Airbus A310

Airbus Out of production since 1998
1982First flight
255Units built
220Typical passengers
9,630 kmRange
148On Vuelopedia
Airbus A310 illustration Illustrative image; it may differ from the actual aircraft.

The Airbus A310 is a wide-body airliner designed and manufactured by Airbus Industrie GIE, then a consortium of European aerospace manufacturers. Airbus had identified a demand for an aircraft smaller than the A300, the first twin-jet wide-body. On 7 July 1978, the A310 (initially the A300B10) was launched with orders from Swissair and Lufthansa. On 3 April 1982, the first prototype conducted its maiden flight, and the A310 received its type certificate on 11 March 1983. Keeping the same eight-abreast cross-section, the A310 is 6.95 m (22 ft 10 in) shorter than the initial A300 variants, has a smaller wing, down from 260 to 219 m2 (2,800 to 2,360 sq ft), and a longer flying range up to 5,150 nautical miles (9,540 km; 5,930 mi). The A310 introduced a two-crew glass cockpit, later adopted for the A300-600 with a common type rating.

Specifications

Figures for the A310-300 variant, the most representative of the family

Length46.7 m153 ft
Wingspan43.9 m144 ft
Height15.8 m52 ft
Range9,630 km5,200 NMWith a typical passenger load
Cruise speed850 km/h459 ktMach 0.80
Service ceiling12,530 m41,109 ftIt flies above Everest (1.4 times its height)
Maximum take-off weight164,000 kg361,558 lb
Maximum payload84,793 kg186,936 lbIts 220 passengers with baggage would weigh about 22.0 t; the rest is fuel and cargo
Typical capacity220 passengersUp to 280 in a high-density layout
Endurance11 h 20 minAt cruise speed, non-stop

The type first flew in 1982 (44 years ago) · About 255 units built · Production ended in 1998

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

The story of the type

Development

Background

On 26 September 1967, the governments of France, West Germany and the United Kingdom signed a memorandum of understanding to commence the joint development of the 300-seat Airbus A300. The French and West Germans reached a firm agreement on 29 May 1969, after the British withdrew from the project on 10 April 1969. This collaborative effort between the two states resulted in the production of the consortium's first airliner, known as the Airbus A300. The A300 was a wide-body medium-to-long range passenger airliner; it holds the distinction of being the first twin-engine wide-body aircraft in the world. The design was relatively revolutionary for its time, and featured a number of industry firsts, making the first use of composite materials on a commercial aircraft; during 1977, the A300 became the first ETOPS-compliant aircraft, which was made possible due to its high performance and safety standards. The A300 would be produced in a range of models, and sold relatively well to airlines across the world, eventually reaching a total of 561 delivered aircraft during its production life.

During the development of the earlier A300, a range of different aircraft size and capacity were studied by the consortium; the resulting Airbus A300B proposal was one of the smaller options. When the A300B1 prototypes emerged, a number of airlines issued requests for an aircraft with greater capacity, which resulted in the initial production A300B2 version. As the A300 entered service, it became increasingly apparent that there was also a sizeable market for a smaller aircraft; some operators did not have enough traffic to justify the relatively large A300, while others wanted more frequency or lower aircraft-distance costs at the expense of higher seat-distance cost (specifically Swissair and Lufthansa). At the same time, there was great pressure for Airbus to validate itself beyond the design and manufacture of a single airliner. In response to these desires, Airbus explored the options for producing a smaller derivative of the A300B2.

Design effort

In order to minimise the associated research and development costs for the tentative project, Airbus chose to examine several early design studies performed during the A300 programme. The company ultimately chose to prioritise its focus on one option, which became known as the A300B10MC (standing for Minimum Change). As envisioned, the airliner's capacity was reduced to a maximum of 220 passengers, which was viewed at the time as being a desired capacity amongst many airlines. However, such a design would have resulted in a relatively small fuselage being mated to a comparatively large wing and oversized undercarriage; such an arrangement would have, amongst other things, made the aircraft consume an unnecessarily larger amount of fuel as it carried heavier weight than what was otherwise required.

Another problem for the programme was presented in the form of inflation, the rate of which in the United Kingdom (one of the early members of the Airbus consortium) was around 35 per cent during 1979–80. This factor was responsible for significantly raising the program's development costs and, as a knock-on effect, increase the per-unit cost of the resulting airliner. During the development of the A300, British manufacturer Hawker Siddeley Aviation (HSA) had been appointed as the subcontractor to perform the manufacturing of the wing of the aircraft; shortly afterwards, the British government chose to withdraw from the newly formed venture during 1969. In 1977, HSA subsequently merged with three other British aircraft companies, resulting in the formation of British Aerospace (BAe). By this point in time, the British government had publicly indicated its intentions to rejoin the Airbus programme. In May 1976, the French government entered into a series of discussions on cooperation, during which its representatives stated that the placing of an order by British Airways (BA) was a condition for the re-admission of the United Kingdom into Airbus Industrie as a full partner.

