| One-Eleven | |
|---|---|
| A British Island Airways BAC One-Eleven. | |
| Role | Short-range jetliner |
| Manufacturer | British Aircraft Corporation |
| First flight | 20 August 1963 |
| Introduction | 1965 |
| Status | Limited Service |
| Primary users | British Airways American Airlines Braniff Airways British United Airways |
| Produced | 1963–1982 (United Kingdom) 1982–1989 (Romania) |
| Number built | 244 |
The British Aircraft Corporation One-Eleven, also known as the BAC-111, BAC-1-11 or BAC 1-11, was a British short-range jet airliner of the 1960s and 1970s. Conceived by Hunting Aircraft, it was developed and produced by the British Aircraft Corporation when Hunting merged into BAC along with other British aircraft makers in 1960.
The One-Eleven was designed to replace the Vickers Viscount on short-range routes. Following the French Sud Aviation Caravelle, it was the second short-haul jet airliner to enter service. This gave it the advantage of more efficient engines and previous jet-airliner experiences, making it a popular model; over half its sales at launch were to the largest and most lucrative market, 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.
Contents |
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, under British government pressure, merged with Vickers-Armstrongs, Bristol, and English Electric to form BAC.
In 1961, BAC decided to continue work on the Hunting 107 as a private venture. It redesignated it One-Eleven, meaning 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 configuration, and reduced its capacity to 80 seats; this version became the One-Eleven 200, the original design having retroactively become the 100.
On 9 May 1961 British United Airways (BUA) placed the first order for ten One-Eleven 200s. On 23 October Braniff Airways in the United States ordered six. Mohawk Airlines sent representatives to Europe seeking out a new aircraft to bring them into the jet era, and on 24 July 1962 concluded an agreement for four One-Elevens.[1] Other orders followed from Kuwait Airways for three, and Central African Airways for two. Braniff subsequently doubled its order to twelve, while Aer Lingus ordered four. Western Airlines ordered ten aircraft but later cancelled. Bonanza Air Lines also wanted to order One-Elevens at a later stage but was stopped by protectionist action of the United States 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. 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. On 17 July 1963, American Airlines ordered fifteen aircraft, bringing the order total to sixty, plus options for more. American Airlines eventually bought a total of thirty of the 400-series, making the airline the largest ever customer of One-Elevens.
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 a 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, flown by test pilot Mike Lithgow, crashed with the loss of all on board on 22 October during stall testing. The investigation led to the discovery of what became known as deep stall or superstall, a phenomenon caused by reduced airflow to the tailplane caused by the combined blanking effects of the wing and the aft-mounted engine nacelles at high angles of attack, which prevents recovery of normal (nose-down) flight.[2] To preclude such stalls, 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. The specially modified aircraft used for testing this problem is located at Brooklands Museum, Weybridge, Surrey, UK.
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 modification of the aircraft. By the end of 1964, thirteen aircraft had rolled off the production line.
The One-Eleven was certified 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 airlines had received 34 aircraft. Demand continued to be buoyant, with a second production line set up at Weybridge.
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 8 ft 4in (2.54 m) ahead of the wing and 5 ft 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 reduce runway requirements.
BEA/British Airways 500 series aircraft (denoted 1-11 510ED) varied significantly from other 1-11s, at BEA's 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. Their additional equipment included a more sophisticated autoflight system, which allowed CAT II autolandings and included an autothrottle. The modifications went as far as reversing the "on" position of most switches to match that of the Trident; indeed, the 510ED was so different from other One-Elevens and 500 series aircraft that a different type rating was required to fly it.
Having faced competition from US aircraft by 1966, by 1970 the One-Eleven also faced competition from newer, smaller aircraft such as the Fokker F28. The F28 was lighter, less complex, and cheaper. The One-Eleven 475 of 1970 was launched to compete with the F28. It combined the 400 fuselage with the higher power and larger wing of the 500 and was intended for hot and high operations, however only ten One-Eleven Mk 475 were sold. In 1977, the One-Eleven 670, a quiet and updated 475, was offered to the Japanese domestic market, also 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 a quieter and more powerful version of the Spey engine, 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.
By 1974, BAC invested 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, but was ultimately 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 U.S. short/medium range airliners and it did not progress to the design stage.
The BAC Two-Eleven and Three-Eleven were British airliner studies proposed by the British Aircraft Corporation in the late 1960s which never made it to production.
On 9 June 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 1-11.
The first Rombac One-Eleven, (YR-BRA cn 401) a series 561RC was rolled out at Romaero Băneasa factory on 27 August 1982, and flew for the first time on 18 September 1982. Production continued until 1989 at a much slower pace than foreseen in the contract: nine aircraft were delivered. The first aircraft was delivered to TAROM on 29 December 1982. The Romanian carrier took delivery of all but two of the aircraft produced, with the remaining two going to Romavia, the last of which (YR-BRI cn 409) was delivered on 1 January 1993.
