800 kg)
- Powerplant: 2× Rolls-Royce RB.163 Spey Mk. 506 turbofans, 10,600 lbf (47 kN) each
Performance
- Maximum speed: 470 knots (540 mph, 870 km/h)
- Cruise speed: 430 knots (495 mph, 795 km/h)
- Range: 1,250 nm (1,440 mi, 2,320 km)
- Service ceiling: 35,000 ft (10,700 m)
[edit] Incidents
- On 10 June 1990, British Airways Flight 5390's cockpit window blew out resulting in the flight crew to cling to the pilot's legs. The plane made an emergency landing at Southampton Airport. The pilot survived.
[edit] References
[edit] External links
[edit] Related content
Comparable aircraft
Designation sequence
- BAC 1-11 - BAC TSR-2 - BAC 167 - SEPECAT Jaguar - Concorde - Panavia Tornado
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