However, both BA and Rolls-Royce had not relinquished their will to collaborate with the Americans in future aircraft endeavours and, in BA's case, procure American aircraft. During the late 1970s, BA sought to purchase two separate types of aircraft in development by American company Boeing, initially known as the 7N7 and 7X7, which would develop into the 757 and 767, the latter of which being an intended rival to the upcoming A310, as well as the existing Boeing 747. Independent of the British government, BAe commenced its own dialogue between itself and American aircraft manufacturers Boeing and McDonnell Douglas, for the purpose of assessing if BAe could participate in any of their future programmes, although the company's chairman, Lord Beswick, publicly stated that the overall aim of the firm was to pursue collaboration in Europe. At the 1978 Farnborough Air Show, Eric Varley, the British Secretary of State for Industry, announced that BAe was to rejoin Airbus Industrie and participate as a full partner from 1 January 1979 onwards.

Variants

The A310 is available in two basic versions: the medium-range A310-200 and the longer-range A310-300. The first version of the aircraft to be developed was the -200, but this was later joined by the -300, which then became the standard production version of the aircraft. The short-range -100 variant was never developed due to low demand.

A310-200

The first A310, the 162nd Airbus off the production line, made its maiden flight on 3 April 1982 powered by the earlier Pratt & Whitney JT9D-7R4D1 engines. The -200 entered service with Swissair and Lufthansa a year later. Late series -200 also featured wing fences identical to those of the -300. The first three A310s were initially fitted with outboard ailerons; they were later removed once testing showed them to be unnecessary. Production of the A310-200 ended in 1988.

A310-200C

A convertible version, the seats can be removed and cargo placed on the main deck, the A310-200C entered service with Martinair on 29 November 1984.

A310-200F

The freight version of the A310-200 was available as a new build, or as a conversion of existing wide-bodied aircraft. The A310-200F freighter can carry 39 t (86,000 lb) of freight for 5,950 km (3,210 nmi; 3,700 mi). No production freighters of the A310-200F were produced. The converted Airbus A310-200F entered service with FedEx Express in 1994.

A310-300

First flown on 8 July 1985, the -300 is dimensionally identical to the -200, although it provides an increased Maximum Take-Off Weight (MTOW) and an increase in range, provided by additional centre and horizontal stabiliser (trim-tank) fuel tanks. This model also introduced wingtip fences to improve aerodynamic efficiency, a feature that has since been retrofitted to some -200s. The aircraft entered service in 1986 with Swissair. The A310-300 incorporates a computerised fuel distribution system which allows it to be trimmed in flight, optimising the centre of gravity by shuttling up to 5,000 kg (11,000 lb) of fuel in and out of the horizontal stabiliser tank, controlled by the Centre of Gravity Control Computer.

A310-300C

The combi version of the A310-300. It can be easily converted for passenger or cargo transport: the seats can be removed and cargo placed on the main deck.

A310-300F

The freight version of the A310-300. Operators such as FedEx Express acquired modified ex-passenger A310s, usually starting with the -300 version. No production freighters of the A310-300F were produced.

A310 MRT/MRTT

The A310 has been operated by several air forces as a pure transport, the A310-300 MRT (Multi-Role Transport). However several have now been converted to the A310 MRTT (Multi-Role Tanker Transport) configuration by EADS, providing an air-to-air refuelling capability. At least six have been completed; four by the German Air Force (Luftwaffe), and two by the Royal Canadian Air Force (RCAF). Deliveries began in 2004. Three were converted at EADS EFW in Dresden, Germany; the other three at Lufthansa Technik in Hamburg, Germany.

A310 Zero G

One A310 airframe became a scientific research laboratory dedicated to weightlessness. This reduced-gravity aircraft is used to realise parabolas, allowing to perform twenty-two seconds of weightlessness. Operated by Novespace, subsidiary of CNES, French Space Agency, A310 Zero G is based at Bordeaux Mérignac airport. It also performs scientific flights, recreational flights under the Air Zero G brand, and movie special effects, such as for The Mummy (2017).

Differences between variants

Below is a list of major differences between the A310 variants.

Aircraft model designations

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

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This page was last updated on October 10, 2026

APA

Vuelopedia. (2026, October 10). Airbus A310. Retrieved October 16, 2026, from https://vuelopedia.org/en/model/a310

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BibTeX

@misc{vuelopedia_en_model_a310,
  author       = {{Vuelopedia}},
  title        = {{Airbus A310}},
  publisher    = {Fundación Poderia},
  year         = {2026},
  date         = {2026-10-10},
  url          = {https://vuelopedia.org/en/model/a310},
  howpublished = {\url{https://vuelopedia.org/en/model/a310}},
  urldate      = {2026-10-16},
  note         = {Accessed 2026-10-16}
}

Wikipedia

{{cite web |url=https://vuelopedia.org/en/model/a310 |title=Airbus A310 |website=Vuelopedia |publisher=Fundación Poderia |date=2026-10-10 |access-date=2026-10-16 |language=en}}

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