There were three reasons why the Rombac initiative failed: Romania's economy and international position deteriorated to the point where supplies for One-Eleven manufacture slowed to a trickle; the market foreseen by the Romanians failed to show an interest, though some Rombac machines were leased out to European operators; the One-Eleven's noise level and fuel economy had failed to keep pace with US and West European competition. Adopting a new engine would have resolved noise and fuel economy issues, however Rolls-Royce repeatedly refused to allow its Tay engine to be used on Romanian One-Elevens. This reluctance is assumed be based upon fears that the Fokker 100, the Tay's launch airframe, would suffer from the Romanian competition.
The BAC-One Eleven found itself in direct competition with the Douglas DC-9, and the aircraft was on the market more than a year before the Boeing 737.[3] Advantages over the DC-9 included a cheaper unit cost. However the DC-9 offered more seating and its engines were interchangeable with those on the Boeing 727. These factors encouraged Trans Australia Airlines to purchase the DC-9 instead.[4]
Mohawk Airlines' first One-Eleven, christened Ohio, went into service on 25 June 1965. By the end of the decade, the airline operated a fleet of 20 BAC One-Elevens.[5] This significant investment directly led to the demise of the company, a gamble that didn't pay off due to an economic downturn and strike action.[6] Perhaps one of the most notable incidents of a single aircraft in North America; a Philippine Airlines' One-Eleven was involved in a ground hijacking incident in 21 May 1982. The lone hijacker, John Clearno, was overpowered by the cockpit crew following hours of negotiation, no passengers or crew were injured.[7]
In Europe One-Elevens 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 of bringing the Rolls-Royce Spey engines into compliance with this, by developing a hush kit, proved expensive for the smaller operators still using this aircraft type. Therefore very few 1-11s were fitted with hush kits, and most European operators disposed of the type from their fleet.
Total production of the One-Eleven in British and Romanian factories was 244, with two airframes left incomplete in Romania. A major initiative to re-engine corporate One-Elevens with Tay engines gathered pace in the USA in the late 1980s and early 1990s but came to naught after several successful test flights. Passive opposition from the engine maker among other factors is claimed to have sabotaged its chances of success.
British Airways retired its last One-Eleven in 1998. In 2010, the European Aviation Safety Agency accepted an Airbus request to revoke the Type Certificate for the BAC One Eleven. As a result BAC 1-11 aircraft registered in any EU Member State are no longer eligible for a Normal Certificate of Airworthiness.
The BAC One-Eleven was widely used by civil and military operators.
As of July 2010 a total of 12 BAC One-Eleven aircraft (all variants) remain in airline service with International Trans Air Business.
Northrop Grumman continues to operate three BAC One-Eleven 401/AK aircraft as airborne testbeds.[8] The aircraft are operated from the Baltimore/Washington International Thurgood Marshall Airport.[9]
| Measurement | 200 | 300/400 | 475 | 500 |
|---|---|---|---|---|
| Cockpit crew | 2 | |||
| Seating capacity | 89 to 119 | |||
| Length | 28.50 metres (93 ft 6 in) | 32.61 metres (107 ft 0 in) | ||
| Wingspan | 26.98 metres (88 ft 6 in) | 28.50 metres (93 ft 6 in) | ||
| Wing area | 91.04 square metres (979.9 sq ft) | 95.78 square metres (1,031.0 sq ft) | ||
| Height | 7.47 metres (24 ft 6 in) | |||
| Cabin Width | 3.16 metres (10 ft 4 in) | |||
| Fuselage Width | 3.4 metres (11 ft 2 in) | |||
| Typical empty weight | 21,049 kilograms (46,410 lb) | 23,050 kilograms (50,800 lb) | 23,464 kilograms (51,730 lb) | 24,758 kilograms (54,580 lb) |
| Maximum take-off weight | 35,833 kilograms (79,000 lb) | 40,142 kilograms (88,500 lb) | 44,678 kilograms (98,500 lb) | 47,400 kilograms (104,000 lb) |
| Maximum landing weight | 32,204 kilograms (71,000 lb) | 35,380 kilograms (78,000 lb) | 39,462 kilograms (87,000 lb) | |
| Maximum payload | 7,981 kilograms (17,600 lb) | 9,083 kilograms (20,020 lb) | 9,647 kilograms (21,270 lb) | 11,983 kilograms (26,420 lb) |
| Takeoff run at MTOW | 1,981 metres (6,499 ft) | 2,270 metres (7,450 ft) | 1,676 metres (5,499 ft) | 1,981 metres (6,499 ft) |
| Service ceiling | 10,670 metres (35,010 ft) | 11,285 metres (37,024 ft) | ||
| Maximum cruising speed | 882 km/h (548 mph) | 871 km/h (541 mph) | ||
| Range fully loaded | 1,140 kilometres (710 mi) | 2,300 kilometres (1,400 mi) | 3,000 kilometres (1,900 mi) | 2,744 kilometres (1,705 mi) |
| Engine (x 2) | Rolls-Royce RB.163 Spey Mk 506-14 |
Rolls-Royce RB.163 Spey Mk 511-14 |
Rolls-Royce RB.163 Spey Mk 512-14DW |
|
| Max. thrust (x 2) | 4,720 Kgf 10,410 lbf (46.3 kN) |
5,200 Kgf 11,400 lbf (51.0 kN) |
5,690 Kgf 12,550 lbf (55.8 kN) |
|
|
|||||
|
|||||||||||||||||||||||
|
||||||||||||||